W DOC AIRBUS | AMM A320F

AIDS INTERCONNECTION (DMU, DAR) - DESCRIPTION AND OPERATION

** ON A/C NOT FOR ALL
1. General
A. Purpose of the Aircraft Integrated Data System
With the integration of modern, state-of-the-art technology like the fly-by-wire or the Full Authorized Digital Engine Control (FADEC) the complexity of the aircraft systems leads to the development of the Central Fault Maintenance System (CFDS) and the Aircraft Integrated Data System (AIDS).
While the CFDS is intend to assist the line maintenance in isolating faults, detected by the BITE functions of the individual aircraft system, the main function of the AIDS is to convert various critical flight parameters into a recordable form.
The recorded parameters are then stored on one of the subsequent storage mediums:
  • A Digital Flight Data Recorder (DFDR / FDIMU configuration (FDIU part))
  • An optional Quick Access Recorder (QAR / FDIMU configuration (FDIU part))
  • An optional Digital AIDS Recorder (DAR / FDIMU configuration (DMU part)).
Long term trend monitoring of the engines and the APU avoid expensive unscheduled maintenance actions outside the main base of the aircraft operator. Continuous monitoring of the engines and the APU is also intended to substitute fixed interval inspections by on demand maintenance.
In addition the AIDS is used for various tasks like hard landing detection, crew proficiency monitoring and any type of special investigations and trouble shooting on system level.

B. Realization of the Aircraft Integrated Data System
The AIDS is organized around the DMU which interfaces with other aircraft systems. The parameters from several aircraft systems data lines are transferred into the DMU through the ARINC-429 DITS data busses.
Based on the occurrence of specific conditions or events, the DMU triggers pre-defined actions. As a result of specific trigger conditions AIDS reports the subsequent actions can take place:
  • Generation of AIDS reports
  • Data recording on the Digital AIDS Recorder (DAR, WGL-DAR) (optional)
  • Storage in the DMU internal Smart AIDS Recorder (SAR).
The subsequent options are available for the manipulation of print report:
  • Printout through the cockpit printer
  • Transmission through the ACARS
  • Retrieval through the MDDU and/or PDL
  • Downloaded on the PCMCIA card.
You can also retrieve the SAR data through the MDDU and/or PDL.
(1) AIDS Part Function:
The AIDS-part of the FDIMU monitors the data supplied by different aircraft systems. This data enables the operator to adapt his maintenance-planning. Long-term trend-monitoring of the engines and the APU prevent expensive unscheduled maintenance-actions out of the primary base from the aircraft operator. Also the AIDS is used for different tasks like hard landing-detection, team-proficiency-monitoring and trouble-shooting on system-level.

(2) DFDRS Part Function:
(Ref. AMM D/O 31-33-00-00).
** ON A/C NOT FOR ALL
2. Component Location
F AIDS elements in cockpit - Component location ** ON A/C NOT FOR ALL
F Linear Accelerometer - Component location ** ON A/C NOT FOR ALL
F DMU (FDIMU) and DAR (WDAR) - Component location ** ON A/C NOT FOR ALL
The DMU (FDIMU) and/or DAR are installed in the electronics rack, the remote print button is installed on the pedestal of the cockpit.
For the component location of equipment which is not part of the circuit TV see the related ATA chapter:

ATA 22-82 AFL - CONTROL AND DISP. UNIT for CA
ATA 23-24 COM - AIRCRAFT COMMUNICATION for RB
ATA 31-32 IND - CENTRALIZED FAULT DISP for TW
ATA 31-33 IND - FLIGHT DATA RECORDING for TU
ATA 31-35 IND - MULTIFUNCTION PRINTER for TW
FIN FUNCTIONAL
DESIGNATION		 PANEL ZONE ACCESS
DOOR		 ATA REF
** ON A/C NOT FOR ALL
1TV DMU 87VU 120 31-36-34
** ON A/C NOT FOR ALL
10TV1 DISK - FDIMU S/W, FDIU PART 87VU 120 31-36-00
10TV2 DISK - FDIMU S/W, DMU SYSTEM 87VU 120 31-36-00
** ON A/C NOT FOR ALL
10TV DMU/FDIU (FDIMU) 87VU 120 31-36-34
** ON A/C NOT FOR ALL
10TV DMU/FDIU (FDIMU) 87VU 120 31-36-34
** ON A/C NOT FOR ALL
2TV DAR 87VU 120 31-36-52
2TV1 MEMORY MEDIA (DAR) 87VU 120 31-36-00
** ON A/C NOT FOR ALL
10TVSW3 FDIMU S/W, ACMS DMU PART, OFP 87VU 120 31-36-00
10TVMD3 FDIMU S/W, ACMS DMU PART, OFP 87VU 120 31-36-00
** ON A/C NOT FOR ALL
10TVSW2 FDIMU S/W, ACMS DMU PART, OFP 87VU 120 31-36-00
10TVMD2 FDIMU S/W, ACMS DMU PART (MEDIA), OFP 87VU 120 31-36-00
10TVMD2 FDIMU S/W, ACMS DMU PART (MEDIA), OFP 210 31-36-00
10TVSW2 FDIMU S/W, ACMS DMU PART, OFP 824 120 31-36-00
10TVMD2 FDIMU S/W, ACMS DMU PART (MEDIA), OFP 824 120 31-36-00
10TVSW3 FDIMU S/W, ACMS DMU PART, OFP 824 120 31-36-00
10TVMD3 FDIMU S/W, ACMS DMU PART, OFP 824 120 31-36-00
** ON A/C NOT FOR ALL
3. System Description
F System Block Diagram ** ON A/C NOT FOR ALL

The AIDS mainly consists of the Data Management Unit (DMU) or DMU-part of FDIMU and an optional Digital AIDS Recorder (DAR). The DMU / FDIMU (DMU-part) is the central part of the AIDS and is programmable via the Application Generation Station (AGS) or Ground Support Equipment (GSE).
The DMU / FDIMU (DMU-part) is a high-performance avionic computer specialized in the acquisition of ARINC 429 DITS data and associated processing. The tasks are processed in real time.
An integral part of the DMU / FDIMU (DMU-part) is the Smart Access Recorder (SAR). This module stores the flight data using solid state memory.
If installed, the other part of the DMU is the PCMCIA interface. This interface is able to accept the rotate and solid state ATA disks to store SAR data, DAR data or generated AIDS standard reports.

A. System Architecture
(1) Hardware
  • A Data Management Unit (DMU) / Flight Digital Interface and Management Unit (FDIMU)
  • A Digital AIDS Recorder (DAR) (option)
  • An in the DMU integrated Smart Access Recorder (SAR).

(2) Software
  • Boot software
  • DMU / FDIMU (DMU-part) system software
  • DMU / FDIMU (DMU-part) setup data-base software.

(3) Generic Function of the DMU / FDIMU (DMU-part)
One of the usual functions of the DMU / FDIMU (DMU-part) is the generation of reports as a result of specific events defined by trigger conditions.

The subsequent AIDS standard reports are defined:
Additional AIDS reports:
For most of these reports, changes in the trigger limits or in the length of the report can occur. Also, user-specific trigger-conditions can be created for each report with the GSE-based reconfiguration software. New complete reports, other than the above listed standard-reports, can be programmed by the airline user.

The DMU / FDIMU can record AIDS data through the DAR, through the SAR or through the integrated PCMCIA interface (if installed). The storage media of the DAR is a magnetic tape cartridge or an optical disk. To read the SAR data, use a floppy disk through the PDL/MDDU or a PCMCIA card through the PCMCIA interface (if installed).

The DMU / FDIMU (DMU-part) has different communication interfaces for operator dialogue and ground communications. The operation of these communication channels is usually programmable. For example, reports can be printed, transmitted to the ground through ACARS or retrieved with a floppy disk through the PDL / MDDU. This shows that each airline user can setup the DMU / FDIMU to support the airline specific-data-link structure satisfactorily.

(4) DMU / FDIMU (DMU-part) Transfer Interfaces:
(a) MCDU
  • Manual request of reports and SAR/DAR recording
  • Display of list of stored reports and SAR files
  • Online display of selected aircraft parameters
  • Different control and reprogramming menus
  • Entry for access to the PCMCIA card information (if installed).

(b) PRINTER
  • Printout of reports, manually started (by MCDU)
  • Automatic printout of reports
  • Printout of MCDU screens
  • Printout of software load messages.

(c) PDL/MDDU
  • Retrieval of reports and SAR files, manually started (by MCDU)
  • Automatic retrieval of reports and SAR files
  • Load of DMU / FDIMU software.

(d) ACARS
  • Download of reports, manually started (by MCDU)
  • Automatic download of reports
  • Upload of request for report generation
  • Upload of reprogramming messages.

(e) DAR (optional)
  • Recording of AIDS data, manually started (by MCDU)
  • Automatical recording of AIDS data.

(f) SAR
The data from the SAR data storage buffer are retrievable through the PDL/MDDU.
A remote print button (3TV) is found on the pedestal in the cockpit to start manually some specific reports. Also, the SAR recording is triggered through the print button. The report / SAR channel assignment of the remote print button is AGS / GSE programmable.

(g) PCMCIA (if installed)
The integrated PCMCIA interface has an optional DAR recording function and can store SAR generated files and AIDS standard reports. Also, it is possible to emulate a data loader function. When this functions are used, a PCMCIA card must be inserted in the PCMCIA interface.

(h) Additional Processor Board CPU-2
The additonal processor board is programmable by accepting AGS / GSE generated files. The AGS /GSE is a Personal Computer (PC) based ground support equipment. An ARINC 615 data loader interface is also provided to access the additional processor board for the upload of AGS / GSE generated files. Also for the download of memorized data.
** ON A/C NOT FOR ALL
4. Power Supply
F AIDS - Power Supply ** ON A/C NOT FOR ALL

The DMU / FDIMU is connected to the 115 V AC bus via the circuit breaker 4TV / 5TV (AIDS). The DAR is connected to the 115 V AC bus via the circuit breaker 4TV / 5TV and 28 V DC bus via circuit breaker 9TU.
------------------------------------------------------------
COMPONENT ! VOLTAGE ! BUSBAR ! C/B
------------------------------------------------------------
DMU / FDIMU ! 115 V AC ! 202XP NORM ! 4TV / 5TV
DAR / WDAR ! 115 V AC ! 202XP NORM ! 4TV / 5TV
! 28 V DC ! 202PP NORM ! 9TU
------------------------------------------------------------

** ON A/C NOT FOR ALL
5. Interface
A. Architecture of Inputs
The DMU / FDIMU is connected to various source systems to collect the whole parameter set. The block diagram of input sources (Ref. AMM D/O 31-37-00-00) shows the connection of the DMU / FDIMU to the respective sources.
B. DMU / FDIMU (DMU-Part) Input Sources
These systems are connected to the DMU / FDIMU (DMU-PART):
(1) Air Conditioning (ATA 21)
  • Pressure Controller (11HL, 12HL)
  • Zone Controller (8HK)
  • Pack Controller (7HH, 27HH).
(2) Auto Flight (ATA 22)
  • Multipurpose Control and Display Unit (3CA1, 3CA2)
  • Flight Control Unit (2CA)
  • Flight Augmentation Computer (1CC1, 1CC2)
  • Flight Management, Guidance and Envelope Computer (1CA1, 1CA2).
(3) Communication (ATA23)
  • Aircraft Communications Addressing and Reporting Management Unit (1RB1).
(4) Flight Controls (ATA 27)
  • Flight Control Data Concentrator (3CE1, 3CE2)
  • Slat and Flap Control Computer (21CV, 22CV).
(5) Fuel (ATA 28)
  • Fuel Quantity Unit (3QT).
(6) Indication/Recording (ATA 31)
  • Display Management Computer (1WT1, 1WT2)
  • Flight Warning Computer (1WW1, 1WW2)
  • System Data Acquisition Concentrator (1WV1, 1WV2)
  • Flight Data Interface Unit (2TU) (if DMU installed).
(7) Landing Gear (ATA 32)
  • Break System Control Unit 1, 2 (10GG)
  • Landing Gear Control and Interface Unit (5GA1, 5GA2).
(8) Navigation (ATA 34)
  • Ground Proximity Warning Computer (1WZ)
  • Air Data/inertial Reference Unit (1FP1, 1FP2).
(9) Pneumatic (ATA 36)
  • Bleed Monitoring Computer (1HA1, 1HA2).
(10) Onboard Maintenance System (ATA 45)
  • Central Fault Display Interface Unit (1TM1)
  • Printer (2TP).
(11) Airborne Auxiliary Power (ATA 49)
  • Electronic Control Box (59KD).
(12) Engine Fuel and Control (ATA 73)
  • Engine Vibration Monitoring Unit (2EV)
  • Electronic Engine Control/Engine Control Unit Eng 1, Eng 2 (4000KS).
C. Summary of Input/Output Data
The connection between the related computers and the FDIMU (DMU-part) is shown in the AIDS Inputs - Schematic.
The summary of the input pin assignment is shown:
  • For FDIMU (DMU-part) bus outputs - Table 1
  • For FDIMU (DMU-part) bus inputs - Table 2
  • For FDIMU ETHERNET provision - Table 3
  • For FDIMU (DMU-part) DITS inputs - Table 4
  • For FDIMU (DMU-part) discrete inputs - Table 5
  • For FDIMU (DMU-part) discrete outputs - Table 6
  • For FDIMU power supply and ground pins - Table 7
  • For FDIMU test connector pin assignment - Table 8.
-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! SPEED ! DESTINATION ! PORT NO !
! ! HI ! LO ! ! HI ! LO ! ! !
!---------------------------------------------------------------------------- !
! TP ! 11E ! 11F ! ARINC 429 ! ! X ! CFDIU, MCDU 1, ! OUT A !
! ! ! ! ! ! ! MCDU 2, PRINTER ! !
! ! ! ! ! ! ! ! !
! MP ! 11J ! 11K ! ARINC 429 ! ! X ! ACARS ! OUT B !
! ! ! ! ! ! ! ! !
! TP ! 11C ! 11D ! ARINC 429 ! X ! ! MDDU ! OUT C !
! ! ! ! ! ! ! ! !
! TP ! 11G ! 11H ! ARINC 429 ! ! X ! RESERVED ! OUT D !
! ! ! ! ! ! ! ! !
! TP ! 13A ! 13B ! HARVARD ! ! ! DAR RECORD DATA ! !
! ! ! ! BI-PHASE ! ! ! ! !
! ! ! ! ! ! ! ! !
! TP ! 15A ! 15B ! SPECIAL ! ! ! DAR SYNC SIGNAL ! !
! ! ! ! ! ! ! ! !
! TP ! 12A ! 12B ! RS 422 ! ! ! RESERVED FOR ! !
! ! ! ! ! ! ! DAR CONTROL OUT ! !
-------------------------------------------------------------------------------

FDIMU (DMU-part) Bus Outputs - Table 1

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! SPEED ! DESTINATION ! PORT NO !
! ! HI ! LO ! ! HI ! LO ! ! !
!---------------------------------------------------------------------------- !
! TP ! 11E ! 11F ! ARINC 429 ! ! X ! CFDIU, MCDU 1, ! OUT A !
! ! ! ! ! ! ! MCDU 2, PRINTER ! !
! ! ! ! ! ! ! ! !
! MP ! 11J ! 11K ! ARINC 429 ! ! X ! ACARS ! OUT B !
! ! ! ! ! ! ! ! !
! TP ! 11C ! 11D ! ARINC 429 ! X ! ! PDL ! OUT C !
! ! ! ! ! ! ! ! !
! TP ! 11G ! 11H ! ARINC 429 ! ! X ! RESERVED ! OUT D !
! ! ! ! ! ! ! ! !
! TP ! 13A ! 13B ! HARVARD ! ! ! DAR RECORD DATA ! !
! ! ! ! BI-PHASE ! ! ! ! !
! ! ! ! ! ! ! ! !
! TP ! 15A ! 15B ! SPECIAL ! ! ! DAR SYNC SIGNAL ! !
! ! ! ! ! ! ! ! !
! TP ! 12A ! 12B ! RS 422 ! ! ! RESERVED FOR ! !
! ! ! ! ! ! ! DAR CONTROL OUT ! !
-------------------------------------------------------------------------------

FDIMU (DMU-part) Bus Outputs - Table 1

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! SPEED ! SOURCE ! PORT NO !
! ! HI ! LO ! ! HI ! LO ! LRU / SYSTEM ! !
!---------------------------------------------------------------------------- !
! MP ! 5C ! 5D ! ARINC 429 ! ! X ! CFDIU ! IN-A !
! ! ! ! ! ! ! ! !
! MP ! 5J ! 5K ! ARINC 429 ! ! X ! ACARS ! IN-B !
! ! ! ! ! ! ! ! !
! MP ! 11C ! 11D ! ARINC 429 ! X ! ! MDDU ! IN-C !
! ! ! ! ! ! ! ! !
! MP ! 11A ! 11B ! ARINC 429 ! ! X ! MCDU 2 ! IN-E !
! ! ! ! ! ! ! ! !
! TP ! 11A ! 11B ! ARINC 429 ! ! X ! MCDU 1 ! IN-F !
! ! ! ! ! ! ! ! !
! TP ! 11J ! 11K ! ARINC 429 ! ! X ! PRINTER ! IN-H !
! ! ! ! ! ! ! ! !
! MP ! 12A ! 12B ! RS 422 ! ! ! DAR CONTROL IN ! !
-------------------------------------------------------------------------------

FDIMU (DMU-Part) Bus Inputs - Table 2

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! SPEED ! SOURCE ! PORT NO !
! ! HI ! LO ! ! HI ! LO ! LRU / SYSTEM ! !
!---------------------------------------------------------------------------- !
! MP ! 5C ! 5D ! ARINC 429 ! ! X ! CFDIU ! IN-A !
! ! ! ! ! ! ! ! !
! MP ! 5J ! 5K ! ARINC 429 ! ! X ! ACARS ! IN-B !
! ! ! ! ! ! ! ! !
! MP ! 11C ! 11D ! ARINC 429 ! X ! ! PDL ! IN-C !
! ! ! ! ! ! ! ! !
! MP ! 11A ! 11B ! ARINC 429 ! ! X ! MCDU 2 ! IN-E !
! ! ! ! ! ! ! ! !
! TP ! 11A ! 11B ! ARINC 429 ! ! X ! MCDU 1 ! IN-F !
! ! ! ! ! ! ! ! !
! TP ! 11J ! 11K ! ARINC 429 ! ! X ! PRINTER ! IN-H !
! ! ! ! ! ! ! ! !
! MP ! 12A ! 12B ! RS 422 ! ! ! DAR CONTROL IN ! !
-------------------------------------------------------------------------------

FDIMU (DMU-Part) Bus Inputs - Table 2

------------------------------------------------------------------------------
! CONNECTOR! PIN ! TYPE / DESCRIPTION !
!----------!-----!-----------------------------------------------------------!
! MP ! 14A ! TIN !
! ! ! !
! MP ! 14B ! TIP !
! ! ! !
! MP ! 14C ! TON !
! ! ! !
! MP ! 14D ! TOP !
! ! ! !
------------------------------------------------------------------------------

FDIMU ETHERNET Provision - Table 3


+-----------------------------------------------------------------------------+
! CONNECTOR ! PIN ! TYPE ! SPEED ! SOURCE ! PORT !SHARED!
! ! HI ! LO ! ! HI ! LO ! LRU / SYSTEM ! NO ! with !
! ! ! ! ! ! ! ! ! FDIU !
!-----------------------------------------------------------------------------!
! TP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 1 ! 05 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 2 ! 39 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 1 ! 04 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 2 ! 38 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 1 (ADC) ! 03 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 1 (IRS) ! 10 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 2 (ADC) ! 59 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 2 (IRS) ! 62 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6J ! 6K ! ARINC 429 ! ! X ! ADIRU 3 (ADC) ! 34 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6J ! 6K ! ARINC 429 ! X ! ! ADIRU 3 (IRS) ! 45 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 1 (FMC) ! 31 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 1 (FGC) ! 35 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 2 (FMC) ! 11 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 2 (FGC) ! 63 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 1 ! 53 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 1 ! 54 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 2 ! 15 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 2 ! 29 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 1 ! 55 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 2 ! 16 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 1 ! 58 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 2 ! 44 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS A) ! 08 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS B) ! 42 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 1 ! 02 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 2 ! 37 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 1 ! 07 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 2 ! 41 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 1 ! 50 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 2 ! 14 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2G ! 2H ! ARINC 429 ! ! X ! FQU (FUEL) ! 33 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2G ! 2H ! ARINC 429 ! ! X ! APU ECB ! 12 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 1! 01 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 2! 36 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 1 ! 49 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 2 ! 25 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2E ! 2F ! ARINC 429 ! ! X ! EVMU ! 32 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2E ! 2F ! ARINC 429 ! ! X ! ZONE CTRL (A) ! 60 ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5E ! 5F ! ARINC 429 ! ! X ! FDIU ! 67 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5C ! 5D ! ARINC 429 ! ! X ! GPWS ! 09 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL ! 06 ! !
! ! ! ! ! ! ! LH (A) ! ! !
! ! ! ! ! ! ! ACSC 1 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL RH ! 40 ! !
! ! ! ! ! ! ! RH (A) ! ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC1 ! 51 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC2 ! 26 ! !
+-----------------------------------------------------------------------------+

DMU DITS Inputs - Table 4

+-----------------------------------------------------------------------------+
! CONNECTOR ! PIN ! TYPE ! SPEED ! SOURCE ! PORT !SHARED!
! ! HI ! LO ! ! HI ! LO ! LRU / SYSTEM ! NO ! with !
! ! ! ! ! ! ! ! ! FDIU !
!-----------------------------------------------------------------------------!
! TP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 1 ! 06 ! !
! ! ! ! ! ! ! Ch. A ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 2 ! 30 ! !
! ! ! ! ! ! ! Ch. A ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 1 ! 05 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 2 ! 29 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 1 (ADC) ! 04 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 1 (IRS) ! 23 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 2 (ADC) ! 28 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 2 (IRS) ! 47 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6J ! 6K ! ARINC 429 ! ! X ! ADIRU 3 (ADC) ! 22 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6J ! 6K ! ARINC 429 ! X ! ! ADIRU 3 (IRS) ! 46 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 1 (FMC) ! 03 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 1 (FGC) ! 24 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 2 (FMC) ! 27 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 2 (FGC) ! 48 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 1 ! 18 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 1 ! 19 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 2 ! 42 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 2 ! 43 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 1 ! 21 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 2 ! 45 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 1 ! 20 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 2 ! 44 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS A) ! 13 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS B) ! 37 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 1 ! 02 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 2 ! 26 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 1 ! 11 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 2 ! 35 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 1 ! 12 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 2 ! 36 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2G ! 2H ! ARINC 429 ! ! X ! FQU (FUEL) ! 09 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2G ! 2H ! ARINC 429 ! ! X ! APU ECB ! 33 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 1! 01 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 2! 25 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 1 ! 10 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 2 ! 34 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2E ! 2F ! ARINC 429 ! ! X ! EVMU ! 08 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2E ! 2F ! ARINC 429 ! ! X ! ZONE CTRL (A) ! 32 ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5E ! 5F ! ARINC 429 ! ! X ! FDIU ! 15 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5C ! 5D ! ARINC 429 ! ! X ! GPWS ! 14 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL ! 07 ! !
! ! ! ! ! ! ! LH (A) ! ! !
! ! ! ! ! ! ! ACSC 1 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL ! 31 ! !
! ! ! ! ! ! ! RH (A) ! ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 14A ! 14B ! ARINC 429 ! ! ! SPARE (high ! 51 ! !
! ! ! ! ! ! !volt. protected)! ! !
! ! ! ! ! ! ! ED48A200 only ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 14J ! 14K ! ARINC 429 ! ! ! SPARE (high ! 55 ! !
! ! ! ! ! ! !volt. protected)! ! !
! ! ! ! ! ! ! ED48A200 only ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC 1 ! 16 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5J ! 5K ! ARINC 429 ! ! ! SPARE ! 17 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 4G ! 4H ! ARINC 429 ! ! ! SPARE (ATE) ! 50 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5E ! 5F ! ARINC 429 ! ! ! SPARE ! 41 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC 2 ! 40 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 4G ! 4H ! ARINC 429 ! ! ! SPARE (ATE) ! 49 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3E ! 3F ! ARINC 429 ! ! ! SPARE ! 51 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3G ! 3H ! ARINC 429 ! ! ! SPARE ! 52 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3J ! 3K ! ARINC 429 ! ! ! SPARE ! 53 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 4E ! 4F ! ARINC 429 ! ! ! SPARE ! 54 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3E ! 3F ! ARINC 429 ! ! ! SPARE ! 55 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3G ! 3H ! ARINC 429 ! ! ! SPARE ! 56 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3J ! 3K ! ARINC 429 ! ! ! SPARE ! 57 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 4E ! 4F ! ARINC 429 ! ! ! SPARE ! 58 ! !
!-----------------------------------------------------------------------------!
! (A) ZONE- and PACK-CONTROLLER installed !
! (B) ACSC installed !
+-----------------------------------------------------------------------------+

DMU DITS Inputs - Table 4

+-----------------------------------------------------------------------------+
! CONNECTOR ! PIN ! TYPE ! SPEED ! SOURCE ! PORT !SHARED!
! ! HI ! LO ! ! HI ! LO ! LRU / SYSTEM ! NO ! with !
! ! ! ! ! ! ! ! ! FDIU !
!-----------------------------------------------------------------------------!
! TP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 1 ! 06 ! !
! ! ! ! ! ! ! Ch. A ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 8K ! 9K ! ARINC 429 ! ! X ! ECU/EEC ENG 2 ! 30 ! !
! ! ! ! ! ! ! Ch. A ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 1 ! 05 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1J ! 1K ! ARINC 429 ! ! X ! BMC 2 ! 29 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 1 (ADC) ! 04 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 1 (IRS) ! 23 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1G ! 1H ! ARINC 429 ! ! X ! ADIRU 2 (ADC) ! 28 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7A ! 7B ! ARINC 429 ! X ! ! ADIRU 2 (IRS) ! 47 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6J ! 6K ! ARINC 429 ! ! X ! ADIRU 3 (ADC) ! 22 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6J ! 6K ! ARINC 429 ! X ! ! ADIRU 3 (IRS) ! 46 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 1 (FMC) ! 03 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 1 (FGC) ! 24 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1E ! 1F ! ARINC 429 ! ! X ! FMGC 2 (FMC) ! 27 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 7C ! 7D ! ARINC 429 ! X ! ! FMGC 2 (FGC) ! 48 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 1 ! 18 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 1 ! 19 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6A ! 6B ! ARINC 429 ! X ! ! FWC 2 ! 42 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6C ! 6D ! ARINC 429 ! X ! ! DMC 2 ! 43 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 1 ! 21 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 6G ! 6H ! ARINC 429 ! X ! ! SDAC 2 ! 45 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 1 ! 20 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 6E ! 6F ! ARINC 429 ! X ! ! FAC 2 ! 44 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS A) ! 13 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5A ! 5B ! ARINC 429 ! ! X ! FCU 1 (BUS B) ! 37 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 1 ! 02 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1C ! 1D ! ARINC 429 ! ! X ! LGCIU 2 ! 26 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 1 ! 11 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3A ! 3B ! ARINC 429 ! ! X ! SFCC 2 ! 35 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 1 ! 12 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 3C ! 3D ! ARINC 429 ! ! X ! FCDC 2 ! 36 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2G ! 2H ! ARINC 429 ! ! X ! FQU (FUEL) ! 09 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2G ! 2H ! ARINC 429 ! ! X ! APU ECB ! 33 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 1! 01 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 1A ! 1B ! ARINC 429 ! ! X ! PRESSURE CTRL 2! 25 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 1 ! 10 ! X !
! ! ! ! ! ! ! ! ! !
! MP ! 2J ! 2K ! ARINC 429 ! ! X ! BSCU 2 ! 34 ! X !
! ! ! ! ! ! ! ! ! !
! TP ! 2E ! 2F ! ARINC 429 ! ! X ! EVMU ! 08 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2E ! 2F ! ARINC 429 ! ! X ! ZONE CTRL (A) ! 32 ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5E ! 5F ! ARINC 429 ! ! X ! FDIU ! 15 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5C ! 5D ! ARINC 429 ! ! X ! GPWS ! 14 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL ! 07 ! !
! ! ! ! ! ! ! LH (A) ! ! !
! ! ! ! ! ! ! ACSC 1 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 2C ! 2D ! ARINC 429 ! ! X ! PACK CNTRL ! 31 ! !
! ! ! ! ! ! ! RH (A) ! ! !
! ! ! ! ! ! ! ACSC 2 (B) ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 14A ! 14B ! ARINC 429 ! ! ! SPARE (high ! 51 ! !
! ! ! ! ! ! !volt. protected)! ! !
! ! ! ! ! ! ! ED48A200 only ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 14J ! 14K ! ARINC 429 ! ! ! SPARE (high ! 55 ! !
! ! ! ! ! ! !volt. protected)! ! !
! ! ! ! ! ! ! ED48A200 only ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC 1 ! 16 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 5J ! 5K ! ARINC 429 ! ! ! SPARE ! 17 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 4G ! 4H ! ARINC 429 ! ! ! SPARE (ATE) ! 50 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5E ! 5F ! ARINC 429 ! ! ! SPARE ! 41 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 5G ! 5H ! ARINC 429 ! ! X ! HUDC 2 ! 40 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 4G ! 4H ! ARINC 429 ! ! ! SPARE (ATE) ! 49 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3E ! 3F ! ARINC 429 ! ! ! SPARE ! ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3G ! 3H ! ARINC 429 ! ! ! SPARE ! 52 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 3J ! 3K ! ARINC 429 ! ! ! SPARE ! 53 ! !
! ! ! ! ! ! ! ! ! !
! TP ! 4E ! 4F ! ARINC 429 ! ! ! SPARE ! 54 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3E ! 3F ! ARINC 429 ! ! ! SPARE ! ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3G ! 3H ! ARINC 429 ! ! ! SPARE ! 56 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 3J ! 3K ! ARINC 429 ! ! ! SPARE ! 57 ! !
! ! ! ! ! ! ! ! ! !
! MP ! 4E ! 4F ! ARINC 429 ! ! ! SPARE ! 58 ! !
!-----------------------------------------------------------------------------!
! (A) ZONE- and PACK-CONTROLLER installed !
! (B) ACSC installed !
+-----------------------------------------------------------------------------+

DMU DITS Inputs - Table 4

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! INP!
! ! ! ! ! NO !
!-----------+-----+-----------+------------------------------------------+----!
! MP ! 13G ! 717 SHUNT ! REMOTE PRINT : GND SIGNAL WHEN NOT ! 01 !
! ! ! ! DEPRESSED ! !
! ! ! ! ! !
! MP ! 15A ! - ! DIG GROUND ! -- !
! ! ! ! ! !
! MP ! 15B ! 717 SHUNT ! PROGRAM DISCR 1 > PROGRAMMING ! 02 !
! ! ! ! ! !
! MP ! 15C ! 717 SHUNT ! PROGRAM DISCR 2 ! !
! ! ! ! ! !
! MP ! 15D ! 717 SHUNT ! PROGRAM DISCR 3 ! !
! ! ! ! ! !
! MP ! 15E ! 717 SHUNT ! PROGRAM DISCR 4 ! !
! ! ! ! ! !
! MP ! 15F ! 717 SHUNT ! PROGRAM DISCR 5 ! !
! ! ! ! ! !
! MP ! 15G ! 717 SHUNT ! PROGRAM DISCR 6 ! 03 !
! ! ! ! ! !
! TP ! 14G ! 717 SHUNT ! MDDU SELECTION ! 05 !
! ! ! ! ! !
! TP ! 13E ! 717 SHUNT ! DAR BITE : FAULT = GND ! 13 !
! ! ! ! NO FAULT = 28VDC ! !
! ! ! ! ! !
! TP ! 13F ! 717 SHUNT ! DAR TRACK CHANGE : 0V FOR 1.5 SEC ! 14 !
! ! ! ! IF NOT 28VDC ! !
! ! ! ! ! !
! MP ! 13E ! 717 SHUNT ! DAR TAPE LOW : LOW = GND ! 15 !
! ! ! ! NOT LOW = 28VDC ! !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! DAR TRANSPORT RDY : READY = GND ! 16 !
! ! ! ! NOT READY = 28VDC ! !
! ! ! ! ! !
! MP ! 13J ! 717 SHUNT ! DAR TRACK 1 SELECT : CASE GND DURING ! 17 !
! ! ! ! SELECTION ! !
! ! ! ! IF NOT 28VDC ! !
! ! ! ! ! !
! MP ! 13K ! 717 SHUNT ! DAR TAPE MOTION : CORR = GND ! 18 !
! ! ! ! NOT CORR = 28VDC ! !
-------------------------------------------------------------------------------

FDIMU (DMU-part) Discrete Inputs - Table 5

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! INP!
! ! ! ! ! NO !
!-----------------------------------------------------------------------------!
! MP ! 13G ! 717 SHUNT ! REMOTE PRINT : GND SIGNAL WHEN NOT ! 01 !
! ! ! ! DEPRESSED ! !
! ! ! ! ! !
! MP ! 15A ! - ! DIG GROUND ! -- !
! ! ! ! ! !
! MP ! 15B ! 717 SHUNT ! PROGRAM DISCR 1 > PROGRAMMING ! 02 !
! ! ! ! ! !
! MP ! 15C ! 717 SHUNT ! PROGRAM DISCR 2 ! !
! ! ! ! ! !
! MP ! 15D ! 717 SHUNT ! PROGRAM DISCR 3 ! !
! ! ! ! ! !
! MP ! 15E ! 717 SHUNT ! PROGRAM DISCR 4 ! !
! ! ! ! ! !
! MP ! 15F ! 717 SHUNT ! PROGRAM DISCR 5 ! !
! ! ! ! ! !
! MP ! 15G ! 717 SHUNT ! PROGRAM DISCR 6 ! 03 !
! ! ! ! ! !
! TP ! 15G ! 717 SHUNT ! Load Enable ! 05 !
! ! ! ! ! !
! TP ! 13E ! 717 SHUNT ! DAR BITE : FAULT = GND ! 13 !
! ! ! ! NO FAULT = 28VDC ! !
! ! ! ! ! !
! TP ! 13F ! 717 SHUNT ! DAR TRACK CHANGE : 0V FOR 1.5 SEC ! 14 !
! ! ! ! OTHERWISE 28VDC ! !
! ! ! ! ! !
! MP ! 13E ! 717 SHUNT ! DAR TAPE LOW : LOW = GND ! 15 !
! ! ! ! NOT LOW = 28VDC ! !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! DAR TRANSPORT RDY : READY = GND ! 16 !
! ! ! ! NOT READY = 28VDC ! !
! ! ! ! ! !
! MP ! 13J ! 717 SHUNT ! DAR TRACK 1 SELECT : CASE GND DURING ! 17 !
! ! ! ! SELECTION, ! !
! ! ! ! OTHERWISE 28VDC ! !
! ! ! ! ! !
! MP ! 13K ! 717 SHUNT ! DAR TAPE MOTION : CORR = GND ! 18 !
! ! ! ! NOT CORR = 28VDC ! !
-------------------------------------------------------------------------------

FDIMU (DMU-part) Discrete Inputs - Table 5

+-----------------------------------------------------------------------------+
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! INP!
! ! ! ! ! NO !
!-----------+-----+-----------+------------------------------------------+----!
! MP ! 13G ! 717 SHUNT ! REMOTE PRINT :GND SIGNAL WHEN NOT ! 01 !
! ! ! ! DEPRESSED ! !
! ! ! ! ! !
! MP ! 15A ! - ! DIG GROUND ! -- !
! ! ! ! ! !
! MP ! 15B ! 717 SHUNT ! PROGRAM DISCR 1 > PROGRAMMING ! 02 !
! ! ! ! ! !
! MP ! 15C ! 717 SHUNT ! PROGRAM DISCR 2 ! !
! ! ! ! ! !
! MP ! 15D ! 717 SHUNT ! PROGRAM DISCR 3 ! !
! ! ! ! ! !
! MP ! 15E ! 717 SHUNT ! PROGRAM DISCR 4 ! !
! ! ! ! ! !
! MP ! 15F ! 717 SHUNT ! PROGRAM DISCR 5 ! !
! ! ! ! ! !
! MP ! 15G ! 717 SHUNT ! PROGRAM DISCR 6 ! 03 !
! ! ! ! ! !
! TP ! 14G ! 717 SHUNT ! MDDU SELECTION ! 05 !
! ! ! ! ! !
! TP ! 13E ! 717 SHUNT ! DAR BITE :FAULT= GND ! 13 !
! ! ! ! NO FAULT = +28VDC ! !
! ! ! ! ! !
! TP ! 13F ! 717 SHUNT ! DAR TRACK CHANGE :0V FOR 1.5 SEC ! 14 !
! ! ! ! IF NOT +28VDC ! !
! ! ! ! ! !
! MP ! 13E ! 717 SHUNT ! DAR TAPE LOW :LOW = GND ! 15 !
! ! ! ! NOT LOW = +28VDC ! !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! DAR TRANSPORT RDY :READY = GND ! 16 !
! ! ! ! NOT READY = +28VDC ! !
! ! ! ! ! !
! MP ! 13J ! 717 SHUNT ! DAR TRACK 1 SELECT :CASE GND DURING ! 17 !
! ! ! ! SELECTION, ! !
! ! ! ! IF NOT +28VDC ! !
! ! ! ! ! !
! MP ! 13K ! 717 SHUNT ! DAR TAPE MOTION :CORR = GND ! 18 !
! ! ! ! NOT CORR = +28VDC ! !
! ! ! ! ! !
! MP ! 14E ! 717 SHUNT ! Interlock WEFA1 ENABLE = GND ! 19 !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 14F ! 717 SHUNT ! SPARE ! 20 !
! ! ! ! ! !
! MP ! 14G ! 717 SHUNT ! Interlock WEFA3 ENABLE = +28VDC or ! 21 !
! ! ! ! Open Line ! !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 14H ! 717 SHUNT ! Interlock WEFA2 ENABLE = GND ! 22 !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 13G ! 717 SHUNT ! SPARE ! 23 !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! SPARE ! 24 !
! ! ! ! ! !
+-----------------------------------------------------------------------------+

FDIMU (DMU-part) Discrete Inputs - Table 5

+-----------------------------------------------------------------------------+
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! INP!
! ! ! ! ! NO !
!-----------+-----+-----------+------------------------------------------+----!
! MP ! 13G ! 717 SHUNT ! REMOTE PRINT :GND SIGNAL WHEN NOT ! 01 !
! ! ! ! DEPRESSED ! !
! ! ! ! ! !
! MP ! 15A ! - ! DIG GROUND ! -- !
! ! ! ! ! !
! MP ! 15B ! 717 SHUNT ! PROGRAM DISCR 1 > PROGRAMMING ! 02 !
! ! ! ! ! !
! MP ! 15C ! 717 SHUNT ! PROGRAM DISCR 2 ! !
! ! ! ! ! !
! MP ! 15D ! 717 SHUNT ! PROGRAM DISCR 3 ! !
! ! ! ! ! !
! MP ! 15E ! 717 SHUNT ! PROGRAM DISCR 4 ! !
! ! ! ! ! !
! MP ! 15F ! 717 SHUNT ! PROGRAM DISCR 5 ! !
! ! ! ! ! !
! MP ! 15G ! 717 SHUNT ! PROGRAM DISCR 6 ! 03 !
! ! ! ! ! !
! TP ! 14G ! 717 SHUNT ! PDL SELECTION ! 05 !
! ! ! ! ! !
! TP ! 13E ! 717 SHUNT ! DAR BITE :FAULT= GND ! 13 !
! ! ! ! NO FAULT = +28VDC ! !
! ! ! ! ! !
! TP ! 13F ! 717 SHUNT ! DAR TRACK CHANGE :0V FOR 1.5 SEC ! 14 !
! ! ! ! OTHERWISE +28VDC ! !
! ! ! ! ! !
! MP ! 13E ! 717 SHUNT ! DAR TAPE LOW :LOW = GND ! 15 !
! ! ! ! NOT LOW = +28VDC ! !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! DAR TRANSPORT RDY :READY = GND ! 16 !
! ! ! ! NOT READY = +28VDC ! !
! ! ! ! ! !
! MP ! 13J ! 717 SHUNT ! DAR TRACK 1 SELECT :CASE GND DURING ! 17 !
! ! ! ! SELECTION, ! !
! ! ! ! OTHERWISE +28VDC ! !
! ! ! ! ! !
! MP ! 13K ! 717 SHUNT ! DAR TAPE MOTION :CORR = GND ! 18 !
! ! ! ! NOT CORR = +28VDC ! !
! ! ! ! ! !
! MP ! 14E ! 717 SHUNT ! Interlock WEFA1 ENABLE = GND ! 19 !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 14F ! 717 SHUNT ! SPARE ! 20 !
! ! ! ! ! !
! MP ! 14G ! 717 SHUNT ! Interlock WEFA3 ENABLE = +28VDC or ! 21 !
! ! ! ! Open Line ! !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 14H ! 717 SHUNT ! Interlock WEFA2 ENABLE = GND ! 22 !
! ! ! ! DISABLE = +28VDC ! !
! ! ! ! ! !
! MP ! 13G ! 717 SHUNT ! SPARE ! 23 !
! ! ! ! ! !
! MP ! 13H ! 717 SHUNT ! SPARE ! 24 !
! ! ! ! ! !
+-----------------------------------------------------------------------------+

FDIMU (DMU-part) Discrete Inputs - Table 5

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! OUT!
! ! ! ! ! NO !
!-----------------------------------------------------------------------------!
! TP ! 15D ! ABD 0048 ! DMU FAIL ! 01 !
! ! ! ! ! !
! MP ! 13A ! REF SPEC ! DAR RUN CONTROL H : ! !
! ! ! ! > DMU INTERNAL ! 06 !
! MP ! 13B ! REF SPEC ! DAR RUN CONTROL L : LINK ! !
! ! ! ! : ! !
! MP ! 13F ! - ! DAR SPEED CTRL COMMON (0V OR +5V) ! !
! ! ! ! : ! !
! TP ! 13J ! REF SPEC ! DAR SPEED SELECT X 2 ! 02 !
! ! ! ! ! !
! TP ! 13K ! REF SPEC ! DAR SPEED SELECT X 4 ! 03 !
! ! ! ! ! !
! TP ! 14J ! REF SPEC ! DAR SPEED SELECT X 16 ! 04 !
! ! ! ! ! !
! TP ! 14K ! REF SPEC ! DAR SPEED SELECT X 8 ! 05 !
! ! ! ! ! !
! TP ! 15G ! REF SPEC ! DAR SPEED SELECT X 32 ! 09 !
-------------------------------------------------------------------------------

FDIMU (DMU-part) Discrete Outputs - Table 6

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! TYPE ! DESCRIPTION ! OUT!
! ! ! ! ! NO !
!-----------------------------------------------------------------------------!
! TP ! 15D ! ABD 0048 ! DMU FAIL ! 01 !
! ! ! ! ! !
! MP ! 13A ! REF SPEC ! DAR RUN CONTROL H : ! !
! ! ! ! > DMU INTERNAL ! 06 !
! MP ! 13B ! REF SPEC ! DAR RUN CONTROL L : LINK ! !
! ! ! ! : ! !
! MP ! 13F ! - ! DAR SPEED CTRL COMMON (0V OR +5V) ! !
! ! ! ! : ! !
! TP ! 13J ! REF SPEC ! DAR SPEED SELECT X 2 ! 02 !
! ! ! ! ! !
! TP ! 13K ! REF SPEC ! DAR SPEED SELECT X 4 ! 03 !
! ! ! ! ! !
! TP ! 14J ! REF SPEC ! DAR SPEED SELECT X 16 ! 04 !
! ! ! ! ! !
! TP ! 14K ! REF SPEC ! DAR SPEED SELECT X 8 ! 05 !
! ! ! ! ! !
! TP ! 15G ! REF SPEC ! DAR SPEED SELECT X 32 ! 09 !
! ! ! ! ! !
! TP ! 15E ! ABD 0048 ! SPARE ! 07 !
! ! ! ! ! !
! TP ! 15F ! ABD 0048 ! SPARE ! 08 !
+-----------------------------------------------------------------------------+

FDIMU (DMU-part) Discrete Outputs - Table 6

-------------------------------------------------------------------------------
! CONNECTOR ! PIN ! DESCRIPTION !
!-----------------------------------------------------------------------------!
! BP ! 1 ! 115V AC H !
! ! ! !
! BP ! 7 ! 115V AC L !
! ! ! !
! TP ! 15H ! DIGITAL GROUND !
! ! ! !
! TP ! 15J ! DIGITAL GROUND !
! ! ! !
! TP ! 15K ! CASE GROUND !
! ! ! !
! MP ! 15H ! DIGITAL GROUND !
! ! ! !
! MP ! 15J ! DIGITAL GROUND !
! ! ! !
! MP ! 15K ! CASE GROUND !
-------------------------------------------------------------------------------

FDIMU Power Supply and Ground Pins - Table 7

-------------------------------------------------------------------------------
! PIN ! CONTACT FUNCTION ! TYPE ! IN/OUT ! NOTE !
!-----!----------------------------------!-----------!--------------!---------!
! 1 ! 115 V AC / 400 HZ (H) ! Power ! ! !
! ! ATE Power Out 15 Watts maximum ! ! ! !
! ! ! ! ! !
! 2 ! Power Guard ! ! ! !
! ! ! ! ! !
! 3 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 4 ! +12 V DC Supply Test Point ! Power Test! ! !
! ! ! ! ! !
! 5 ! D 232OA DMU Serial 1 Out ! RS232 ! SERIAL OUT ! !
! 6 ! D 232IA DMU Serial 1 In ! RS232 ! SERIAL IN ! !
! 7 ! D 232OB DMU Serial 2 Out ! RS232 ! SERIAL OUT ! !
! ! ! ! ! !
! 8 ! D 429I49H DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! Testport H ! ! ! !
! 9 ! D 429I49L DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! Testport L ! ! ! !
! 10 ! F PDLIH FDIU ARINC429 In ! ARINC 429 ! IN ! !
! ! PDL/MDDU H ! ! ! !
! 11 ! F PDLIL FDIU ARINC429 In ! ARINC 429 ! IN ! !
! ! PDL/MDDU L ! ! ! !
! ! ! ! ! !
! 12 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 13 ! D DSCO1 DMU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 1 ! 717 SHUNT ! ! !
! ! ! ! ! !
! 14 ! F QAROH FDIU Bipolar QAR Out H ! ARINC 429 ! OUT !BipolarRZ!
! 15 ! F QAROL FDIU Bipolar QAR Out L ! ARINC 429 ! OUT !BipolarRZ!
! ! ! ! ! !
! 16 ! F BRDCSTH FDIU ARINC429 ! ARINC 429 ! OUT ! !
! ! Broadcast to DMU Out H ! ! ! !
! 17 ! F BRDCSTL FDIU ARINC429 ! ARINC 429 ! OUT ! !
! ! Broadcast to DMU Out L ! ! ! !
! ! ! ! ! !
! 18 ! D PDLIH DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! PDL/MDDU H ! ! ! !
! 19 ! D PDLIL DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! PDL/MDDU L ! ! ! !
! ! ! ! ! !
! 20 ! F PDLENA Discrete In PDL ! ARINC ! IN ! !
! ! Enable/MDDU Select ! 717 SHUNT ! ! !
! ! ! ! ! !
! 21 ! D PDLENA Discrete In PDL ! ARINC ! IN ! !
! ! Enable/MDDU Select ! 717 SHUNT ! ! !
! ! ! ! ! !
! 22 ! CGND Chassis Ground ! ! ! !
! ! ! ! ! !
! 23 ! reserved Power Guard ! ! ! !
! ! ! ! ! !
! 24 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 25 ! -12 V DC Supply Test Point ! Power Test! ! !
! ! ! ! ! !
! 26 ! F 232O FDIU Serial 1 Out ! RS232 ! SERIAL OUT ! !
! 27 ! F 232I FDIU Serial 1 In ! RS232 ! SERIAL IN ! !
! 28 ! D 232IB DMU Serial 2 In ! RS232 ! SERIAL IN ! !
! ! ! ! ! !
! 29 ! D 429I50H DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! Spare 8 H ! ! ! !
! 30 ! D 429I50L DMU ARINC429 In ! ARINC 429 ! IN ! !
! ! Spare 8 L ! ! ! !
! ! ! ! ! !
! 31 ! F PDLOH FDIU ARINC429 Out ! ARINC 429 ! OUT ! !
! ! PDL/MDDU H ! ! ! !
! 32 ! F PDLOL FDIU ARINC429 Out ! ARINC 429 ! OUT ! !
! ! PDL/MDDU L ! ! ! !
! ! ! ! ! !
! 33 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 34 ! F DSCO2 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 2 ! 717 SHUNT ! ! !
! 35 ! F DSCO3 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 3 ! 717 SHUNT ! ! !
! 36 ! F DSCO4 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 4 ! 717 SHUNT ! ! !
! 37 ! F DSCO5 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 5 ! 717 SHUNT ! ! !
! 38 ! F DSCO6 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 6 ! 717 SHUNT ! ! !
! ! ! ! ! !
! 39 ! ! ! ! !
! ! ! ! ! !
! 40 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 41 ! D DSCO2 DMU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 2 ! 717 SHUNT ! ! !
! ! ! ! ! !
! 42 ! F FAIL FDIU ARINC717 Discrete ! ARINC ! OUT ! !
! ! Out FDIU FAIL ! 717 SHUNT ! ! !
! 43 ! 115 V AC RET / 400 HZ (H) ! Power ! ! !
! ! ATE Power Out 15 Watts maximum ! ! ! !
! ! ! ! ! !
! 44 ! reserved Power Guard ! ! ! !
! ! ! ! ! !
! 45 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 46 ! + 5 V DC Supply Test Point ! Power Test! ! !
! ! ! ! ! !
! 47 ! + 3.3 V DC Supply Test Point ! Power Test! ! !
! ! ! ! ! !
! 48 ! ! ! ! !
! ! ! ! ! !
! 49 ! F DFDROH FDIU Bipolar DFDR Out H ! ARINC 429 ! OUT !BipolarRZ!
! 50 ! F DFDROL FDIU Bipolar DFDR Out L ! ARINC 429 ! OUT !BipolarRZ!
! ! ! ! ! !
! 51 ! D PDLOH DMU ARINC429 OUT ! ARINC 429 ! OUT ! !
! ! PDL/MDDU H ! ! ! !
! 52 ! D PDLOL DMU ARINC429 OUT ! ARINC 429 ! OUT ! !
! ! PDL/MDDU L ! ! ! !
! ! ! ! ! !
! 53 ! DGND Digital Ground ! ! ! !
! ! ! ! ! !
! 54 ! D DAROL DMU Bipolar DAR Out L ! ARINC 429 ! OUT !BipolarRZ!
! 55 ! D DAROH DMU Bipolar DAR Out H ! ARINC 429 ! OUT !BipolarRZ!
! ! ! ! ! !
! 56 ! D DSCO4 DMU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 4 ! 717 SHUNT ! ! !
! 57 ! F DSCO7 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 7 ! 717 SHUNT ! ! !
! 58 ! F DSCO8 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 8 ! 717 SHUNT ! ! !
! 59 ! D DSCO3 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 3 ! 717 SHUNT ! ! !
! 60 ! ! ! ! !
! ! ! ! ! !
! 61 ! F DSCO1 FDIU ARINC717 Spare ATE ! ARINC ! OUT ! !
! ! Discrete Out 1 ! 717 SHUNT ! ! !
! 62 ! D FAIL DMU ARINC717 Discrete ! ARINC ! OUT ! !
! ! Out DMU FAIL ! 717 SHUNT ! ! !
-------------------------------------------------------------------------------

Test Connector Pin Assignment - Table 8

-------------------------------------------------------------------------------
! NAME ! PIN ! FUNCTION ! TYPE ! NOTES !
!-----------!-------!-----------------------!---------!---------------------- !
! Ph115V ! 1 ! Phase 115V / 400Hz ! Output ! Output power = 15W max!
! Ntr115V ! 43 ! Neutral 115V/400Hz ! Output ! !
! PS+12V ! 4 ! Power Supply +12V ! Output ! Test only !
! PS-12V ! 25 ! Power Supply -12V ! Output ! Test only !
! PS+5V ! 46 ! Power Supply +5V ! Output ! Test only !
! Rezerved ! 47 ! --- ! --- ! --- !
! ! ! ! ! !
! MGND ! 22 ! Chassis Ground ! ! !
! EGND ! 3 ! Digital Ground ! ! !
! EGND ! 24 ! Digital Ground ! ! !
! EGND ! 45 ! Digital Ground ! ! !
! ! ! ! ! !
! BAT ! 48 ! Battery Test ! Output ! Test only !
! ! ! ! ! !
! TXD1 ! 26 ! RS232 line n°1 ! Output ! CPU FDIU !
! RXD1 ! 27 ! RS232 line n°1 ! Input ! !
! TXD2 ! 5 ! RS232 line n°2 ! Output ! CPU DMU !
! RXD2 ! 6 ! RS232 line n°2 ! Input ! !
! TXD3 ! 7 ! RS232 line n°3 ! Output ! Reserved for extension!
! RXD3 ! 28 ! RS232 line n°3 ! Input ! !
! ! ! ! ! !
! ATE1A ! 8 ! ATE channel 1 line A ! Input ! ARINC 429 port 49 !
! ATE1B ! 9 ! ATE channel 1 line B ! Input ! ARINC 429 port 49 !
! ATE2A ! 29 ! ATE channel 2 line A ! Input ! ARINC 429 port 50 !
! ATE2B ! 30 ! ATE channel 2 line A ! Input ! ARINC 429 port 50 !
! ! ! ! ! !
! DFDRA ! 49 ! DSDR line A ! Output ! ARINC !
! DFDRB ! 50 ! DSDR line B ! Output ! ARINC !
! ! ! ! ! !
! ADLINA ! 10 ! ADL data in line A ! Input ! ARINC !
! ADLINB ! 11 ! ADL data in line B ! Input ! ARINC !
! ADLAUTFA ! 31 ! ADL FDIU data out ! Output ! ARINC !
! ! ! line A ! ! !
! ADLAUDFB ! 32 ! ADL FDIU data out ! Output ! ARINC !
! ! ! line B ! ! !
! ADLAUTDA ! 51 ! ADL DMU data out ! Output ! ARINC !
! ! ! line A ! ! !
! ADLAUTDB ! 52 ! ADL DMU data out ! Output ! ARINC !
! ! ! line B ! ! !
! ADLFENA ! 20 ! Enable ADL FDIU (load)! Input ! Disc. shunt !
! ADLDENA ! 21 ! Enable ADL DMU (load) ! Input ! Disc. shunt !
! ! ! ! ! !
! FCTRSV1 ! 41 ! Factory reserved input! Input ! Disc. shunt !
! ! ! n°1 ! ! !
! FCTRSV2 ! 61 ! Factory reserved input! Input ! Disc. shunt !
! ! ! n°2 ! ! !
! ! ! ! ! !
! FDIUBITE ! 42 ! FDIU BITE ! Output ! Disc. shunt !
! DMUBITE ! 62 ! DMU BITE ! Output ! Disc. shunt !
! FCTRSV3 ! 13 ! Factory reserved input! Output ! Test only !
! ! ! n°1 ! ! !
! FCTRSV4 ! 14 ! Factory reserved input! Output ! Test only !
! ! ! n°2 ! ! !
! FCTRSV4 ! 15 ! Factory reserved input! Output ! Test only !
! ! ! n°3 ! ! !
! ADLDINA ! 18 ! ADL DMU Input A ! Input ! ARINC !
! ADLDINB ! 19 ! ADL DMU Input B ! Input ! ARINC !
! UL1 ! 16 ! Unaffected line n°1 ! In/Out ! !
! UL2 ! 17 ! Unaffected line n°2 ! In/Out ! !
! UL3 ! 34 ! Unaffected line n°3 ! In/Out ! !
! UL4 ! 35 ! Unaffected line n°4 ! In/Out ! !
! UL5 ! 36 ! Unaffected line n°5 ! In/Out ! !
! UL6 ! 37 ! Unaffected line n°6 ! In/Out ! !
! UL7 ! 38 ! Unaffected line n°7 ! In/Out ! !
! DFDRBITE ! 54 ! BITE DFDR ! Output ! Disc. shunt !
! UL8 ! 55 ! Unaffected line n°8 ! In/Out ! !
! RS422OUTA ! 56 ! RS422reserved ! Out ! !
! RS422OUTB ! 57 ! RS422reserved ! Out ! !
! RS422INA ! 58 ! RS422reserved ! In ! !
! RS422INB ! 59 ! RS422reserved ! In ! !
! EGND !Digital! Unaffected line n° ! ! !
! ! ground! ! ! !
! EGND !Digital! Unaffected line n° ! ! !
! ! ground! ! ! !
! EGND !Digital! ! ! !
! ! ground! ! ! !
! EGND !Digital! ! ! !
! ! ground! ! ! !
! UHSIN !Unaffec! ! Input ! !
! !ted hi-! ! ! !
! !speed ! ! ! !
! !line ! ! ! !
! UHSOUT !Unaffec! ! Output ! !
! !ted hi-! ! ! !
! !speed ! ! ! !
-------------------------------------------------------------------------------

Test Connector Pin Assignment - Table 8

D. Filtered Parameters
+-----------------------------------------------------+
! FDIMU Input ! Name ! Type ! Samp ! Time !
! Param No ! ! ! Per ! Const !
! ! ! ! Second ! T !
!--------------+--------------+------+--------+-------!
! 02.1.075.00 #! GW ! BNR ! 1 ! 3 !
! 04.1.324.01 #! PTCH ! BNR ! 4 ! 12 !
! 04.1.325.01 #! ROLL ANGLE ! BNR ! 4 ! 12 !
! 04.1.361.-- #! IALT ! BNR ! 8 ! 24 !
! 04.1.312.01 #! GS ! BNR ! 8 ! 24 !
! 04.1.364.01 #! VACC ! BNR ! 4 ! 12 !
! 04.1.365.01 #! IVV ! BNR ! 4 ! 12 !
! 06.1.203.01 #! ALT ! BNR ! 1 ! 3 !
! 06.1.205.01 #! MACH ! BNR ! 2 ! 6 !
! 06.1.211.01 #! TAT ! BNR ! 1 ! 3 !
! 17.1.301.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.302.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.303.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.304.00 ! A/C TYPE ! DIS ! 1 ! *1 !
! 1B.1.127.01 #! SLAT ! BNR ! 1 ! 3 !
! 29.1.002.11 #! SDAC DSW 8 ! DIS ! 2 ! * !
! ! BIT 16 ! ! ! !
! 26.1.126.01 #! FWC FLT PH ! BNR ! 2 ! * !
! ! BIT 11 TO 14 ! ! ! !
! 26.1.316.01 #! OIT ENG 1 ! BNR ! 1 ! 3 !
! 26.1.316.10 #! OIT ENG 2 ! BNR ! 1 ! 3 !
! 26.1.317.01 #! OIP ENG 1 ! BNR ! 2 ! 6 !
! 26.1.317.10 #! OIP ENG 2 ! BNR ! 2 ! 6 !
! 26.1.322.01 #! TN ENG 1 ! BNR ! 1 ! 3 !
! 26.1.322.10 #! TN ENG 2 ! BNR ! 1 ! 3 !
! 3D.1.035.01 ! EVM DSW ENG1 ! DIS ! 4 ! * !
! ! BIT 11,12 ! ! ! !
! 3D.1.035.10 ! EVM DSW ENG2 ! DIS ! 4 ! * !
! ! BIT 11,12 ! ! ! !
! 5C.1.057.01 #! PRESS DSW ! DIS ! 4 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14,15,16 ! ! ! !
! ! BIT 17,26 ! ! ! !
! 5C.1.144.01 #! CAB DIF PRS ! BNR ! 4 ! 12 !
! 5C.1.151.01 #! CAB ALT ! BNR ! 2 ! 6 !
! 5D.2.060.10 ! ZONE CTR DSW ! DIS ! 2 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14,15,16 ! ! ! !
! 6D.1.021.01 #! LGCIU DSW 2 ! DIS ! 4 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14 ! ! ! !
! 7A.1.037.01 ! APU DSW 1 ! DIS ! 2 ! * !
! ! BIT 11,17,18 ! ! ! !
! ! BIT 21,22 ! ! ! !
! 7A.1.050.01 ! APU SN ! BCD ! 1 ! *1 !
! 7C.1.046.01 ! ESN ENG1 ! BCD ! 1 ! *3 !
! 7C.2.046.10 ! ESN ENG2 ! BCD ! 1 ! *3 !
! 7C.1.047.01 ! ESN ENG1 ! BCD ! 1 ! *3 !
! 7C.2.047.10 ! ESN ENG2 ! BCD ! 1 ! *3 !
! 7C.1.131.01 ! P2 ENG1 ! BNR ! 2 ! 6 !
! 7C.2.131.10 ! P2 ENG2 ! BNR ! 2 ! 6 !
! 7C.1.244.01 ! FF ENG1 ! BNR ! 2 ! 6 !
! 7C.2.244.10 ! FF ENG2 ! BNR ! 2 ! 6 !
! 7C.1.270.01 ! DSW ENG1 ! DIS ! 4 ! * !
! ! BIT 13,14,18,! ! ! !
! ! 26 ! ! ! !
! 7C.2.270.10 ! DSW ENG2 ! DIS ! 4 ! * !
! ! BIT 13,14,18 ! ! ! !
! ! 26 ! ! ! !
! 7C.1.344.01 ! N2 ENG 1 ! BNR ! 4 ! 12 !
! 7C.2.344.10 ! N2 ENG 2 ! BNR ! 4 ! 12 !
! 7C.1.345.01 ! EGT ENG1 ! BNR ! 1 ! 3 !
! 7C.2.345.10 ! EGT ENG2 ! BNR ! 1 ! 3 !
! 7C.1.346.01 ! N1 ENG1 ! BNR ! 4 ! 12 !
! 7C.2.346.10 ! N1 ENG2 ! BNR ! 4 ! 12 !
! 8E.1.062.11 ! PACK DSW LH ! DIS ! 2 ! * !
! ! BIT 13,14 ! ! ! !
! 8E.2.062.00 ! PACK DSW RH ! DIS ! 2 ! * !
! ! BIT 13,14 ! ! ! !
! 8E.1.126.11 ! PACK FL. LH ! BNR ! 2 ! 6 !
! 8E.2.126.00 ! PACK FL. RH ! BNR ! 2 ! 6 !
! 7C.1.306.01 ! HPT ENG1 ! BNR ! 1 ! 3 !
! 7C.2.306.10 ! HPT ENG2 ! BNR ! 1 ! 3 !
! 7C.1.307.01 ! LPT ENG1 ! BNR ! 1 ! 3 !
! 7C.2.307.10 ! LPT ENG2 ! BNR ! 1 ! 3 !
! 29.1.001.00 ! LH WING AI/V ! DIS ! 2 ! * !
! ! POS BIT 18 ! ! ! !
! 29.1.001.11# ! RH WING AI/V ! DIS ! 2 ! * !
! ! POS BIT 18 ! ! ! !
! 29.1.003.11# ! APU MASTER SW! DIS ! 2 ! * !
! ! OFF BIT 16 ! ! ! !
! 29.1.055.01# ! CROSS FEED ! DIS ! 4 ! * !
! ! VALVE POS ! ! ! !
! ! BIT 16 ! ! ! !
! 5D.2.061.10 ! NACELLE AI ! DIS ! 1 ! * !
! ! POS BIT 27,28! ! ! !
! 6F.1.066.01 ! ENG2 HPV, PRV! DIS ! 4 ! * !
! ! POS BIT 15,17! ! ! !
! 6F.1.067.01 ! ENG1 HPV, PRV! DIS ! 4 ! * !
! ! POS BIT 15,17! ! ! !
!-----------------------------------------------------!
!# = If this parameter is not available, the !
! appropriate parameter from the alternative !
! system is used. !
!* = For minimum three consecutive samples the !
! appropriate bits (every bit separately) must !
! remain stable before incorporating the new !
! status into logic decisions. !
!*1= For minimum three consecutive samples the !
! appropriate bits (every bit separately) must !
! remain stable before incorporating the new !
! status into logic decisions (at power up only). !
+-----------------------------------------------------+

Filtered Parameters - Table 9

+-----------------------------------------------------+
! FDIMU Input ! Name ! Type ! Samp ! Time !
! Param No ! ! ! Per ! Const !
! ! ! ! Second ! T !
!--------------+--------------+------+--------+-------!
! 02.1.075.00 #! GW ! BNR ! 1 ! 3 !
! 04.1.324.01 #! PTCH ! BNR ! 4 ! 12 !
! 04.1.325.01 #! ROLL ANGLE ! BNR ! 4 ! 12 !
! 04.1.361.-- #! IALT ! BNR ! 8 ! 24 !
! 04.1.312.01 #! GS ! BNR ! 8 ! 24 !
! 04.1.364.01 #! VACC ! BNR ! 4 ! 12 !
! 04.1.365.01 #! IVV ! BNR ! 4 ! 12 !
! 06.1.203.01 #! ALT ! BNR ! 1 ! 3 !
! 06.1.205.01 #! MACH ! BNR ! 2 ! 6 !
! 06.1.211.01 #! TAT ! BNR ! 1 ! 3 !
! 17.1.301.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.302.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.303.00 ! A/C-IDENT ! ISO ! 1 ! *1 !
! 17.1.304.00 ! A/C TYPE ! DIS ! 1 ! *1 !
! 1B.1.127.01 #! SLAT ! BNR ! 1 ! 3 !
! 29.1.002.11 #! SDAC DSW 8 ! DIS ! 2 ! * !
! ! BIT 16 ! ! ! !
! 26.1.126.01 #! FWC FLT PH ! BNR ! 2 ! * !
! ! BIT 11 TO 14 ! ! ! !
! 26.1.316.01 #! OIT ENG 1 ! BNR ! 1 ! 3 !
! 26.1.316.10 #! OIT ENG 2 ! BNR ! 1 ! 3 !
! 26.1.317.01 #! OIP ENG 1 ! BNR ! 2 ! 6 !
! 26.1.317.10 #! OIP ENG 2 ! BNR ! 2 ! 6 !
! 26.1.322.01 #! TN ENG 1 ! BNR ! 1 ! 3 !
! 26.1.322.10 #! TN ENG 2 ! BNR ! 1 ! 3 !
! 3D.1.035.01 ! EVM DSW ENG1 ! DIS ! 4 ! * !
! ! BIT 11,12 ! ! ! !
! 3D.1.035.10 ! EVM DSW ENG2 ! DIS ! 4 ! * !
! ! BIT 11,12 ! ! ! !
! 5C.1.057.01 #! PRESS DSW ! DIS ! 4 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14,15,16 ! ! ! !
! ! BIT 17,26 ! ! ! !
! 5C.1.144.01 #! CAB DIF PRS ! BNR ! 4 ! 12 !
! 5C.1.151.01 #! CAB ALT ! BNR ! 2 ! 6 !
! 5D.2.060.10 ! ZONE CTR DSW ! DIS ! 2 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14,15,16 ! ! ! !
! 6D.1.021.01 #! LGCIU DSW 2 ! DIS ! 4 ! * !
! ! BIT 11,12,13 ! ! ! !
! ! BIT 14 ! ! ! !
! 7A.1.037.01 ! APU DSW 1 ! DIS ! 2 ! * !
! ! BIT 11,17,18 ! ! ! !
! ! BIT 21,22 ! ! ! !
! 7A.1.050.01 ! APU SN ! BCD ! 1 ! *1 !
! 7C.1.046.01 ! ESN ENG1 ! BCD ! 1 ! *3 !
! 7C.2.046.10 ! ESN ENG2 ! BCD ! 1 ! *3 !
! 7C.1.047.01 ! ESN ENG1 ! BCD ! 1 ! *3 !
! 7C.2.047.10 ! ESN ENG2 ! BCD ! 1 ! *3 !
! 7C.1.131.01 ! P2 ENG1 ! BNR ! 2 ! 6 !
! 7C.2.131.10 ! P2 ENG2 ! BNR ! 2 ! 6 !
! 7C.1.244.01 ! FF ENG1 ! BNR ! 2 ! 6 !
! 7C.2.244.10 ! FF ENG2 ! BNR ! 2 ! 6 !
! 7C.1.270.01 ! DSW ENG1 ! DIS ! 4 ! * !
! ! BIT 13,14 ! ! ! !
! 7C.2.270.10 ! DSW ENG2 ! DIS ! 4 ! * !
! ! BIT 13,14 ! ! ! !
! 7C.1.145.01 ! DSW ENG1 ! DIS ! 4 ! * !
! ! BIT 16, 19 ! ! ! !
! 7C.2.145.10 ! DSW ENG2 ! DIS ! 4 ! * !
! ! BIT 16, 19 ! ! ! !
! 7C.1.340.01 ! EPR ENG1 ! BNR ! 4 ! 12 !
! 7C.2.340.10 ! EPR ENG2 ! BNR ! 4 ! 12 !
! 7C.1.344.01 ! N2 ENG 1 ! BNR ! 4 ! 12 !
! 7C.2.344.10 ! N2 ENG 2 ! BNR ! 4 ! 12 !
! 7C.1.345.01 ! EGT ENG1 ! BNR ! 1 ! 3 !
! 7C.2.345.10 ! EGT ENG2 ! BNR ! 1 ! 3 !
! 7C.1.346.01 ! N1 ENG1 ! BNR ! 4 ! 12 !
! 7C.2.346.10 ! N1 ENG2 ! BNR ! 4 ! 12 !
! 8E.1.062.11 ! PACK DSW LH ! DIS ! 2 ! * !
! ! BIT 13,14 ! ! ! !
! 8E.2.062.00 ! PACK DSW RH ! DIS ! 2 ! * !
! ! BIT 13,14 ! ! ! !
! 8E.1.126.11 ! PACK FL. LH ! BNR ! 2 ! 6 !
! 8E.2.126.00 ! PACK FL. RH ! BNR ! 2 ! 6 !
! 7C.1.330.01 ! ACC ENG1 ! BNR ! 4 ! 12 !
! 7C.2.330.10 ! ACC ENG2 ! BNR ! 4 ! 12 !
! 29.1.001.00 ! LH WING AI/V ! DIS ! 2 ! * !
! ! POS BIT 18 ! ! ! !
! 29.1.001.11# ! RH WING AI/V ! DIS ! 2 ! * !
! ! POS BIT 18 ! ! ! !
! 29.1.003.11# ! APU MASTER SW! DIS ! 2 ! * !
! ! OFF BIT 16 ! ! ! !
! 29.1.055.01# ! CROSS FEED ! DIS ! 4 ! * !
! ! VALVE POS ! ! ! !
! ! BIT 16 ! ! ! !
! 5D.2.061.10 ! NACELLE AI ! DIS ! 1 ! * !
! ! POS BIT 27,28! ! ! !
! 6F.1.066.01 ! ENG2 HPV, PRV! DIS ! 4 ! * !
! ! POS BIT 15,17! ! ! !
! 6F.1.067.01 ! ENG1 HPV, PRV! DIS ! 4 ! * !
! ! POS BIT 15,17! ! ! !
!--------------+--------------+------+--------+-------!
!# = If this parameter is not available, the !
! appropriate parameter from the alternative !
! system must be used. !
!* = For at least three consecutive samples the !
! appropriate bits (every bit separately) must !
! remain stable before incorporating the new !
! status into logic decisions. !
!*1= For at least three consecutive samples the !
! appropriate bits (every bit separately) must !
! remain stable before incorporating the new !
! status into logic decisions (at power up only). !
+-----------------------------------------------------+

Filtered Parameters - Table 9

E. Printer Word
PRINTER ! DMU
------------------!------------------------------------------------------------
POLL ! !
! RTS !
CTS ! !
! STX !
! 1st CNTL WORD !
! 2nd CNTL WORD !> 1st block
! data for line 0 ! block is
! 1st CNTL WORD ! limited to
! 2nd CNTL WORD ! 128 words
! data for line 1 !
! . !
! . !
! . !
! 1st CNTL WORD !
! 2nd CNTL WORD !
! data for line 1 !
! ETX !
ACK ! !
! !
POLL ! !
! RTS !
CTS ! !
! STX !
! 1st CNTL WORD !
! 2nd CNTL WORD !
! data for line I+1 !
! . !> 2nd block
! . ! block is
! . ! limited to
! 1st CNTL WORD ! 128 words
! 2nd CNTL WORD !
! data for line J !
! EOT !
ACK ! !
The printer then polls the highest priority system.

Printer Word Exchange - Table 10

PRINTER ! DMU
------------------!------------------------------------------------------------
POLL ! !
! RTS !
CTS ! !
! STX Start 1st record !
! 1st CTL !
! 2nd CTL > sub-record 1 ! max
! data for line 1 !>
! 1st CTL ! 255 words
! 2nd CTL > sub-record 2 !
! data for line 2 !
! . !
! . !
! . !
! 1st CTL !
! 2nd CTL > sub-record I !
! data for line I !
! ETX End of text !
ACK ! !
POLL ! !
! RTS !
CTS ! !
! STX Start 2nd record !
! 1st CTL !
! 2nd CTL > sub-record I+1 !
! data for line I+1 !
! . ! max
! . !>
! . ! 255 words
! 1st CTL !
! 2nd CTL > sub-record J !
! data for line I+1 !
! EOT End of transmission !
ACK ! !
The printer then polls the highest priority system.
The time between each STX, CTL and data word must not exceed 200ms.

Printer Word Exchange - Table 10

F. DAR Frame Assignment (Word 1-64)
+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS !04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS !04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position ! FCDC!6C/1/362/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/326/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 25 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 25 !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 26 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/272/10! 1 !1/4! 26 !
! ! 3 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/276/01! 1 !1/4! 22 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/276/10! 1 !1/4! 23 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/274/01! 1 !1/4! 11 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/274/10! 1 !1/4! 12 !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order ! FGC I01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC I01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position ! FCDCI6C/1/364/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDCI6C/2/364/10! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 23 !
! ! ! ! ! ! DMC I25/2/272/10! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 27 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 27 !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 12 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 13 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/2/042/01! 1 !1/4! 14 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position ! FCDC!6C/1/365/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/365/10! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC !25/2/272/10! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word ! FWC !26/1/126/00! 1 !1/4! 14 !
! ! ! ! ! ! FFWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/271/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/271/10! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF ! SDAC!29/1/002/11! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/350/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/350/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC discrete status word ! FWC !26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC !26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS word #2 ! FCDC!6C/1/041/01! 1 !1/4! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 272/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 272/00 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude ! IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude ! IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position longitude! IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 ! FWC !26/1/073/01! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/01! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 ! FWC !26/1/073/10! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle ! ECU/!7C/1/ ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle ! ECU/!7C/1/ ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date ! FDIU!17/1/260/00! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date ! FDIU!17/1/260/00! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases ! FDIU!26/1/126/01! 1 !1/4! 14 !
! ! ! ! ! ! FDIU!26/2/260/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: status word ! DMC !25/1/301/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC !25/2/301/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universial time ! FDIU!17/1/125/00! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight ! FMC !02/1/075/00! 1 !1/4! 28 !
! ! ! ! ! (10kgs) ! FMC !02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/1/346/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: status word ! SDAC!29/1/046/01! 1 !1/4! 26 !
! ! ! ! ! ! SDAC!29/2/046/01! ! ! !
! ! 1-4! 1 ! 1 ! FWC bus: status word ! FWC !26/1/017/11! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC !26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine ! ECU/!7C/1/345/01! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!25 ! ! ! ! T B D ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 ! EVMU!3D/1/135/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 ! EVMU!3D/1/136/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th ! FGC !01/1/235/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th ! FGC !01/1/235/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th ! FGC !01/1/236/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th ! FGC !01/1/236/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection ! FWC !26/1/014/10! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection ! FWC !26/1/014/01! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert ! FWC !26/1/016/10! 1 ! 1 ! 18 !
! ! 1-4! 9 ! 1 ! GPWS modes ON ! FWC !26/1/016/01! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC !26/2/016/01! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) ! DMC !25/1/274/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 7 ! 1 ! MIDDLE marker ! DMC !25/1/274/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker ! DMC !25/1/274/01! 1 ! 1 ! 13 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting ! SDAC!29/1/002/11! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/11! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading ! IRS !04/1/320/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS !04/2/320/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU status word ! FCU !A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed ! ADC !06/1/206/01! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) ! ADC !06/2/206/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Indicated angle of ! ADC !06/1/221/01! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Indicated angle of ! ADC !06/1/221/01! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 3 ! Derate Take off ! EEC!7C/1/270/01! 1 ! 1 ! 13 !
! ! ! ! ! ! EEC!7C/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left ! FCDC!6C/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left ! FCDC!6C/1/314/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off ! BSCU!6E/1/026/01! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault ! BSCU!6E/1/026/01! 1 ! 1 ! 20 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! position ! FCDC!6C/1/305/10! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on ! BSCU!6E/1/027/01! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on ! BSCU!6E/1/027/01! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on ! BSCU!6E/1/027/01! 1 ! 1 ! 22 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! !6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 2 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 18 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!51 ! 1.3! 12 ! 6 ! N1 command engine #1 ! EEC!7C/1/341/01! 1 !1/2! 27 !
! ! 2.4! 12 ! 6 ! N1 command engine #2 ! EEC!7C/2/341/10! 1 !1/2! 27 !
! ! 1 ! 6 ! 6 ! N1 target feedback engine ! EEC!7C/1/341/01! 1 !1/4! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 14 !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 13 !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 15 !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 11 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 12 !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. ! DMC!25/1/230/00! 1 !1/4! 29 !
! ! ! ! ! END DATA ! DMC!25/2/230/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/2/344/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 22 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 28 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/2/244/10! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED ! IRS!04/1/315/01! 1 !1/4! 28 !
! ! ! ! ! ! IRS!04/2/315/10! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 16 !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 14 !
! ! 2 ! 12 ! 12 ! Altitude baro setting capt! DMC!25/1/222/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
! ! 3 ! 12 ! 9 ! Decision height ! DMC!25/1/370/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC!25/2/370/10! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 22 !
! ! 4 ! 8 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 26 !
! ! 4 ! 7 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 20 !
! ! 4 ! 6 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 11 !
! ! 4 ! 5 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 19 !
! ! 4 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 17 !
! ! 4 ! 3 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 18 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 21 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 15 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading ! DMC!25/1/101/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/101/10! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 !1/4! 21 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting capt! DMC!25/1/222/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine ! DMC!25/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/114/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS !04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS !04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position ! FCDC!6C/1/362/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/326/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 25 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 25 !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 26 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/272/10! 1 !1/4! 26 !
! ! 3 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/276/01! 1 !1/4! 22 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/276/10! 1 !1/4! 23 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/274/01! 1 !1/4! 11 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/274/10! 1 !1/4! 12 !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order ! FGC I01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC I01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position ! FCDCI6C/1/364/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDCI6C/2/364/10! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 23 !
! ! ! ! ! ! DMC I25/2/272/10! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 27 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 27 !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 12 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 13 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/2/042/01! 1 !1/4! 14 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position ! FCDC!6C/1/365/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/365/10! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC !25/2/272/10! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word ! FWC !26/1/126/00! 1 !1/4! 14 !
! ! ! ! ! ! FFWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/271/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/271/10! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF ! SDAC!29/1/002/11! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/350/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/350/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC discrete status word ! FWC !26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC !26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS word #2 ! FCDC!6C/1/041/01! 1 !1/4! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 272/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 272/00 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude ! IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude ! IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position longitude! IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 ! FWC !26/1/073/01! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/01! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 ! FWC !26/1/073/10! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle ! ECU/!7C/1/ ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle ! ECU/!7C/1/ ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date ! FDIU!17/1/260/00! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date ! FDIU!17/1/260/00! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases ! FDIU!26/1/126/01! 1 !1/4! 14 !
! ! ! ! ! ! FDIU!26/2/260/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: status word ! DMC !25/1/301/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC !25/2/301/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universal time ! FDIU!17/1/125/00! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight ! FMC !02/1/075/00! 1 !1/4! 28 !
! ! ! ! ! (10kgs) ! FMC !02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/1/346/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: status word ! SDAC!29/1/046/01! 1 !1/4! 26 !
! ! ! ! ! ! SDAC!29/2/046/01! ! ! !
! ! 1-4! 1 ! 1 ! FWC bus: status word ! FWC !26/1/017/11! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC !26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine ! ECU/!7C/1/345/01! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!25 ! ! ! ! T B D ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 ! EVMU!3D/1/135/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 ! EVMU!3D/1/136/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th ! FGC !01/1/235/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th ! FGC !01/1/235/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th ! FGC !01/1/236/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th ! FGC !01/1/236/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection ! FWC !26/1/014/10! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection ! FWC !26/1/014/01! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert ! FWC !26/1/016/10! 1 ! 1 ! 18 !
! ! 1-4! 9 ! 1 ! GPWS modes ON ! FWC !26/1/016/01! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC !26/2/016/01! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) ! DMC !25/1/274/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 7 ! 1 ! MIDDLE marker ! DMC !25/1/274/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker ! DMC !25/1/274/01! 1 ! 1 ! 13 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting ! SDAC!29/1/002/11! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/11! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading ! IRS !04/1/320/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS !04/2/320/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU status word ! FCU !A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed ! ADC !06/1/206/01! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) ! ADC !06/2/206/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Shown angle of ! ADC !06/1/221/01! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Shown angle of ! ADC !06/1/221/01! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 3 ! Derate T/Off Limit Mode ! EEC!7C/1/270/01! 1 ! 1 ! 23 !
! ! ! ! ! selected ! EEC!7C/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left ! FCDC!6C/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left ! FCDC!6C/1/314/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off ! BSCU!6E/1/026/01! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault ! BSCU!6E/1/026/01! 1 ! 1 ! 20 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! position ! FCDC!6C/1/305/10! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on ! BSCU!6E/1/027/01! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on ! BSCU!6E/1/027/01! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on ! BSCU!6E/1/027/01! 1 ! 1 ! 22 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! !6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 2 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 18 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!51 ! 1.3! 12 ! 6 ! N1 command engine #1 ! ECU!7C/1/341/01! 1 !1/2! 27 !
! ! 2.4! 12 ! 6 ! N1 command engine #2 ! ECU!7C/2/341/10! 1 !1/2! 27 !
! ! 1 ! 6 ! 6 ! N1 target feedback engine ! ECU!7C/1/341/01! 1 !1/4! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 14 !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 13 !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 15 !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 11 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 12 !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. ! DMC!25/1/230/00! 1 !1/4! 29 !
! ! ! ! ! END DATA ! DMC!25/2/230/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/2/344/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 22 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 28 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/2/244/10! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED ! IRS!04/1/315/01! 1 !1/4! 28 !
! ! ! ! ! ! IRS!04/2/315/10! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 16 !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 14 !
! ! 2 ! 12 ! 12 ! Altitude baro setting capt! DMC!25/1/222/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
! ! 3 ! 12 ! 9 ! Decision height ! DMC!25/1/370/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC!25/2/370/10! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 22 !
! ! 4 ! 8 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 26 !
! ! 4 ! 7 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 20 !
! ! 4 ! 6 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 11 !
! ! 4 ! 5 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 19 !
! ! 4 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 17 !
! ! 4 ! 3 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 18 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 21 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 15 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading ! DMC!25/1/101/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/101/10! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 !1/4! 21 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting capt! DMC!25/1/222/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine ! DMC!25/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/114/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS !04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS !04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position ! FCDC!6C/1/362/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/326/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 25 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 25 !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 26 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/272/10! 1 !1/4! 26 !
! ! 3 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/276/01! 1 !1/4! 22 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/276/10! 1 !1/4! 23 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/274/01! 1 !1/4! 11 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/274/10! 1 !1/4! 12 !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order ! FGC I01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC I01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position ! FCDCI6C/1/364/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDCI6C/2/364/10! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 23 !
! ! ! ! ! ! DMC I25/2/272/10! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 27 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 27 !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 12 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 13 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/2/042/01! 1 !1/4! 14 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position ! FCDC!6C/1/365/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/365/10! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC !25/2/272/10! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word ! FWC !26/1/126/00! 1 !1/4! 14 !
! ! ! ! ! ! FFWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/271/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/271/10! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF ! SDAC!29/1/002/11! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/350/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/350/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC discrete status word ! FWC !26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC !26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS word #2 ! FCDC!6C/1/041/01! 1 !1/4! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 272/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 272/00 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude ! IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude ! IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position longitude! IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 ! FWC !26/1/073/01! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/01! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 ! FWC !26/1/073/10! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle ! ECU/!7C/1/ ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle ! ECU/!7C/1/ ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date ! FDIU!17/1/260/00! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date ! FDIU!17/1/260/00! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases ! FDIU!26/1/126/01! 1 !1/4! 14 !
! ! ! ! ! ! FDIU!26/2/260/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: status word ! DMC !25/1/301/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC !25/2/301/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universal time ! FDIU!17/1/125/00! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight ! FMC !02/1/075/00! 1 !1/4! 28 !
! ! ! ! ! (10kgs) ! FMC !02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/1/346/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: status word ! SDAC!29/1/046/01! 1 !1/4! 26 !
! ! ! ! ! ! SDAC!29/2/046/01! ! ! !
! ! 1-4! 1 ! 1 ! FWC bus: status word ! FWC !26/1/017/11! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC !26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine ! ECU/!7C/1/345/01! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!25 ! ! ! ! T B D ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 ! EVMU!3D/1/135/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 ! EVMU!3D/1/136/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th ! FGC !01/1/235/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th ! FGC !01/1/235/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th ! FGC !01/1/236/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th ! FGC !01/1/236/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection ! FWC !26/1/014/10! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection ! FWC !26/1/014/01! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert ! FWC !26/1/016/10! 1 ! 1 ! 18 !
! ! 1-4! 9 ! 1 ! GPWS modes ON ! FWC !26/1/016/01! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC !26/2/016/01! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) ! DMC !25/1/274/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 7 ! 1 ! MIDDLE marker ! DMC !25/1/274/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker ! DMC !25/1/274/01! 1 ! 1 ! 13 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting ! SDAC!29/1/002/11! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/11! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading ! IRS !04/1/320/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS !04/2/320/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU status word ! FCU !A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed ! ADC !06/1/206/01! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) ! ADC !06/2/206/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Indicated angle of ! ADC !06/1/221/01! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Indicated angle of ! ADC !06/1/221/01! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 3 ! Derate T/Off Limit Mode ! EEC!7C/1/270/01! 1 ! 1 ! 13 !
! ! ! ! ! selected ! EEC!7C/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left ! FCDC!6C/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left ! FCDC!6C/1/314/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off ! BSCU!6E/1/026/01! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault ! BSCU!6E/1/026/01! 1 ! 1 ! 20 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! position ! FCDC!6C/1/305/10! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on ! BSCU!6E/1/027/01! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on ! BSCU!6E/1/027/01! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on ! BSCU!6E/1/027/01! 1 ! 1 ! 22 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! !6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 2 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 18 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!51 ! 1.3! 12 ! 6 ! EPR command engine #1 ! EEC!7C/1/341/01! 1 !1/2! 27 !
! ! 2.4! 12 ! 6 ! EPR command engine #2 ! EEC!7C/2/341/10! 1 !1/2! 27 !
! ! 1 ! 6 ! 6 ! EPR target (echo) ! EEC!7C/1/341/01! 1 !1/4! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 14 !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 13 !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 15 !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 11 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 12 !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. ! DMC!25/1/230/00! 1 !1/4! 29 !
! ! ! ! ! END DATA ! DMC!25/2/230/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/2/344/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 22 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 28 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/2/244/10! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED ! IRS!04/1/315/01! 1 !1/4! 28 !
! ! ! ! ! ! IRS!04/2/315/10! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 16 !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 14 !
! ! 2 ! 12 ! 12 ! Altitude baro setting capt! DMC!25/1/222/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
! ! 3 ! 12 ! 9 ! Decision height ! DMC!25/1/370/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC!25/2/370/10! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 22 !
! ! 4 ! 8 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 26 !
! ! 4 ! 7 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 20 !
! ! 4 ! 6 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 11 !
! ! 4 ! 5 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 19 !
! ! 4 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 17 !
! ! 4 ! 3 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 18 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 21 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 15 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading ! DMC!25/1/101/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/101/10! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 !1/4! 21 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting capt! DMC!25/1/222/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine ! DMC!25/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/114/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position !FCDC !6C/1/362/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/362/10 ! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/1/272/01 ! 1 !1/4! 25 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: discrete status !DMC !25/2/272/10 ! 1 !1/4! 25 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/1/272/01 ! 1 !1/4! 26 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 2 ! 1 ! 1 ! DMC bus: status word !DMC !25/2/272/10 ! 1 !1/4! 26 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/1/276/01 ! 1 !1/4! 22 !
! ! ! ! ! word (label 276) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status !DMC !25/2/276/10 ! 1 !1/4! 23 !
! ! ! ! ! word (label 276) ! ! ! ! ! !
! ! 4 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/1/274/01 ! 1 !1/4! 11 !
! ! ! ! ! word (label 274) ! ! ! ! ! !
! ! 4 ! 1 ! 1 ! DMC bus: discrete status !DMC !25/2/274/10 ! 1 !1/4! 12 !
! ! ! ! ! word (label 274) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position !FCDC !6C/1/364/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/364/10 ! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: discrete status !DMC !25/1/272/01 ! 1 !1/4! 23 !
! ! ! ! ! word (label 272) !DMC !25/2/272/10 ! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/1/272/01 ! 1 !1/4! 27 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 2 ! 1 ! 1 ! DMC bus: discrete status !DMC !25/2/272/10 ! 1 !1/4! 27 !
! ! ! ! ! word (label 272) ! ! ! ! ! !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/042/01 ! 1 !1/4! 12 !
! ! ! ! ! word #3 !FCDC !6C/2/042/10 ! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS status !FCDC !6C/1/042/01 ! 1 !1/4! 13 !
! ! ! ! ! word #3 !FCDC !6C/2/042/10 ! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS status !FCDC !6C/2/042/01 ! 1 !1/4! 14 !
! ! ! ! ! word #3 !FCDC !6C/2/042/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position !FCDC !6C/1/365/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/365/10 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/272/01 !1 !1/4! 24 !
! ! ! ! ! word (label 272) !DMC !25/2/272/10 ! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word !FWC !26/1/126/00 ! 1 !1/4! 14 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/143/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 23 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 !1/4! 25 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF!SDAC !29/1/002/11 ! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/350/01 ! 1 !1/4! 25 !
! ! ! ! ! word (label 350) !DMC !25/2/350/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label=015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/041/01 ! 1 !1/4! 20 !
! ! ! ! ! word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word !FCU !A1/1A/272/00! 1 ! 1 ! 23 !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word !FCU !A1/1B/272/00! ! ! !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude!IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! !IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude!IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! !IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position !IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! longitude !IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 !FWC !26/1/073/01 ! 1 !1/4! 27 !
! ! ! ! ! !FWC !26/2/073/01 ! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 !FWC !26/1/073/10 ! 1 !1/4! 27 !
! ! ! ! ! !FWC !26/2/073/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle !EIU !7B/1/133/xx ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle !EIU !7B/1/133/xx ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date !FDIU !17/1/260/00 ! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date !FDIU !17/1/260/00 ! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases !FWC !26/1/126/01 ! 1 !1/4! 14 !
! ! ! ! ! !FWC !26/2/126/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: Discrete status !DMC !25/1/301/01 ! 1 ! 1 ! 28 !
! ! ! ! ! word (label 301) !DMC !25/2/301/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universial time !FDIU !17/1/125/00 ! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight !FMC !02/1/075/00 ! 1 !1/4! 28 !
! ! ! ! ! (10kgs) (switched !FMC !02/2/075/00 ! ! ! !
! ! ! ! ! parameter) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor !EIU !7B/1/331/xx ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: Discrete status!SDAC !29/1/046/01 ! 1 ! 1 ! 26 !
! ! ! ! ! word (label 046) !SDAC !29/2/046/01 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/11 ! 1 ! 1 ! 29 !
! ! ! ! ! (Label=017 SDI=11) !FWC !26/2/017/11 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine !EIU !7C/1/345/01 ! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!25 ! ! ! ! SPARE ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 !EIU !7B/1/135/XX ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 !EIU !7B/1/136/XX ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd !FGC !01/1/233/00 ! 1 !1/4! 22 !
! ! ! ! ! character) !FGC !01/2/233/00 ! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd !FGC !01/1/233/00 ! 2 !1/4! 29 !
! ! ! ! ! character) !FGC !01/2/233/00 ! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th !FGC !01/1/234/00 ! 1 !1/4! 22 !
! ! ! ! ! character) !FGC !01/2/234/00 ! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th !FGC !01/1/234/00 ! 2 !1/4! 29 !
! ! ! ! ! character) !FGC !01/2/234/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th !FGC !01/1/235/00 ! 1 !1/4! 22 !
! ! ! ! ! character) !FGC !01/2/235/00 ! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th !FGC !01/1/235/00 ! 2 !1/4! 29 !
! ! ! ! ! character) !FGC !01/2/235/00 ! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th !FGC !01/1/236/00 ! 1 !1/4! 22 !
! ! ! ! ! character) !FGC !01/2/236/00 ! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th !FGC !01/1/236/00 ! 2 !1/4! 29 !
! ! ! ! ! character) !FGC !01/2/236/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection !FWC !26/1/014/10 ! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection !FWC !26/1/014/01 ! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert !FWC !26/1/016/10 ! 1 ! 1 ! 18 !
! ! ! ! ! !FWC !26/2/016/10 ! ! ! !
! ! 1-4! 9 ! 1 ! GPWS modes ON !FWC !26/1/016/01 ! 1 ! 1 ! 18 !
! ! ! ! ! !FWC !26/2/016/01 ! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) !DMC !25/1/274/01 ! 1 ! 1 ! 15 !
! ! ! ! ! !DMC !25/2/274/10 ! ! ! !
! ! 1-4! 6 ! 1 ! MIDDLE marker !DMC !25/1/274/01 ! 1 ! 1 ! 14 !
! ! ! ! ! !DMC !25/2/274/10 ! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker !DMC !25/1/274/01 ! 1 ! 1 ! 13 !
! ! ! ! ! !DMC !25/2/274/10 ! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting !SDAC !29/1/002/10 ! 1 ! 1 ! 28 !
! ! ! ! ! !SDAC !29/2/002/10 ! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting !SDAC !29/1/002/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !SDAC !29/2/002/01 ! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting !SDAC !29/1/002/11 ! 1 ! 1 ! 29 !
! ! ! ! ! !SDAC !29/2/002/11 ! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting !SDAC !29/1/002/10 ! 1 ! 1 ! 29 !
! ! ! ! ! !SDAC !29/2/002/10 ! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting !SDAC !29/1/002/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !SDAC !29/2/002/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading !IRS !04/1/320/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/320/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCU Discrete status word !FCU !A1/1A/273/00! 1 ! 1 ! 12 !
! ! ! ! ! (Label=273 SDI=00) !FCU !A1/1B/273/00! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed !ADC !06/1/206/01 ! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) !ADC !06/2/206/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Indicated angle of !ADC !06/1/221/01 ! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! ! ! ! ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Indicated angle of !ADC !06/1/221/01 ! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01 ! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10 ! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01 ! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10 ! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01 ! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 3 ! 3 ! Derate Takeoff !EIU !7C/1/270/xx ! 1 ! 1 ! 13 !
! ! ! ! ! !EIU !7C/2/270/xx ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left !FCDC !6C/1/314/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/314/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left !FCDC !6C/1/314/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/314/10 ! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off !BSCU !6E/1/026/01 ! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault !BSCU !6E/1/026/01 ! 1 ! 1 ! 20 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command !FCDC !6C/1/305/01 ! 1 ! 2 ! 29 !
! ! ! ! ! position !FCDC !6C/2/305/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command !FCDC !6C/1/305/01 ! 2 ! 2 ! 25 !
! ! ! ! ! position !FCDC !6C/1/305/10 ! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on !BSCU !6E/1/027/01 ! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on !BSCU !6E/1/027/01 ! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on !BSCU !6E/1/027/01 ! 1 ! 1 ! 22 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command !FCDC !6C/1/306/01 ! 1 ! 2 ! 29 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command !FCDC !6C/1/306/01 ! 2 ! 2 ! 25 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 3 ! 2 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 18 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 13 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!51 ! 1.3! 12 ! 6 ! N1 command engine #1 !ECU/ !7B/1/341/xx ! 1 !1/2! 27 !
! ! ! ! ! !EEC ! ! ! ! !
! ! 2.4! 12 ! 6 ! N1 command engine #2 !ECU/ !7B/2/341/xx ! 1 !1/2! 27 !
! ! ! ! ! !EEC ! ! ! ! !
! ! 1 ! 6 ! 6 ! N1 target feedback !ECU/ !7B/1/343/xx ! 1 !1/4! 27 !
! ! ! ! ! engine #1 !EEC ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status !DMC !25/2/273/01 ! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status !DMC !25/2/273/10 ! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!--------------------------!--- !------------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: Discrete status !DMC !25/1/273/01 ! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: Discrete status !DMC !25/1/273/01 ! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 1 ! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/273/01 ! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/273/01 ! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/273/01 ! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. !DMC !25/1/230/00 ! 1 !1/4! 29 !
! ! ! ! ! END DATA !DMC !25/2/230/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor !EIU !7C/2/344/xx ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 22 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 28 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate !EIU !7B/2/244/xx ! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! ! ! ! ! !
!---!----!----!----!--------------------------!---- !----------- !---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED !IRS !04/1/315/01 ! 1 !1/4! 28 !
! ! ! ! ! !IRS !04/2/315/10 ! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 16 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 14 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Altitude baro setting !DMC !25/1/222/01 ! 1 !1/4! 26 !
! ! ! ! ! capt !DMC !25/2/222/10 ! ! ! !
! ! 3 ! 12 ! 9 ! Decision height !DMC !25/1/370/01 ! 1 !1/4! 24 !
! ! ! ! ! !DMC !25/2/370/10 ! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 22 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 8 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 26 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 7 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 20 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 6 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 11 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 5 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 19 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 4 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 17 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 3 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 18 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 2 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 21 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
! ! 4 ! 1 ! 1 ! DMC bus: Discrete status !DMC !25/2/275/10 ! 1 !1/4! 15 !
! ! ! ! ! word (label 275) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading !DMC !25/1/101/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/101/10 ! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: Discrete status !DMC !25/1/276/01 ! 1 !1/4! 21 !
! ! ! ! ! Word (label 276) !DMC !25/2/276/10 ! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting !DMC !25/1/222/01 ! 2 !1/4! 27 !
! ! ! ! ! capt !DMC !25/2/222/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine !DMC !25/1/114/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/114/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
+---+----+----+----+--------------------------+-----+-----------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS !04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS !04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position ! FCDC!6C/1/362/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/326/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 25 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 25 !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 26 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/272/10! 1 !1/4! 26 !
! ! 3 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/276/01! 1 !1/4! 22 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/276/10! 1 !1/4! 23 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/274/01! 1 !1/4! 11 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/274/10! 1 !1/4! 12 !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order ! FGC I01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC I01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position ! FCDCI6C/1/364/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDCI6C/2/364/10! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 23 !
! ! ! ! ! ! DMC I25/2/272/10! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 27 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 27 !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 12 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 13 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/2/042/01! 1 !1/4! 14 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position ! FCDC!6C/1/365/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/365/10! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC !25/2/272/10! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word ! FWC !26/1/126/00! 1 !1/4! 14 !
! ! ! ! ! ! FFWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/271/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/271/10! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF ! SDAC!29/1/002/11! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/350/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/350/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC discrete status word ! FWC !26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC !26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS word #2 ! FCDC!6C/1/041/01! 1 !1/4! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 272/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 272/00 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude ! IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude ! IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position longitude! IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 ! FWC !26/1/073/01! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/01! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 ! FWC !26/1/073/10! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle ! ECU/!7C/1/ ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle ! ECU/!7C/1/ ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date ! FDIU!17/1/260/00! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date ! FDIU!17/1/260/00! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases ! FDIU!26/1/126/01! 1 !1/4! 14 !
! ! ! ! ! ! FDIU!26/2/260/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: status word ! DMC !25/1/301/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC !25/2/301/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universal time ! FDIU!17/1/125/00! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight ! FMC !02/1/075/00! 1 !1/4! 28 !
! ! ! ! ! (10kgs) ! FMC !02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/1/346/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: status word ! SDAC!29/1/046/01! 1 !1/4! 26 !
! ! ! ! ! ! SDAC!29/2/046/01! ! ! !
! ! 1-4! 1 ! 1 ! FWC bus: status word ! FWC !26/1/017/11! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC !26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine ! ECU/!7C/1/345/01! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!25 ! ! ! ! Spare ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 ! EVMU!3D/1/135/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 ! EVMU!3D/1/136/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th ! FGC !01/1/235/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th ! FGC !01/1/235/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th ! FGC !01/1/236/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th ! FGC !01/1/236/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection ! FWC !26/1/014/10! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection ! FWC !26/1/014/01! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert ! FWC !26/1/016/10! 1 ! 1 ! 18 !
! ! 1-4! 9 ! 1 ! GPWS modes ON ! FWC !26/1/016/01! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC !26/2/016/01! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) ! DMC !25/1/274/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 7 ! 1 ! MIDDLE marker ! DMC !25/1/274/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker ! DMC !25/1/274/01! 1 ! 1 ! 13 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting ! SDAC!29/1/002/11! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/11! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading ! IRS !04/1/320/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS !04/2/320/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU status word ! FCU !A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed ! ADC !06/1/206/01! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) ! ADC !06/2/206/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Indicated angle of ! ADC !06/1/221/01! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Indicated angle of ! ADC !06/1/221/01! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 3 ! Derate T/Off Limit Mode ! EEC!7C/1/270/01! 1 ! 1 ! 23 !
! ! ! ! ! selected ! EEC!7C/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left ! FCDC!6C/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left ! FCDC!6C/1/314/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off ! BSCU!6E/1/026/01! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault ! BSCU!6E/1/026/01! 1 ! 1 ! 20 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! position ! FCDC!6C/1/305/10! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on ! BSCU!6E/1/027/01! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on ! BSCU!6E/1/027/01! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on ! BSCU!6E/1/027/01! 1 ! 1 ! 22 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! !6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 2 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 18 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!51 ! 1.3! 12 ! 6 ! N1 command engine #1 ! ECU!7C/1/341/01! 1 !1/2! 27 !
! ! 2.4! 12 ! 6 ! N1 command engine #2 ! ECU!7C/2/341/10! 1 !1/2! 27 !
! ! 1 ! 6 ! 6 ! N1 target feedback engine ! ECU!7C/1/341/01! 1 !1/4! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 14 !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 13 !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 15 !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 11 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 12 !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. ! DMC!25/1/230/00! 1 !1/4! 29 !
! ! ! ! ! END DATA ! DMC!25/2/230/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/2/344/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 22 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 28 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/2/244/10! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED ! IRS!04/1/315/01! 1 !1/4! 28 !
! ! ! ! ! ! IRS!04/2/315/10! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 16 !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 14 !
! ! 2 ! 12 ! 12 ! Altitude baro setting capt! DMC!25/1/222/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
! ! 3 ! 12 ! 9 ! Decision height ! DMC!25/1/370/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC!25/2/370/10! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 22 !
! ! 4 ! 8 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 26 !
! ! 4 ! 7 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 20 !
! ! 4 ! 6 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 11 !
! ! 4 ! 5 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 19 !
! ! 4 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 17 !
! ! 4 ! 3 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 18 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 21 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 15 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading ! DMC!25/1/101/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/101/10! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 !1/4! 21 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting capt! DMC!25/1/222/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine ! DMC!25/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/114/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)
DAR Frame Assignment (Word 1-64) - FDIMU P/N ED48A200WR, IAE engines
+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 1 ! 1 ! 12 ! 12 ! Synchro word 1 ! ! ! ! ! !
! ! ! ! ! (MSB 001001000111 LSB) ! ! ! ! ! !
! ! 2 ! 12 ! 12 ! Syschro word 2 ! ! ! ! ! !
! ! ! ! ! (MSB 010110111000 LSB) ! ! ! ! ! !
! ! 3 ! 12 ! 12 ! Synchro word 3 ! ! ! ! ! !
! ! ! ! ! (MSB 101001000111 LSB) ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Synchro Word 4 ! ! ! ! ! !
! ! ! ! ! (MSB 110110111000 LSB) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 2 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS !04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS !04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 3 ! 1-4! 12 ! 10 ! LH spoiler #2 position ! FCDC!6C/1/362/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/326/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 25 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 25 !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 26 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/272/10! 1 !1/4! 26 !
! ! 3 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/276/01! 1 !1/4! 22 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/276/10! 1 !1/4! 23 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/274/01! 1 !1/4! 11 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC I25/2/274/10! 1 !1/4! 12 !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 4 ! 1-4! 12 ! 12 ! FD roll order ! FGC I01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC I01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----I-----------!---!---!----!
! 5 ! 1-4! 12 ! 10 ! LH spoiler #4 position ! FCDCI6C/1/364/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDCI6C/2/364/10! ! ! !
! ! 1 ! 2 ! 2 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 23 !
! ! ! ! ! ! DMC I25/2/272/10! ! ! !
! ! 2 ! 2 ! 1 ! DMC bus: status word ! DMC I25/1/272/01! 1 !1/4! 27 !
! ! 2 ! 1 ! 1 ! DMC bus: status word ! DMC !25/2/272/10! 1 !1/4! 27 !
! ! 3 ! 2 ! 2 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 12 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/1/042/01! 1 !1/4! 13 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: EFCS word #3 ! FCDC!6C/2/042/01! 1 !1/4! 14 !
! ! ! ! ! ! FCDC!6C/2/042/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 6 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 7 ! 1-4! 12 ! 10 ! LH spoiler #5 position ! FCDC!6C/1/365/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/365/10! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/272/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC !25/2/272/10! ! ! !
! ! 3 ! 2 ! 2 ! FWC discrete status word ! FWC !26/1/126/00! 1 !1/4! 14 !
! ! ! ! ! ! FFWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 8 ! 1-4! 12 ! 12 ! FD pitch order ! FGC !01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC !01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
! 9 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!11 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00 ! ! ! !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/271/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/271/10! ! ! !
! ! 2 ! 1 ! 1 ! APU master switch P/B OFF ! SDAC!29/1/002/11! 1 !1/4! 16 !
! ! 3 ! 1 ! 1 ! DMC bus: status word ! DMC !25/1/350/01! 1 !1/4! 25 !
! ! ! ! ! ! DMC !25/2/350/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!12 ! 1-4! 12 ! 10 ! FWC discrete status word ! FWC !26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC !26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS word #2 ! FCDC!6C/1/041/01! 1 !1/4! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!13 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! 1 ! 1 ! 23 !
! ! 1-4! 2 ! 1 ! FCU discrete status word ! FCU !A1/1A/ ! 1 ! 1 ! 23 !
! ! ! ! ! ! ! 272/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FCU discrete status word ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! ! 272/00 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!15 ! 1 ! 8 ! 1 ! Present position latitude ! IRS !04/1/310/ ! 1 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 1 ! 7 ! 7 ! Present position latitude ! IRS !04/1/310/ ! 2 !1/4! 27 !
! ! ! ! ! ! IRS !04/2/310/ ! ! ! !
! ! 2 ! 8 ! 8 ! Present position longitude! IRS !04/1/311/ ! 2 !1/4! 29 !
! ! ! ! ! ! IRS !04/2/311/ ! ! ! !
! ! 3 ! 8 ! 8 ! OIL quantity engine #1 ! FWC !26/1/073/01! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/01! ! ! !
! ! 4 ! 8 ! 8 ! OIL quantity engine #2 ! FWC !26/1/073/10! 1 !1/4! 27 !
! ! ! ! ! ! FWC !26/2/073/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!17 ! 1-4! 12 ! 1 ! Throttle resolver angle ! ECU/!7C/1/ ! 1 ! 1 ! 29 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver angle ! ECU/!7C/1/ ! 2 ! 1 ! 27 !
! ! ! ! ! engine #1 ! EEC ! 133/01 ! ! ! !
! ! 1 ! 6 ! 6 ! GMT date ! FDIU!17/1/260/00! 1 !1/4! 29 !
! ! 2 ! 5 ! 5 ! GMT date ! FDIU!17/1/260/00! 2 !1/4! 23 !
! ! 3 ! 4 ! 4 ! Flight phases ! FDIU!26/1/126/01! 1 !1/4! 14 !
! ! ! ! ! ! FDIU!26/2/260/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!18 ! 1-4! 12 ! 11 ! DMC bus: status word ! DMC !25/1/301/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC !25/2/301/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!19 ! 1 ! 12 ! 7 ! UTC (Universial time ! FDIU!17/1/125/00! 1 !1/4! 29 !
! ! ! ! ! coordinated BCD) ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! Actual gross weight ! FMC !02/1/075/00! 1 !1/4! 28 !
! ! ! ! ! (10kgs) ! FMC !02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!21 ! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/1/346/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! SDAC bus: status word ! SDAC!29/1/046/01! 1 !1/4! 26 !
! ! ! ! ! ! SDAC!29/2/046/01! ! ! !
! ! 1-4! 1 ! 1 ! FWC bus: status word ! FWC !26/1/017/11! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC !26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!23 ! 1-4! 12 ! 10 ! EGT LPT exit temp engine ! ECU/!7C/1/345/01! 1 ! 1 ! 27 !
! ! ! ! ! #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!25 ! 1-4! 12 ! 10 ! EPR Actual engine #1 ! EEC !7C/1/340/01! 1 ! 1 ! 27 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!27 ! 1-4! 12 ! 6 ! N1 vibration eng #1 ! EVMU!3D/1/135/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #1 ! EVMU!3D/1/136/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!29 ! 1 ! 12 ! 12 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (1st & 2nd ! FGC !01/1/233/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/233/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (3rd & 4th ! FGC !01/1/234/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/234/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!31 ! 1 ! 12 ! 12 ! Flight number (5th & 6th ! FGC !01/1/235/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 2 ! 7 ! 7 ! Flight number (5th & 6th ! FGC !01/1/235/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/235/00! ! ! !
! ! 3 ! 12 ! 12 ! Flight number (7th & 8th ! FGC !01/1/236/00! 1 !1/4! 22 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
! ! 4 ! 7 ! 7 ! Flight number (7th & 8th ! FGC !01/1/236/00! 2 !1/4! 29 !
! ! ! ! ! character) ! FGC !01/2/236/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!33 ! 1-4! 12 ! 1 ! Windshear detection ! FWC !26/1/014/10! 1 ! 1 ! 29 !
! ! ! ! ! system #2 ! ! ! ! ! !
! ! 1-4! 11 ! 1 ! Windshear detection ! FWC !26/1/014/01! 1 ! 1 ! 29 !
! ! ! ! ! system #1 ! ! ! ! ! !
! ! 1-4! 10 ! 1 ! GPWS G/S visual alert ! FWC !26/1/016/10! 1 ! 1 ! 18 !
! ! 1-4! 9 ! 1 ! GPWS modes ON ! FWC !26/1/016/01! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC !26/2/016/01! ! ! !
! ! 1-4! 8 ! 1 ! INNER marker (airways) ! DMC !25/1/274/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 7 ! 1 ! MIDDLE marker ! DMC !25/1/274/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 6 ! 1 ! OUTER marker ! DMC !25/1/274/01! 1 ! 1 ! 13 !
! ! ! ! ! ! DMC !25/2/274/10! ! ! !
! ! 1-4! 5 ! 1 ! HF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 4 ! 1 ! HF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 28 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
! ! 1-4! 3 ! 1 ! VHF3 emitting ! SDAC!29/1/002/11! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/11! ! ! !
! ! 1-4! 2 ! 1 ! VHF2 emitting ! SDAC!29/1/002/10! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 1-4! 1 ! 1 ! VHF1 emitting ! SDAC!29/1/002/01! 1 ! 1 ! 29 !
! ! ! ! ! ! SDAC!29/2/002/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!34 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!35 ! 1-4! 12 ! 10 ! Magnetic heading ! IRS !04/1/320/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS !04/2/320/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU status word ! FCU !A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU !A1/1B/ ! ! ! !
! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!36 ! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!37 ! 1-4! 12 ! 12 ! Computed air speed ! ADC !06/1/206/01! 1 ! 1 ! 27 !
! ! ! ! ! (switched parameter) ! ADC !06/2/206/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!38 ! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!39 ! 1-4! 12 ! 1 ! Indicated angle of ! ADC !06/1/221/01! 1 ! 1 ! 29 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 11 ! 8 ! Indicated angle of ! ADC !06/1/221/01! 2 ! 1 ! 27 !
! ! ! ! ! attack system #1 ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! Nose Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 12 !
! ! ! ! ! compressed (ON) !LGCIU!6D/1/021/10! ! ! !
! ! 1-4! 2 ! 1 ! RH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 14 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
! ! 1-4! 1 ! 1 ! LH Landing gear !LGCIU!6D/1/021/01! 1 ! 1 ! 13 !
! ! ! ! ! compressed (ON) !LGCIU!6D/2/021/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!40 ! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!41 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!42 ! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!43 ! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 3 ! Derate T/Off Limit Mode ! EEC!7C/1/270/01! 1 ! 1 ! 13 !
! ! ! ! ! selected ! EEC!7C/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!45 ! 1-4! 12 ! 1 ! Elevator position left ! FCDC!6C/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position left ! FCDC!6C/1/314/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/314/10! ! ! !
! ! 1-4! 2 ! 1 ! Auto brake off ! BSCU!6E/1/026/01! 1 ! 1 ! 19 !
! ! 1-4! 1 ! 1 ! Auto brake fault ! BSCU!6E/1/026/01! 1 ! 1 ! 20 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!47 ! 1-4! 12 ! 1 ! Capt pitch command ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch command ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! position ! FCDC!6C/1/305/10! ! ! !
! ! 1-4! 3 ! 1 ! Deceleration low on ! BSCU!6E/1/027/01! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! Deceleration med on ! BSCU!6E/1/027/01! 1 ! 1 ! 21 !
! ! 1-4! 1 ! 1 ! Deceleration max on ! BSCU!6E/1/027/01! 1 ! 1 ! 22 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!49 ! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! !6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 2 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 18 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!51 ! 1.3! 12 ! 6 ! EPR command engine #1 ! EEC!7C/1/341/01! 1 !1/2! 27 !
! ! 2.4! 12 ! 6 ! EPR command engine #2 ! EEC!7C/2/341/10! 1 !1/2! 27 !
! ! 1 ! 6 ! 6 ! EPR target (echo) ! EEC!7C/1/341/01! 1 !1/4! 27 !
! ! ! ! ! engine #1 ! ! ! ! ! !
! ! 2 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 5 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 14 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 4 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 13 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 3 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 15 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 2 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 11 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 3 ! 1 ! 1 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 12 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
! ! 4 ! 5 ! 5 ! DMC bus: discrete status ! DMC!25/2/273/10! 1 !1/4! 20 !
! ! ! ! ! word (label 273) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!53 ! 1 ! 5 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 14 !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 13 !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 15 !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 11 !
! ! 1 ! 1 ! 1 ! DMC bus: status word ! DMC!25/1/273/01! 1 !1/4! 12 !
! ! 2 ! 12 ! 12 ! NAV. DATA BASE EFFECT. ! DMC!25/1/230/00! 1 !1/4! 29 !
! ! ! ! ! END DATA ! DMC!25/2/230/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!55 ! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/2/344/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 22 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU status word ! FCU!A1/1A/ ! 1 ! 1 ! 28 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!57 ! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/2/244/10! 1 ! 1 ! 27 !
! ! ! ! ! engine #2 (in kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!59 ! 1 ! 12 ! 8 ! WIND SPEED ! IRS!04/1/315/01! 1 !1/4! 28 !
! ! ! ! ! ! IRS!04/2/315/10! ! ! !
! ! 1 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 16 !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 14 !
! ! 2 ! 12 ! 12 ! Altitude baro setting capt! DMC!25/1/222/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
! ! 3 ! 12 ! 9 ! Decision height ! DMC!25/1/370/01! 1 !1/4! 24 !
! ! ! ! ! ! DMC!25/2/370/10! ! ! !
! ! 4 ! 9 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 22 !
! ! 4 ! 8 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 26 !
! ! 4 ! 7 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 20 !
! ! 4 ! 6 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 11 !
! ! 4 ! 5 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 19 !
! ! 4 ! 4 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 17 !
! ! 4 ! 3 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 18 !
! ! 4 ! 2 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 21 !
! ! 4 ! 1 ! 1 ! DMC bus: status word ! DMC!25/2/275/10! 1 !1/4! 15 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!61 ! 1-4! 12 ! 9 ! Selected heading ! DMC!25/1/101/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/101/10! ! ! !
! ! 2 ! 3 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 !1/4! 21 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting capt! DMC!25/1/222/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/222/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!63 ! 1-4! 12 ! 9 ! Selected track fine ! DMC!25/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/114/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

G. DAR Frame Assignment (Word 65-128)
+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!65 ! 1-4! 12 ! 12 ! Stall speed ! FAC!0A/1/246/00! 1 ! 2 ! 28 !
! ! ! ! ! ! FAC!0A/2/246/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!66 ! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS!04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!67 ! 1-4! 12 ! 6 ! Right brake pedal angle ! BSCU!6E/1/330/01! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Left brake pedal angle ! BSCU!6E/1/331/01! 1 ! 1 ! 28 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!68 ! 1-4! 12 ! 12 ! FD Roll Order ! FGC!01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!69 ! 1-4! 12 ! 1 ! Stabilizer position #1 ! FCDC!6C/1/315/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/315/10! ! ! !
! ! 1-4! 11 ! 8 ! Stabilizer position #1 ! FCDC!6C/1/315/01! 2 ! 1 ! 25 !
! ! ! ! ! ! FCDC!6C/2/315/10! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 20 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 21 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 19 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!70 ! 1-4! 12 ! 12 ! FD Pitch Order ! FGC!01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!71 ! 1-4! 12 ! 8 ! SLAT actual ! SFCC!1B/1/127/01! 1 ! 1 ! 29 !
! ! ! ! ! position switched ! SFCC!1B/2/127/10! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 16 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 17 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 ! 1 ! 18 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!72 ! 1-4! 12 ! 12 ! FD Pitch Order ! FGC!01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!73 ! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!75 ! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!76 ! 1-4! 12 ! 10 ! FWC Discrete status word ! FWC!26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC!26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: status word ! FCDC!6C/1/041/01! 1 ! 4 ! 20 !
! ! ! ! ! ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!77 ! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/276/01! 1 ! 1 ! 16 !
! ! ! ! ! ! DMC!25/2/276/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!79 ! 1-4! 12 ! 1 ! Aileron position left ! FCDC!6C/1/310/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/310/10! ! ! !
! ! 1-4! 11 ! 9 ! Aileron position left ! FCDC!6C/1/310/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/310/10! ! ! !
! ! 1-4! 2 ! 2 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 25 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!81 ! 1-4! 12 ! 1 ! Capt ROLL command position! FCDC!6C/1/301/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/301/10! ! ! !
! I 1-4! 11 ! 8 ! Catp ROLL command position! FCDC!6C/1/301/01! 2 ! 1 ! 25 !
! ! ! ! ! ! FCDC!6C/2/301/10! ! ! !
! ! 1-4! 3 ! 3 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 1 ! 23 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!82 ! 1-4! 12 ! 12 ! Sideslip target ! FAC!0A/1/077/00! 1 ! 1 ! 29 !
! ! ! ! ! ! FAC!0A/2/077/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!83 ! 1-4! 12 ! 1 ! F/O ROLL command potition ! FCDC!6C/1/302/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/302/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O ROLL command potition ! FCDC!6C/1/302/01! 2 ! 1 ! 25 !
! ! ! ! ! ! FCDC!6C/2/302/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 1 ! 25 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 !1/4! 28 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!84 ! 1-4! 12 ! 12 ! Estimated sideslip ! FAC!0A/1/226/00! 1 ! 1 ! 29 !
! ! ! ! ! (side slip angle) ! !0A/2/226/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!85 ! 1-4! 12 ! 1 ! FCU discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 21 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 11 ! 1 ! FCU discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 15 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 10 ! 2 ! FCU discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 12 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 7 ! 1 ! Deceleration max on ! BSCU!6E/2/027/10! 1 ! 1 ! 22 !
! ! 1-4! 6 ! 1 ! Deceleration med on ! BSCU!6E/2/027/10! 1 ! 1 ! 21 !
! ! 1-4! 5 ! 1 ! Deceleration low on ! BSCU!6E/2/027/10! 1 ! 1 ! 20 !
! ! 1-4! 4 ! 1 ! Auto brake off ! BSCU!6E/2/026/10! 1 ! 1 ! 19 !
! ! 1-4! 3 ! 1 ! Auto brake fault ! BSCU!6E/2/026/10! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! System engaged ! BSCU!6E/2/027/10! 1 ! 1 ! 28 !
! ! 1-4! 1 ! 1 ! System engaged ! BSCU!6E/1/027/01! 1 ! 1 ! 28 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!87 ! 1-4! 12 ! 6 ! Left brake pedal angle ! BSCU!6E/2/331/10! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Right brake pedal angle ! BSCU!6E/2/330/10! 1 ! 1 ! 28 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!89 ! 1 ! 4 ! 4 ! Fleet identification ! FDIU!17/1/304/00! 1 !1/4! 21 !
! ! 2 ! 7 ! 7 ! A/C Tail number word #1 ! FDIU!17/1/301/00! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #1 ! FDIU!17/1/301/00! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #1 ! FDIU!17/1/301/00! 3 !1/4! 31 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!91 ! 1 ! 12 ! 6 ! Engine Family ! FDIU!17/1/304/00! 1 !1/4! 16 !
! ! 1 ! 6 ! 1 ! Engine type (DMU computed)! DMU! ! 1 !1/4! 1 !
! ! 1 ! 5 ! 1 ! Engine type (DMU computed)! DMU! ! 1 !1/4! 2 !
! ! 1 ! 4 ! 1 ! Engine type (DMU computed)! DMU! ! 1 !1/4! 3 !
! ! 1 ! 3 ! 3 ! A/C Type discrete ! DMU! ! 1 !1/4! 3 !
! ! ! ! ! (DMU computed) ! ! ! ! ! !
! ! 2 ! 7 ! 7 ! A/C Tail number word #2 ! FDIU!17/1/302/00! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #2 ! FDIU!17/1/302/00! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #2 ! FDIU!17/1/302/00! 3 !1/4! 31 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!93 ! 2 ! 7 ! 7 ! A/C Tail number word #3 ! FDIU!17/1/303/00! 1 !1/4! 17 !
! ! 3 ! 12 ! 12 ! Engine serial number ! ECU/!7C/1/046/01! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #1 ! ECC ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number ! ECU/!7C/1/047/01! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #1 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!95 ! 3 ! 12 ! 12 ! Engine serial number ! ECU/!7C/2/046/10! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #2 ! EEC ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number ! ECU/!7C/2/047/10! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #2 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!96 ! 1 ! 12 ! 12 ! Zero Fuel CG ! SDAC!29/1/124/01! 1 !1/4! 28 !
! ! ! ! ! ! SDAC!29/2/124/01! ! ! !
! ! 2 ! 12 ! 12 ! Zero Fuel Weight ! SDAC!29/1/167/01! 1 !1/4! 28 !
! ! ! ! ! ! SDAC!29/2/167/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!97 ! 1 ! ! ! Superframe, see Attachment! ! ! ! ! !
! ! 2,4! 12 ! 10 ! DMC bus: status word ! DMC!25/1/300/01! 1 !1/2! 25 !
! ! ! ! ! ! DMC!25/2/300/10! ! ! !
! ! 1 ! 12 ! 3 ! FDIU record version ! FDIU!17/1304/00 ! 1 !1/4! 25 !
! ! 1 ! 2 ! 1 ! FDIU maintenance word ! FDIU!17/1/350/00! 1 !1/4! 12 !
! ! ! ! ! (QAR tape low) ! ! ! ! ! !
! ! 1 ! 1 ! 1 ! DMU input discrete word #1! DMU! ! 1 !1/4! 2 !
! ! ! ! ! (DAR tape low) ! ! ! ! ! !
! ! 3 ! 12 ! 4 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 !1/4! 26 !
! ! ! ! ! ! ! 272/00! ! ! !
! ! 3 ! 8 ! 4 ! FCU Discrete status word ! FCU!A1/1B/ ! 1 !1/4! 26 !
! ! ! ! ! ! ! 272/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!98 ! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word ! DMC!25/1/300/01! 1 ! 1 ! 11 !
! ! ! ! ! ! DMC!25/2/300/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!99 ! 1,3! 12 ! 12 ! Radio height (R/A1) ! DMC!25/1/164/01! 1 !1/2! 27 !
! ! ! ! ! ! DMC!25/2/164/01! ! ! !
! ! 2,4! 12 ! 12 ! Radio height (R/A2) ! DMC!25/1/164/10! 1 !1/2! 27 !
! ! ! ! ! ! DMC!25/2/164/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!100! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!101! 1,3! 12 ! 11 ! ILS1 localizer deviation ! DMC!25/1/173/01! 1 !1/2! 29 !
! ! ! ! ! ! DMC!25/2/173/01! ! ! !
! ! 2,4! 12 ! 11 ! ILS2 localizer deviation ! DMC!25/1/173/10! 1 !1/2! 29 !
! ! ! ! ! ! DMC!25/2/173/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!102! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!103! 1,3! 12 ! 1 ! ILS1 glideslope deviation ! DMC!25/1/174/01! 1 !1/2! 29 !
! ! ! ! ! ! DMC!25/2/174/01! ! ! !
! ! 1,3! 11 ! 10 ! ILS1 glideslope deviation ! DMC!25/1/174/01! 2 !1/2! 27 !
! ! ! ! ! ! DMC!25/2/174/01! ! ! !
! ! 1,3! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/031/01! 1 !1/2! 21 !
! ! ! ! ! ! FWC!26/2/031/01! ! ! !
! ! 2,4! 12 ! 1 ! ILS2 glideslope deviation ! DMC!25/1/174/10! 1 !1/2! 29 !
! ! ! ! ! ! DMC!25/2/174/10! ! ! !
! ! 2,4! 11 ! 10 ! ILS2 glideslope deviation ! DMC!25/1/174/10! 2 !1/2! 27 !
! ! ! ! ! ! DMC!25/2/174/10! ! ! !
! ! 2,4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/031/10! 1 !1/2! 21 !
! ! ! ! ! ! FWC!26/2/031/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!104! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!105! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!106! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!107! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: ! FCDC!6C/1/041/01! 1 ! 1 ! 29 !
! ! ! ! ! EFCS status word #2 ! FCDC!6C/2/041/10! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 11 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 2 ! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 12 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 3 ! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 13 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 4 ! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 15 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!109! 1-4! 12 ! 10 ! ROLL angle ! IRS!04/1/325/01! 1 ! 2 ! 29 !
! ! ! ! ! ! IRS!04/2/325/10! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 2 ! 16 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!111! 1-4! 12 ! 1 ! Rudder position ! SDAC!29/1/312/00! 1 ! 2 ! 29 !
! ! ! ! ! ! SDAC!29/2/312/00! ! ! !
! ! 1-4! 11 ! 9 ! Rudder position ! SDAC!29/1/312/00! 2 ! 2 ! 26 !
! ! ! ! ! ! SDAC!29/2/312/00! ! ! !
! ! 1 ! 2 ! 1 ! SDAC Discrete status word ! SDAC!29/1/066/01! 1 !1/4! 15 !
! ! ! ! ! ! SDAC!29/2/066/01! ! ! !
! ! 1 ! 1 ! 1 ! SDAC Discrete status word ! SDAC!29/1/067/01! 1 !1/4! 15 !
! ! ! ! ! ! SDAC!29/2/067/01! ! ! !
! ! 4 ! 2 ! 1 ! SDAC Discrete status word ! SDAC!29/1/066/01! 1 !1/4! 17 !
! ! ! ! ! ! SDAC!29/2/066/01! ! ! !
! ! 4 ! 1 ! 1 ! SDAC Discrete status word ! SDAC!29/1/067/01! 1 !1/4! 17 !
! ! ! ! ! ! !29/2/067/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!113! 2,4! 12 ! 12 ! Actual Gross Weight ! FMC!02/1/075/00! 1 !1/2! 28 !
! ! ! ! !(10kgs)(switched parameter)! FMC!02/2/075/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!114! 1-4! 12 ! 12 ! AOA Protection Speed ! FAC!0A/1/247/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FAC!0A/2/247/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!115! 2,4! 12 ! 3 ! Actual Gross Weight ! FMC!02/1/075/00! 2 !1/2! 16 !
! ! ! ! !(10kgs)(switched parameter)! FMC!02/2/075/00! ! ! !
! ! 2,4! 1 ! 1 ! DMC status bit = 0 for Kg ! DMC!25/1/305/01! 1 !1/2! 18 !
! ! ! ! ! =1 for LBS ! DMC!25/2/305/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!116! 1-4! 12 ! 12 ! Max AOA Speed ! FAC!0A/1/243/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FAC!0A/2/243/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!123! 1 ! 12 ! 8 ! DME 1 distance ! DMC!25/1/202/01! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/202/01! ! ! !
! ! 1 ! 4 ! 1 ! SDAC Discrete status word ! SDAC!29/1/066/01! 1 !1/4! 21 !
! ! ! ! ! ! SDAC!29/2/066/01! ! ! !
! ! 1 ! 3 ! 1 ! SDAC Discrete status word ! SDAC!29/1/067/01! 1 !1/4! 21 !
! ! ! ! ! ! SDAC!29/2/067/01! ! ! !
! ! 2 ! 12 ! 9 ! VOR 1 frequency ! DMC!25/1/034/01! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/034/01! ! ! !
! ! 2 ! 3 ! 3 ! VOR 1 frequency ! DMC!25/1/034/01! 2 !1/4! 17 !
! ! ! ! ! ! DMC!25/2/034/01! ! ! !
! ! 3 ! 12 ! 9 ! ILS frequency ! DMC!25/1/033/01! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/033/01! ! ! !
! ! 3 ! 3 ! 3 ! ILS frequency ! DMC!25/1/033/01! 2 !1/4! 17 !
! ! ! ! ! ! DMC!25/2/033/01! ! ! !
! ! 4 ! 12 ! 11 ! DME 1 frequency ! DMC!25/1/035/01! 1 !1/4! 28 !
! ! ! ! ! ! DMC!25/2/035/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!125! 1-4! 12 ! 1 ! Selected vertical speed ! DMC!25/1/104/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/104/10! ! ! !
! ! 1-4! 11 ! 7 ! Selected vertical speed ! DMC!25/1/104/01! 2 ! 1 ! 27 !
! ! ! ! ! ! DMC!25/2/104/10! ! ! !
! ! 1,3! 4 ! 1 ! RH wing anti ice valve ! SDAC!29/1/001/00! 1 !1/2! 18 !
! ! ! ! ! closed system #2 ! SDAC!29/2/001/00! ! ! !
! ! 1,3! 3 ! 1 ! RH wing anti ice valve ! SDAC!29/1/001/11! 1 !1/2! 18 !
! ! ! ! ! closed system #1 ! SDAC!29/2/001/11! ! ! !
! ! 1,3! 2 ! 1 ! Engine 2 anti ice ! SDAC!29/1/001/00! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 1,3! 1 ! 1 ! Engine 1 anti ice ! SDAC!29/1/001/11! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 2,4! 4 ! 1 ! Engine 2 anti ice ! SDAC!29/1/003/10! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! SDAC!29/2/003/10! ! ! !
! ! 2,4! 3 ! 1 ! Engine 1 anti ice ! SDAC!29/1/003/01! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! SDAC!29/2/003/01! ! ! !
! ! 2,4! 2 ! 1 ! Wing anti ice P/B ON ! SDAC!29/1/003/11! 1 !1/2! 22 !
! ! ! ! ! ! SDAC!29/2/003/11! ! ! !
! ! 2 ! 1 ! 1 ! APU Bleed valve open ! APU!7A/1/037/01! 1 !1/4! 11 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!127! 1-4! 12 ! 10 ! Selected altitude ! DMC!25/1/102/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC!25/2/102/10! ! ! !
! ! 1,3! 2 ! 1 ! Pack flow control valve ! SDAC!29/1/003/10! 1 !1/2! 21 !
! ! ! ! ! fully closed system #1 ! SDAC!29/2/003/10! ! ! !
! ! 1,3! 1 ! 1 ! Pack flow control valve ! SDAC!29/1/003/01! 1 !1/2! 21 !
! ! ! ! ! fully closed system #1 ! SDAC!29/2/003/01! ! ! !
! ! 2 ! 2 ! 1 ! SDAC Discrete status word ! SDAC!29/1/066/01! 1 !1/4! 11 !
! ! ! ! ! ! SDAC!29/2/066/01! ! ! !
! ! 2 ! 1 ! 1 ! SDAC Discrete status word ! SDAC!29/1/066/01! 1 !1/4! 11 !
! ! ! ! ! ! SDAC!29/2/066/01! ! ! !
! ! 4 ! 2 ! 1 ! XFEED valve fully ! SDAC!29/1/055/10! 1 !1/4! 16 !
! ! ! ! ! closed engine #2 ! SDAC!29/2/055/10! ! ! !
! ! 4 ! 1 ! 1 ! XFEED valve fully ! SDAC!29/1/055/01! 1 !1/4! 16 !
! ! ! ! ! closed engine #1 ! SDAC!29/2/055/01! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!65 ! 1-4! 12 ! 12 ! Stall speed !FAC !0A/1/246/00 ! 1 ! 2 ! 28 !
! ! ! ! ! !FAC !0A/2/246/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!66 ! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!67 ! 1-4! 12 ! 6 ! Right brake pedal angle !BSCU !6E/1/330/01 ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Left brake pedal angle !BSCU !6E/1/331/01 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!68 ! 1-4! 12 ! 12 ! FD Roll Order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!69 ! 1-4! 12 ! 1 ! Stabilizer position #1 !FCDC !6C/1/315/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/315/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Stabilizer position #1 !FCDC !6C/1/315/01 ! 2 ! 1 ! 25 !
! ! ! ! ! !FCDC !6C/2/315/10 ! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 20 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 21 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 19 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!70 ! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!71 ! 1-4! 12 ! 8 ! SLAT actual !SFCC !1B/1/127/01 ! 1 ! 1 ! 29 !
! ! ! ! ! position switched !SFCC !1B/2/127/10 ! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 15 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 16 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 17 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 18 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!72 ! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!73 ! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!75 ! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/276/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 276) !DMC !25/2/276/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!76 ! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label=015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/041/01 ! 1 ! 4 ! 20 !
! ! ! ! ! word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!77 ! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/276/01 ! 1 ! 1 ! 16 !
! ! ! ! ! word (label 276) !DMC !25/2/276/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!79 ! 1-4! 12 ! 1 ! Aileron position left !FCDC !6C/1/310/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/310/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Aileron position left !FCDC !6C/1/310/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/310/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 25 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!81 ! 1-4! 12 ! 1 ! Capt ROLL command !FCDC !6C/1/301/01 ! 1 ! 1 ! 29 !
! ! ! ! ! position !FCDC !6C/2/301/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Catp ROLL command !FCDC !6C/1/301/01 ! 2 ! 1 ! 25 !
! ! ! ! ! position !FCDC !6C/2/301/10 ! ! ! !
! ! 1-4! 3 ! 3 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 1 ! 23 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!82 ! 1-4! 12 ! 12 ! Sideslip target !FAC !0A/1/077/00 ! 1 ! 1 ! 29 !
! ! ! ! ! !FAC !0A/2/077/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!83 ! 1-4! 12 ! 1 ! F/O ROLL command potition!FCDC !6C/1/302/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/302/10 ! ! ! !
! ! 1-4! 11 ! 8 ! F/O ROLL command potition!FCDC !6C/1/302/01 ! 2 ! 1 ! 25 !
! ! ! ! ! !FCDC !6C/2/302/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/043/01 ! 1 ! 1 ! 25 !
! ! ! ! ! word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: EFCS status !FCDC !6C/1/043/01 ! 1 !1/4! 28 !
! ! ! ! ! word #4 !FCDC !6C/2/043/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!84 ! 1-4! 12 ! 12 ! Estimated sideslip !FAC !0A/1/226/00 ! 1 ! 1 ! 29 !
! ! ! ! ! (side slip angle) ! !0A/2/226/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!85 ! 1-4! 12 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 21 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 11 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 15 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 10 ! 2 ! FCU discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 12 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 7 ! 1 ! Deceleration max on !BSCU !6E/2/027/10 ! 1 ! 1 ! 22 !
! ! 1-4! 6 ! 1 ! Deceleration med on !BSCU !6E/2/027/10 ! 1 ! 1 ! 21 !
! ! 1-4! 5 ! 1 ! Deceleration low on !BSCU !6E/2/027/10 ! 1 ! 1 ! 20 !
! ! 1-4! 4 ! 1 ! Auto brake off !BSCU !6E/2/026/10 ! 1 ! 1 ! 19 !
! ! 1-4! 3 ! 1 ! Auto brake fault !BSCU !6E/2/026/10 ! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! System engaged !BSCU !6E/2/027/10 ! 1 ! 1 ! 28 !
! ! 1-4! 1 ! 1 ! System engaged !BSCU !6E/1/027/01 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!87 ! 1-4! 12 ! 6 ! Left brake pedal angle !BSCU !6E/2/331/10 ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Right brake pedal angle !BSCU !6E/2/330/10 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!89 ! 1 ! 4 ! 4 ! Fleet identification !FDIU !17/1/304/00 ! 1 !1/4! 21 !
! ! 2 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 3 !1/4! 31 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!91 ! 1 ! 12 ! 6 ! Engine Family !FDIU !17/1/304/00 ! 1 !1/4! 16 !
! ! 1 ! 6 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 1 !
! ! ! ! ! computed) MP15G ! ! ! ! ! !
! ! 1 ! 5 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 2 !
! ! ! ! ! computed) MP15F ! ! ! ! ! !
! ! 1 ! 4 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 3 !
! ! ! ! ! computed) MP15E ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! A/C Type discrete !DMU ! ! 1 !1/4! 3 !
! ! ! ! ! (DMU computed) MP15B-D ! ! ! ! ! !
! ! 2 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 3 !1/4! 31 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!93 ! 2 ! 7 ! 7 ! A/C Tail number word #3 !FDIU !17/1/303/00 ! 1 !1/4! 17 !
! ! 3 ! 12 ! 12 ! Engine serial number !EIU !7B/1/046/xx ! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #1 ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number !EIU !7B/1/047/xx ! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #1 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!95 ! 3 ! 12 ! 12 ! Engine serial number !EIU !7B/2/046/xx ! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #2 ! ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number !EIU !7B/2/047/xx ! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #2 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!97 ! 1 ! ! ! Superframe, ! ! ! ! ! !
! ! ! ! ! see Attachment ! ! ! ! ! !
! ! 2,4! 12 ! 10 ! DMC bus: Discrete status !DMC !25/1/300/01 ! 1 !1/2! 25 !
! ! ! ! ! (label 300) !DMC !25/2/300/10 ! ! ! !
! ! 3 ! 12 ! 4 ! FCU Discrete status word !FCU !A1/1A/272/00! 1 !1/4! 26 !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
! ! 3 ! 8 ! 4 ! FCU Discrete status word !FCU !A1/1B/272/00! 1 !1/4! 26 !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!98 ! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word !DMC !25/1/300/01 ! 1 ! 1 ! 11 !
! ! ! ! ! (label 300) !DMC !25/2/300/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!99 ! 1,3! 12 ! 12 ! Radio height (R/A1) !DMC !25/1/164/01 ! 1 !1/2! 27 !
! ! ! ! ! !DMC !25/2/164/01 ! ! ! !
! ! 2,4! 12 ! 12 ! Radio height (R/A2) !DMC !25/1/164/10 ! 1 !1/2! 27 !
! ! ! ! ! !DMC !25/2/164/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!100! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!101! 1,3! 12 ! 11 ! ILS1 localizer deviation !DMC !25/1/173/01 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/173/01 ! ! ! !
! ! 2,4! 12 ! 11 ! ILS2 localizer deviation !DMC !25/1/173/10 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/173/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!102! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!103! 1,3! 12 ! 1 ! ILS1 glideslope deviation!DMC !25/1/174/01 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/174/01 ! ! ! !
! ! 1,3! 11 ! 10 ! ILS1 glideslope deviation!DMC !25/1/174/01 ! 2 !1/2! 27 !
! ! ! ! ! !DMC !25/2/174/01 ! ! ! !
! ! 1,3! 1 ! 1 ! FWC Discrete status word !FWC !26/1/031/01 ! 1 !1/2! 21 !
! ! ! ! ! (Label=031 SDI=01) !FWC !26/2/031/01 ! ! ! !
! ! 2,4! 12 ! 1 ! ILS2 glideslope deviation!DMC !25/1/174/10 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/174/10 ! ! ! !
! ! 2,4! 11 ! 10 ! ILS2 glideslope deviation!DMC !25/1/174/10 ! 2 !1/2! 27 !
! ! ! ! ! !DMC !25/2/174/10 ! ! ! !
! ! 2,4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/031/10 ! 1 !1/2! 21 !
! ! ! ! ! (Label=031 SDI=10) !FWC !26/2/031/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!104! 1-4! 12 ! 12 ! LH spoiler #1 position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!105! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!106! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!107! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: !FCDC !6C/1/041/01 ! 1 ! 1 ! 29 !
! ! ! ! ! EFCS status word #2 !FCDC !6C/2/041/10 ! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 11 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 12 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 13 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 15 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!109! 1-4! 12 ! 10 ! ROLL angle !IRS !04/1/325/01 ! 1 ! 2 ! 29 !
! ! ! ! ! !IRS !04/2/325/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 2 ! 16 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!111! 1-4! 12 ! 1 ! Rudder position !SDAC !29/1/312/00 ! 1 ! 2 ! 29 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1-4! 11 ! 9 ! Rudder position !SDAC !29/1/312/00 ! 2 ! 2 ! 26 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 15 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 1 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 15 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 4 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 17 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 4 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 17 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!113! 2,4! 12 ! 12 ! Actual Gross Weight !FMC !02/1/075/00 ! 1 !1/2! 28 !
! ! ! ! ! (10kgs) (switched !FMC !02/2/075/00 ! ! ! !
! ! ! ! ! parameter) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!114! 1-4! 12 ! 12 ! AOA Protection Speed !FAC !0A/1/247/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FAC !0A/2/247/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!115! 2,4! 12 ! 3 ! Actual Gross Weight !FMC !02/1/075/00 ! 2 !1/2! 16 !
! ! ! ! ! (10kgs) (switched !FMC !02/2/075/00 ! ! ! !
! ! ! ! ! parameter) ! ! ! ! ! !
! ! 2,4! 1 ! 1 ! DMC status bit = 0 for Kg!DMC !25/1/305/01 ! 1 !1/2! 18 !
! ! ! ! ! =1 for LBS !DMC !25/2/305/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!116! 1-4! 12 ! 12 ! Max AOA Speed !FAC !0A/1/243/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FAC !0A/2/243/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!118! 1-4! 1 ! 1 ! WEFAL1:WEFA discreet 1 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! MP14E ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! WEFAL2:WEFA discreet 2 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! TP14H ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! WEFAL3:WEFA discreet 3 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! MP14G ! ! ! ! ! !
! ! 1 ! 12 ! 8 ! WEFA_MW (Byte 0) !DMU ! ! 1 !1/4! 8 !
! ! 2 ! 12 ! 8 ! WEFA_MW (Byte 1) !DMU ! ! 1 !1/4! 16 !
! ! 3 ! 12 ! 8 ! WEFA_MW (Byte 2) !DMU ! ! 1 !1/4! 24 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!120! 1,3! 12 ! 12 ! MW_PCMCIA (Partial data !DMU ! ! 1 !1/2! 12 !
! ! ! ! ! LSB) ! ! ! ! ! !
! ! 2,4! 12 ! 12 ! MW_PCMCIA (Partial data !DMU ! ! 1 !1/2! 24 !
! ! ! ! ! MSB) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!123! 1 ! 12 ! 8 ! DME 1 distance !DMC !25/1/202/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/202/01 ! ! ! !
! ! 1 ! 4 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 21 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 1 ! 3 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 21 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 2 ! 12 ! 9 ! VOR 1 frequency !DMC !25/1/034/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/034/01 ! ! ! !
! ! 2 ! 3 ! 3 ! VOR 1 frequency !DMC !25/1/034/01 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/034/01 ! ! ! !
! ! 3 ! 12 ! 9 ! ILS 1 frequency !DMC !25/1/033/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/033/01 ! ! ! !
! ! 3 ! 3 ! 3 ! ILS 1 frequency !DMC !25/1/033/01 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/033/01 ! ! ! !
! ! 4 ! 12 ! 11 ! DME 1 frequency !DMC !25/1/035/01 ! 1 !1/4! 28 !
! ! ! ! ! !DMC !25/2/035/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!125! 1,3! 2 ! 1 ! Engine 2 anti ice !EIU !7B/2/105/xx ! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 1,3! 1 ! 1 ! Engine 1 anti ice !EIU !7B/1/105/xx ! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 2,4! 4 ! 1 ! Engine 2 anti ice !EIU !7B/2/105/XX ! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! ! ! ! ! !
! ! 2,4! 3 ! 1 ! Engine 1 anti ice !EIU !7B/1/105/XX ! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! ! ! ! ! !
! ! 1,4! 12 ! 1 ! Selected vertical speed !DMC !25/1/104/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/104/10 ! ! ! !
! ! 1,4! 11 ! 7 ! Selected vertical speed !DMC !25/1/104/01 ! 2 ! 1 ! 27 !
! ! ! ! ! !DMC !25/2/104/10 ! ! ! !
! ! 1,3! 4 ! 1 ! RH wing anti ice valve !SDAC !29/1/001/00 ! 1 !1/2! 18 !
! ! ! ! ! closed system #2 !SDAC !29/2/001/00 ! ! ! !
! ! 1,3! 3 ! 1 ! LH wing anti ice valve !SDAC !29/1/001/11 ! 1 !1/2! 18 !
! ! ! ! ! closed system #1 !SDAC !29/2/001/11 ! ! ! !
! ! 2,4! 2 ! 1 ! Wing anti ice P/B ON !SDAC !29/1/003/11 ! 1 !1/2! 22 !
! ! ! ! ! !SDAC !29/2/003/11 ! ! ! !
! ! 2 ! 1 ! 1 ! APU Bleed valve open !APU !7A/1/037/01 ! 1 !1/4! 11 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!127! 1-4! 12 ! 10 ! Selected altitude !DMC !25/1/102/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/102/10 ! ! ! !
! ! 1,3! 2 ! 1 ! Pack flow control valve !SDAC !29/1/003/10 ! 1 !1/2! 21 !
! ! ! ! ! fully closed system #2 !SDAC !29/2/003/10 ! ! ! !
! ! 1,3! 1 ! 1 ! Pack flow control valve !SDAC !29/1/003/01 ! 1 !1/2! 21 !
! ! ! ! ! fully closed system #1 !SDAC !29/2/003/01 ! ! ! !
! ! 2 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 11 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 2 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 11 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 4 ! 2 ! 1 ! XFEED valve fully !SDAC !29/1/055/10 ! 1 !1/4! 16 !
! ! ! ! ! closed engine #2 !SDAC !29/2/055/10 ! ! ! !
! ! 4 ! 1 ! 1 ! XFEED valve fully !SDAC !29/1/055/01 ! 1 !1/4! 16 !
! ! ! ! ! closed engine #1 !SDAC !29/2/055/01 ! ! ! !
+---+----+----+----+--------------------------+-----+------------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!65 ! 1-4! 12 ! 12 ! Stall speed !FAC !0A/1/246/00 ! 1 ! 2 ! 28 !
! ! ! ! ! !FAC !0A/2/246/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!66 ! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!67 ! 1-4! 12 ! 6 ! Right brake pedal angle !BSCU !6E/1/330/01 ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Left brake pedal angle !BSCU !6E/1/331/01 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!68 ! 1-4! 12 ! 12 ! FD Roll Order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!69 ! 1-4! 12 ! 1 ! Stabilizer position #1 !FCDC !6C/1/315/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/315/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Stabilizer position #1 !FCDC !6C/1/315/01 ! 2 ! 1 ! 25 !
! ! ! ! ! !FCDC !6C/2/315/10 ! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 20 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 21 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 19 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!70 ! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!71 ! 1-4! 12 ! 8 ! SLAT actual !SFCC !1B/1/127/01 ! 1 ! 1 ! 29 !
! ! ! ! ! position switched !SFCC !1B/2/127/10 ! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 15 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 16 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 17 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 ! 1 ! 18 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!72 ! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!73 ! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!75 ! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/276/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 276) !DMC !25/2/276/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!76 ! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label=015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/041/01 ! 1 ! 4 ! 20 !
! ! ! ! ! word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!77 ! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/276/01 ! 1 ! 1 ! 16 !
! ! ! ! ! word (label 276) !DMC !25/2/276/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!79 ! 1-4! 12 ! 1 ! Aileron position left !FCDC !6C/1/310/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/310/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Aileron position left !FCDC !6C/1/310/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/310/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 25 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!81 ! 1-4! 12 ! 1 ! Capt ROLL command !FCDC !6C/1/301/01 ! 1 ! 1 ! 29 !
! ! ! ! ! position !FCDC !6C/2/301/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Catp ROLL command !FCDC !6C/1/301/01 ! 2 ! 1 ! 25 !
! ! ! ! ! position !FCDC !6C/2/301/10 ! ! ! !
! ! 1-4! 3 ! 3 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 1 ! 23 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!82 ! 1-4! 12 ! 12 ! Sideslip target !FAC !0A/1/077/00 ! 1 ! 1 ! 29 !
! ! ! ! ! !FAC !0A/2/077/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!83 ! 1-4! 12 ! 1 ! F/O ROLL command potition!FCDC !6C/1/302/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/302/10 ! ! ! !
! ! 1-4! 11 ! 8 ! F/O ROLL command potition!FCDC !6C/1/302/01 ! 2 ! 1 ! 25 !
! ! ! ! ! !FCDC !6C/2/302/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: EFCS status !FCDC !6C/1/043/01 ! 1 ! 1 ! 25 !
! ! ! ! ! word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: EFCS status !FCDC !6C/1/043/01 ! 1 !1/4! 28 !
! ! ! ! ! word #4 !FCDC !6C/2/043/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!84 ! 1-4! 12 ! 12 ! Estimated sideslip !FAC !0A/1/226/00 ! 1 ! 1 ! 29 !
! ! ! ! ! (side slip angle) ! !0A/2/226/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!85 ! 1-4! 12 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 21 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 11 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 15 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 10 ! 2 ! FCU discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 12 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 7 ! 1 ! Deceleration max on !BSCU !6E/2/027/10 ! 1 ! 1 ! 22 !
! ! 1-4! 6 ! 1 ! Deceleration med on !BSCU !6E/2/027/10 ! 1 ! 1 ! 21 !
! ! 1-4! 5 ! 1 ! Deceleration low on !BSCU !6E/2/027/10 ! 1 ! 1 ! 20 !
! ! 1-4! 4 ! 1 ! Auto brake off !BSCU !6E/2/026/10 ! 1 ! 1 ! 19 !
! ! 1-4! 3 ! 1 ! Auto brake fault !BSCU !6E/2/026/10 ! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 1 ! System engaged !BSCU !6E/2/027/10 ! 1 ! 1 ! 28 !
! ! 1-4! 1 ! 1 ! System engaged !BSCU !6E/1/027/01 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!87 ! 1-4! 12 ! 6 ! Left brake pedal angle !BSCU !6E/2/331/10 ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! Right brake pedal angle !BSCU !6E/2/330/10 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!89 ! 1 ! 4 ! 4 ! Fleet identification !FDIU !17/1/304/00 ! 1 !1/4! 21 !
! ! 2 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #1 !FDIU !17/1/301/00 ! 3 !1/4! 31 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!91 ! 1 ! 12 ! 6 ! Engine Family !FDIU !17/1/304/00 ! 1 !1/4! 16 !
! ! 1 ! 6 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 1 !
! ! ! ! ! computed) MP15G ! ! ! ! ! !
! ! 1 ! 5 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 2 !
! ! ! ! ! computed) MP15F ! ! ! ! ! !
! ! 1 ! 4 ! 1 ! Engine type (DMU !DMU ! ! 1 !1/4! 3 !
! ! ! ! ! computed) MP15E ! ! ! ! ! !
! ! 1 ! 3 ! 3 ! A/C Type discrete !DMU ! ! 1 !1/4! 3 !
! ! ! ! ! (DMU computed) MP15B-D ! ! ! ! ! !
! ! 2 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 1 !1/4! 17 !
! ! 3 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 2 !1/4! 24 !
! ! 4 ! 7 ! 7 ! A/C Tail number word #2 !FDIU !17/1/302/00 ! 3 !1/4! 31 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!93 ! 2 ! 7 ! 7 ! A/C Tail number word #3 !FDIU !17/1/303/00 ! 1 !1/4! 17 !
! ! 3 ! 12 ! 12 ! Engine serial number !ECU/ !7C/1/046/01 ! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #1 !EEC ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number !ECU/ !7C/1/047/01 ! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #1 !EEC ! ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!95 ! 3 ! 12 ! 12 ! Engine serial number !ECU/ !7C/2/046/10 ! 1 !1/4! 26 !
! ! ! ! ! (Last half) engine #2 !EEC ! ! ! ! !
! ! 4 ! 12 ! 12 ! Engine serial number !ECU/ !7C/2/047/10 ! 1 !1/4! 26 !
! ! ! ! ! (First half) engine #2 !EEC ! ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!97 ! 1 ! ! ! Superframe, ! ! ! ! ! !
! ! ! ! ! see Attachment ! ! ! ! ! !
! ! 2,4! 12 ! 10 ! DMC bus: Discrete status !DMC !25/1/300/01 ! 1 !1/2! 25 !
! ! ! ! ! (label 300) !DMC !25/2/300/10 ! ! ! !
! ! 3 ! 12 ! 4 ! FCU Discrete status word !FCU !A1/1A/272/00! 1 !1/4! 26 !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
! ! 3 ! 8 ! 4 ! FCU Discrete status word !FCU !A1/1B/272/00! 1 !1/4! 26 !
! ! ! ! ! (Label=272 SDI=00) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!98 ! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word !DMC !25/1/300/01 ! 1 ! 1 ! 11 !
! ! ! ! ! (label 300) !DMC !25/2/300/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!99 ! 1,3! 12 ! 12 ! Radio height (R/A1) !DMC !25/1/164/01 ! 1 !1/2! 27 !
! ! ! ! ! !DMC !25/2/164/01 ! ! ! !
! ! 2,4! 12 ! 12 ! Radio height (R/A2) !DMC !25/1/164/10 ! 1 !1/2! 27 !
! ! ! ! ! !DMC !25/2/164/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!100! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!101! 1,3! 12 ! 11 ! ILS1 localizer deviation !DMC !25/1/173/01 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/173/01 ! ! ! !
! ! 2,4! 12 ! 11 ! ILS2 localizer deviation !DMC !25/1/173/10 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/173/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!102! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!103! 1,3! 12 ! 1 ! ILS1 glideslope deviation!DMC !25/1/174/01 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/174/01 ! ! ! !
! ! 1,3! 11 ! 10 ! ILS1 glideslope deviation!DMC !25/1/174/01 ! 2 !1/2! 27 !
! ! ! ! ! !DMC !25/2/174/01 ! ! ! !
! ! 1,3! 1 ! 1 ! FWC Discrete status word !FWC !26/1/031/01 ! 1 !1/2! 21 !
! ! ! ! ! (Label=031 SDI=01) !FWC !26/2/031/01 ! ! ! !
! ! 2,4! 12 ! 1 ! ILS2 glideslope deviation!DMC !25/1/174/10 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/174/10 ! ! ! !
! ! 2,4! 11 ! 10 ! ILS2 glideslope deviation!DMC !25/1/174/10 ! 2 !1/2! 27 !
! ! ! ! ! !DMC !25/2/174/10 ! ! ! !
! ! 2,4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/031/10 ! 1 !1/2! 21 !
! ! ! ! ! (Label=031 SDI=10) !FWC !26/2/031/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!104! 1-4! 12 ! 12 ! LH spoiler #1 position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!105! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!106! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!107! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: !FCDC !6C/1/041/01 ! 1 ! 1 ! 29 !
! ! ! ! ! EFCS status word #2 !FCDC !6C/2/041/10 ! ! ! !
! ! 1 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 11 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 12 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 13 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 3 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 15 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!109! 1-4! 12 ! 10 ! ROLL angle !IRS !04/1/325/01 ! 1 ! 2 ! 29 !
! ! ! ! ! !IRS !04/2/325/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 2 ! 16 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!111! 1-4! 12 ! 1 ! Rudder position !SDAC !29/1/312/00 ! 1 ! 2 ! 29 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1-4! 11 ! 9 ! Rudder position !SDAC !29/1/312/00 ! 2 ! 2 ! 26 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 15 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 1 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 15 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 4 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 17 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 4 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 17 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!113! 2,4! 12 ! 12 ! Actual Gross Weight !FMC !02/1/075/00 ! 1 !1/2! 28 !
! ! ! ! ! (10kgs) (switched !FMC !02/2/075/00 ! ! ! !
! ! ! ! ! parameter) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!114! 1-4! 12 ! 12 ! AOA Protection Speed !FAC !0A/1/247/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FAC !0A/2/247/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!115! 2,4! 12 ! 3 ! Actual Gross Weight !FMC !02/1/075/00 ! 2 !1/2! 16 !
! ! ! ! ! (10kgs) (switched !FMC !02/2/075/00 ! ! ! !
! ! ! ! ! parameter) ! ! ! ! ! !
! ! 2,4! 1 ! 1 ! DMC status bit = 0 for Kg!DMC !25/1/305/01 ! 1 !1/2! 18 !
! ! ! ! ! =1 for LBS !DMC !25/2/305/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!116! 1-4! 12 ! 12 ! Max AOA Speed !FAC !0A/1/243/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FAC !0A/2/243/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!118! 1-4! 1 ! 1 ! WEFAL1:WEFA discreet 1 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! MP14E ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! WEFAL2:WEFA discreet 2 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! TP14H ! ! ! ! ! !
! ! 1-4! 3 ! 1 ! WEFAL3:WEFA discreet 3 !DMU ! ! 1 ! 1 ! 1 !
! ! ! ! ! MP14G ! ! ! ! ! !
! ! 1 ! 12 ! 8 ! WEFA_MW (Byte 0) !DMU ! ! 1 !1/4! 8 !
! ! 2 ! 12 ! 8 ! WEFA_MW (Byte 1) !DMU ! ! 1 !1/4! 16 !
! ! 3 ! 12 ! 8 ! WEFA_MW (Byte 2) !DMU ! ! 1 !1/4! 24 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!120! 1,3! 12 ! 12 ! MW_PCMCIA (Partial data !DMU ! ! 1 !1/2! 12 !
! ! ! ! ! LSB) ! ! ! ! ! !
! ! 2,4! 12 ! 12 ! MW_PCMCIA (Partial data !DMU ! ! 1 !1/2! 24 !
! ! ! ! ! MSB) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!123! 1 ! 12 ! 8 ! DME 1 distance !DMC !25/1/202/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/202/01 ! ! ! !
! ! 1 ! 4 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 21 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 1 ! 3 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 21 !
! ! ! ! ! (Label=067 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 2 ! 12 ! 9 ! VOR 1 frequency !DMC !25/1/034/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/034/01 ! ! ! !
! ! 2 ! 3 ! 3 ! VOR 1 frequency !DMC !25/1/034/01 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/034/01 ! ! ! !
! ! 3 ! 12 ! 9 ! ILS 1 frequency !DMC !25/1/033/01 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/033/01 ! ! ! !
! ! 3 ! 3 ! 3 ! ILS 1 frequency !DMC !25/1/033/01 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/033/01 ! ! ! !
! ! 4 ! 12 ! 11 ! DME 1 frequency !DMC !25/1/035/01 ! 1 !1/4! 28 !
! ! ! ! ! !DMC !25/2/035/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!125! 1,3! 2 ! 1 ! Engine 2 anti ice !SDAC !29/1/001/00 ! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 1,3! 1 ! 1 ! Engine 1 anti ice !SDAC !29/1/001/11 ! 1 !1/2! 19 !
! ! ! ! ! valve fault (on) ! ! ! ! ! !
! ! 2,4! 4 ! 1 ! Engine 2 anti ice !SDAC !29/1/003/10 ! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! !29/2/003/10 ! ! ! !
! ! 2,4! 3 ! 1 ! Engine 1 anti ice !SDAC !29/1/003/01 ! 1 !1/2! 18 !
! ! ! ! ! P/B ON (closed) ! !29/2/003/01 ! ! ! !
! ! 1,4! 12 ! 1 ! Selected vertical speed !DMC !25/1/104/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/104/10 ! ! ! !
! ! 1,4! 11 ! 7 ! Selected vertical speed !DMC !25/1/104/01 ! 2 ! 1 ! 27 !
! ! ! ! ! !DMC !25/2/104/10 ! ! ! !
! ! 1,3! 4 ! 1 ! RH wing anti ice valve !SDAC !29/1/001/00 ! 1 !1/2! 18 !
! ! ! ! ! closed system #2 !SDAC !29/2/001/00 ! ! ! !
! ! 1,3! 3 ! 1 ! LH wing anti ice valve !SDAC !29/1/001/11 ! 1 !1/2! 18 !
! ! ! ! ! closed system #1 !SDAC !29/2/001/11 ! ! ! !
! ! 2,4! 2 ! 1 ! Wing anti ice P/B ON !SDAC !29/1/003/11 ! 1 !1/2! 22 !
! ! ! ! ! !SDAC !29/2/003/11 ! ! ! !
! ! 2 ! 1 ! 1 ! APU Bleed valve open !APU !7A/1/037/01 ! 1 !1/4! 11 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!127! 1-4! 12 ! 10 ! Selected altitude !DMC !25/1/102/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/102/10 ! ! ! !
! ! 1,3! 2 ! 1 ! Pack flow control valve !SDAC !29/1/003/10 ! 1 !1/2! 21 !
! ! ! ! ! fully closed system #2 !SDAC !29/2/003/10 ! ! ! !
! ! 1,3! 1 ! 1 ! Pack flow control valve !SDAC !29/1/003/01 ! 1 !1/2! 21 !
! ! ! ! ! fully closed system #1 !SDAC !29/2/003/01 ! ! ! !
! ! 2 ! 2 ! 1 ! SDAC Discrete status word!SDAC !29/1/066/01 ! 1 !1/4! 11 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/066/01 ! ! ! !
! ! 2 ! 1 ! 1 ! SDAC Discrete status word!SDAC !29/1/067/01 ! 1 !1/4! 11 !
! ! ! ! ! (Label=066 SDI=01) !SDAC !29/2/067/01 ! ! ! !
! ! 4 ! 2 ! 1 ! XFEED valve fully !SDAC !29/1/055/10 ! 1 !1/4! 16 !
! ! ! ! ! closed engine #2 !SDAC !29/2/055/10 ! ! ! !
! ! 4 ! 1 ! 1 ! XFEED valve fully !SDAC !29/1/055/01 ! 1 !1/4! 16 !
! ! ! ! ! closed engine #1 !SDAC !29/2/055/01 ! ! ! !
+---+----+----+----+--------------------------+-----+------------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

H. DAR Frame Assignment (Word 129-192)
+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!129! 1-4! 12 ! 12 ! Body axis roll rate ! IRS!04/1/327/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS!04/2/327/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!130! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS!04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!131! 1-4! 12 ! 10 ! RH spoiler #2 position ! FCDC!6C/1/372/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/372/10! ! ! !
! ! 1 ! 2 ! 2 ! FWC Discrete status word ! FWC!26/1/126/11! 1 !1/4! 12 !
! ! ! ! ! ! FWC!26/2/126/11! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: status word ! DMC!25/1/270/01! 1 !1/4! 16 !
! ! ! ! ! ! DMC!25/2/270/10! ! ! !
! ! 3 ! 1 ! 1 ! AC2 bus off ! SDAC!29/1/002/10! 1 !1/4! 20 !
! ! ! ! ! ! SDAC!29/2/002/10! ! ! !
! ! 4 ! 2 ! 1 ! DC2 bus off ! SDAC!29/1/004/10! 1 !1/4! 29 !
! ! ! ! ! ! SDAC!29/2/004/10! ! ! !
! ! 4 ! 1 ! 1 ! DC1 bus off ! SDAC!29/1/004/01! 1 !1/4! 29 !
! ! ! ! ! ! SDAC!29/2/004/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!132! 1-4! 12 ! 12 ! FD Roll Order ! FGC!01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!133! 1-4! 12 ! 10 ! RH spoiler #3 position ! FCDC!6C/1/373/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/373/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/272/01! 1 !1/4! 16 !
! ! ! ! ! ! DMC!25/2/272/10! ! ! !
! ! 1 ! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/126/11! 1 !1/4! 13 !
! ! ! ! ! ! FWC!26/2/126/11! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: status word ! DMC!25/1/270/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/270/10! ! ! !
! ! 3 ! 2 ! 2 ! DMC bus: status word ! DMC!25/1/305/01! 1 !1/4! 29 !
! ! ! ! ! ! DMC!25/2/305/10! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 25 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 26 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!134! 1-4! 12 ! 12 ! FD Pitch Order ! FGC!01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!135! 1-4! 12 ! 10 ! RH spoiler #5 position ! FCDC!6C/1/375/01! 1 ! 1 ! 27 !
! ! ! ! ! ! FCDC!6C/2/375/10! ! ! !
! ! 1 ! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 19 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 1 ! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 20 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 2 ! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 21 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 2 ! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 22 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 3 ! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 23 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 3 ! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 24 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/040/01! 1 !1/4! 29 !
! ! ! ! ! EFCS status word #1 ! FCDC!6C/2/040/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!136! 1-4! 12 ! 12 ! FD Pitch Order ! FGC!01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!137! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!139! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 1 ! Eng2 HP fuel valve closed ! FWC!26/1/011/10! 1 ! 1 ! 14 !
! ! ! ! ! ! FWC!26/2/011/10! ! ! !
! ! 1-4! 2 ! 1 ! Eng1 HP fuel valve closed ! FWC!26/1/011/01! 1 ! 1 ! 14 !
! ! ! ! ! ! FWC!26/2/011/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!140! 1-4! 12 ! 10 ! FWC Discrete status word ! FWC!26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC!26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: ! FCDC!6C/1/041/01! 1 ! 4 ! 20 !
! ! ! ! ! EFCS status word #2 ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!141! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 2 ! 1 ! Fuel fire valve engine #2 ! SDAC!29/1/001/10! 1 ! 1 ! 19 !
! ! ! ! ! fully closed ! SDAC!29/2/001/10! ! ! !
! ! 1-4! 1 ! 1 ! Fuel fire valve engine #1 ! SDAC!29/1/001/01! 1 ! 1 ! 19 !
! ! ! ! ! fully closed ! SDAC!29/2/001/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!143! 1-4! 12 ! 12 ! True heading ! IRS!04/1/314/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS!04/2/314/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!145! 1-4! 12 ! 1 ! Throttle resolver ! ECU/!7C/2/133/10! 1 ! 1 ! 29 !
! ! ! ! ! angle engine #2 ! EEC ! ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver ! ECU/!7C/2/133/10! 2 ! 1 ! 27 !
! ! ! ! ! angle engine #2 ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!146! 1-4! 12 ! 12 ! FMGC discrete ! FGC!01/1/273/00! 1 ! 1 ! 25 !
! ! ! ! ! status word #3 ! FGC!01/2/273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!147! 1-4! 12 ! 5 ! FMGC discrete ! FGC!01/1/274/00! 1 ! 1 ! 27 !
! ! ! ! ! status word #1 ! FGC!01/2/274/00! ! ! !
! ! 1-4! 2 ! 2 ! FMGC discrete ! FGC!01/1/273/00! 1 ! 1 ! 13 !
! ! ! ! ! status word #3 ! FGC!01/2/273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!149! 1-4! 12 ! 10 ! N1 Actual (low rotor ! ECU/!7C/2/346/10! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/017/11! 1 ! 1 ! 28 !
! ! ! ! ! ! FWC!26/2/017/11! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/017/11! 1 ! 1 ! 20 !
! ! ! ! ! ! FWC!26/2/017/11! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!151! 1-4! 12 ! 10 ! EGT LPT exit ! ECU/!7C/2/345/10! 1 ! 1 ! 27 !
! ! ! ! ! exit temp engine 2# ! EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/017/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FWC!26/2/017/00! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/017/00! 1 ! 1 ! 20 !
! ! ! ! ! ! FWC!26/2/017/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!153! ! ! ! SEE APPENDIX ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!155! 1-4! 12 ! 6 ! N1 vibration eng #2 ! EVMU!3D/1/135/10! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #2 ! EVMU!3D/1/136/10! 1 ! 1 ! 28 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!157! 1 ! 12 ! 12 ! City pair FROM ! FGC!01/1/040 ! 1 !1/4! 20 !
! ! ! ! ! ! FGC!01/2/040 ! ! ! !
! ! ! ! ! City pair FROM ! FGC!01/1/040 ! 2 !1/4! 29 !
! ! ! ! ! ! FGC!01/2/040 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!159! 1 ! 12 ! 12 ! City pair FROM / TO ! FGC!01/1/041 ! 1 !1/4! 20 !
! ! ! ! ! ! FGC!01/2/041 ! ! ! !
! ! 2 ! 9 ! 9 ! City pair FROM / TO ! FGC!01/1/041 ! 2 !1/4! 29 !
! ! ! ! ! ! FGC!01/2/041 ! ! ! !
! ! 3 ! 12 ! 12 ! City pair TO ! FGC!01/1/042 ! 1 !1/4! 20 !
! ! ! ! ! ! FGC!01/2/042 ! ! ! !
! ! 4 ! 9 ! 9 ! City pair TO ! FGC!01/1/042 ! 2 !1/4! 29 !
! ! ! ! ! ! FGC!01/2/042 ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!161! 1-4! 12 ! 12 ! Body axis YAW rate ! IRS!04/1/330/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS!04/2/330/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!162! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!163! 1-4! 12 ! 10 ! VC trends ! DMC!25/1/262/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC!25/2/262/10! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/271/11! 1 ! 1 ! 11 !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/2/271/11! 1 ! 1 ! 11 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!164! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!165! 1-4! 12 ! 10 ! Ground speed ! IRS!04/1/312/01! 1 ! 1 ! 26 !
! ! ! ! ! ! IRS!04/2/312/10! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/126/11! 1 ! 1 ! 14 !
! ! ! ! ! ! FWC!26/2/126/11! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 19 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!166! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!167! 1-4! 3 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 22 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 18 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1,3! 12 ! 1 ! Shown angle ! ADC!06/2/221/10! 1 !1/2! 29 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
! ! 1,3! 11 ! 8 ! Shown angle ! ADC!06/2/221/10! 2 !1/2! 27 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!168! 1-4! 12 ! 12 ! LH spoiler #1 Position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!169! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!170! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!171! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 20 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 11 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 12 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!173! 1-4! 12 ! 1 ! Elevator position right ! FCDC!6C/1/334/01!1 !1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/334/10! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position right ! FCDC!6C/1/334/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/334/10! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/017/10! 1 ! 1 ! 14 !
! ! ! ! ! ! FWC!26/2/017/10! ! ! !
! ! 1-4! 1 ! 1 ! FWC discrete status word ! FWC!26/1/017/01! 1 ! 1 ! 14 !
! ! ! ! ! ! FWC!26/2/017/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!175! 1-4! 12 ! 1 ! Capt pitch ! FCDC!6C/1/305/01! 1 ! 2 ! 29 !
! ! ! ! ! command position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch ! FCDC!6C/1/305/01! 2 ! 2 ! 25 !
! ! ! ! ! command position ! FCDC!6C/2/305/10! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 26 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 17 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 25 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!177! 1-4! 12 ! 1 ! F/O pitch command position! FCDC!6C/1/306/01! 1 ! 2 ! 29 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command position! FCDC!6C/1/306/01! 2 ! 2 ! 25 !
! ! ! ! ! ! FCDC!6C/2/306/10! ! ! !
! ! 1-4! 3 ! 1 ! WC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 29 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/017/10! 1 ! 1 ! 28 !
! ! ! ! ! ! FWC!26/2/017/10! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/017/01! 1 ! 1 ! 28 !
! ! ! ! ! ! FWC!26/2/017/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!178! 1-4! 12 ! 11 ! Approach speed target ! FGC!01/1/304/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FGC!01/2/304/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!179! 1-4! 12 ! 4 ! DMC bus: status word ! DMC!25/1/302/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC!25/2/302/10! ! ! !
! ! 1-4! 8 ! 7 ! DMC bus: status word ! DMC!25/1/301/01! 1 ! 1 ! 17 !
! ! ! ! ! ! DMC!25/2/301/10! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word ! DMC!25/1/300/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC!25/2/300/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!180! 1-4! 12 ! 10 ! GPWS discrete word #1 ! GPWS!23/1/270/00! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/302/01! 1 ! 1 ! 27 !
! ! ! ! ! ! DMC!25/2/302/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!181! 1-4! 11 ! 11 ! DMC bus: status word ! DMC!25/1/302/01! 1 ! 1 ! 25 !
! ! ! ! ! ! DMC!25/2/302/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!183! 1-4! 12 ! 10 ! N2 Actual (high rotor ! ECU/!7C/1/344/01! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! EEC ! ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/307/01! 1 ! 1 ! 15 !
! ! ! ! ! ! DMC!25/2/307/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!185! 1-4! 12 ! 12 ! Fuel mass flow rate ! ECU/!7C/1/244/01! 1 ! 1 ! 27 !
! ! ! ! ! engine #1 (in Kg) ! EEC ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!187! 1 ! 12 ! 9 ! WIND DIRECTION true ! IRS!04/1/316/01! 1 !1/4! 29 !
! ! ! ! ! ! IRS!04/2/316/10! ! ! !
! ! 1 ! 3 ! 3 ! DMC bus: status word ! DMC!25/1/307/01! 1 !1/4! 19 !
! ! ! ! ! ! DMC!25/2/307/10! ! ! !
! ! 2 ! 12 ! 12 ! Altitude baro setting F/O ! DMC!25/1/223/01! 1 !1/4! 26 !
! ! ! ! ! ! DMC!25/2/223/10! ! ! !
! ! 3 ! 12 ! 1 ! Drift angle ! IRS!04/1/321/01! 1 !1/4! 29 !
! ! ! ! ! ! IRS!04/2/321/10! ! ! !
! ! 3 ! 11 ! 9 ! Drift angle ! IRS!04/1/321/01! 2 !1/4! 26 !
! ! ! ! ! ! IRS!04/2/321/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!189! 1-4! 12 ! 7 ! FLAP actual position ! SFCC!1B/1/137/01! 1 ! 1 ! 17 !
! ! ! ! ! -conf command system #1 ! ! ! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting F/O ! DMC!25/1/223/01! 2 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/223/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!191! 1-4! 12 ! 1 ! Selected FPA ! DMC!25/1/115/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/115/10! ! ! !
! ! 1-4! 11 ! 7 ! Selected FPA ! DMC!25/1/115/01! 2 ! 1 ! 24 !
! ! ! ! ! ! DMC!25/2/115/10! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: status word ! DMC!25/1/270/01! 1 ! 1 ! 24 !
! ! ! ! ! ! DMC!25/2/270/10! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: ! FCDC!6C/1/043/01! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 ! FCDC!6C/2/043/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!129! 1-4! 12 ! 12 ! Body axis roll rate !IRS !04/1/327/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/327/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!130! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!131! 1-4! 12 ! 10 ! RH spoiler #2 position !FCDC !6C/1/372/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/372/10 ! ! ! !
! ! 1 ! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 !1/4! 12 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: status word !DMC !25/1/270/01 ! 1 !1/4! 16 !
! ! ! ! ! (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 3 ! 1 ! 1 ! AC2 bus off !SDAC !29/1/002/10 ! 1 !1/4! 20 !
! ! ! ! ! !SDAC !29/2/002/10 ! ! ! !
! ! 4 ! 2 ! 1 ! DC2 bus off !SDAC !29/1/004/10 ! 1 !1/4! 29 !
! ! ! ! ! !SDAC !29/2/004/10 ! ! ! !
! ! 4 ! 1 ! 1 ! DC1 bus off !SDAC !29/1/004/01 ! 1 !1/4! 29 !
! ! ! ! ! !SDAC !29/2/004/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!132! 1-4! 12 ! 12 ! FD Roll Order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!133! 1-4! 12 ! 10 ! RH spoiler #3 position !FCDC !6C/1/373/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/373/10 ! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/272/01 ! 1 !1/4! 16 !
! ! ! ! ! word (label 272) !DMC !25/2/272/10 ! ! ! !
! ! 1 ! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 !1/4! 13 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 !1/4! 26 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 3 ! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/305/01 ! 1 !1/4! 29 !
! ! ! ! ! word (label 305) !DMC !25/2/305/10 ! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 25 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 26 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!134! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!135! 1-4! 12 ! 10 ! RH spoiler #5 position !FCDC !6C/1/375/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/375/10 ! ! ! !
! ! 1 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 19 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 1 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 20 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 21 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 22 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 23 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 24 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 29 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!136! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/143/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!137! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!139! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 1 ! Eng2 HP fuel valve closed!FWC !26/1/011/10 ! 1 ! 1 ! 14 !
! ! ! ! ! !FWC !26/2/011/10 ! ! ! !
! ! 1-4! 2 ! 1 ! Eng1 HP fuel valve closed!FWC !26/1/011/01 ! 1 ! 1 ! 14 !
! ! ! ! ! !FWC !26/2/011/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!140! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label-015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: !FCDC !6C/1/041/01 ! 1 ! 4 ! 20 !
! ! ! ! ! EFCS status word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!141! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 2 ! 1 ! Fuel fire valve engine #2!SDAC !29/1/001/10 ! 1 ! 1 ! 19 !
! ! ! ! ! fully closed !SDAC !29/2/001/10 ! ! ! !
! ! 1-4! 1 ! 1 ! Fuel fire valve engine #1!SDAC !29/1/001/01 ! 1 ! 1 ! 19 !
! ! ! ! ! fully closed !SDAC !29/2/001/01 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!143! 1-4! 12 ! 12 ! True heading !IRS !04/1/314/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/314/10 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!145! 1-4! 12 ! 1 ! Throttle resolver !EIU !7B/2/133/xx ! 1 ! 1 ! 29 !
! ! ! ! ! angle engine #2 ! ! ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver !EIU !7B/2/133/xx ! 2 ! 1 ! 27 !
! ! ! ! ! angle engine #2 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!146! 1-4! 12 ! 12 ! FMGC discrete !FGC !01/1/273/00 ! 1 ! 1 ! 25 !
! ! ! ! ! status word #3 !FGC !01/2/273/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!147! 1-4! 12 ! 5 ! FMGC discrete !FGC !01/1/274/00 ! 1 ! 1 ! 27 !
! ! ! ! ! status word #1 !FGC !01/2/274/00 ! ! ! !
! ! 1-4! 2 ! 2 ! FMGC discrete !FGC !01/1/273/00 ! 1 ! 1 ! 13 !
! ! ! ! ! status word #3 !FGC !01/2/273/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!149! 1-4! 12 ! 10 ! N1 Actual (low rotor !EIU !7B/2/331/xx ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/11 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=11) !FWC !26/2/017/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/11 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=017 SDI=11) !FWC !26/2/017/11 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!151! 1-4! 12 ! 10 ! EGT LPT exit !EIU !7B/2/345/xx ! 1 ! 1 ! 27 !
! ! ! ! ! exit temp engine 2# ! ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/00 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=17 SDI=00) !FWC !26/2/017/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/00 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=17 SDI=00) !FWC !26/2/017/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!153! ! ! ! Spare ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!155! 1-4! 12 ! 6 ! N1 vibration eng #2 !EIU !7B/2/135/XX ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #2 !EIU !7B/2/136/XX ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!157! 1 ! 12 ! 12 ! City pair FROM !FGC !01/1/040 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/040 ! ! ! !
! ! 2 ! 9 ! 9 ! City pair FROM !FGC !01/1/040 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/040 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!159! 1 ! 12 ! 12 ! City pair FROM / TO !FGC !01/1/041 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/041 ! ! ! !
! ! 2 ! 9 ! 9 ! City pair FROM / TO !FGC !01/1/041 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/041 ! ! ! !
! ! 3 ! 12 ! 12 ! City pair TO !FGC !01/1/042 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/042 ! ! ! !
! ! 4 ! 9 ! 9 ! City pair TO !FGC !01/1/042 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/042 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!161! 1-4! 12 ! 12 ! Body axis YAW rate !IRS !04/1/330/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/330/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!162! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!163! 1-4! 12 ! 10 ! VC trends !DMC !25/1/262/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/262/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/271/11 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=11) ! ! ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/2/271/11 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=11) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!164! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!165! 1-4! 12 ! 10 ! Ground speed !IRS !04/1/312/01 ! 1 ! 1 ! 26 !
! ! ! ! ! !IRS !04/2/312/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 19 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!166! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!167! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 22 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 18 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1,3! 12 ! 1 ! Indicated angle !ADC !06/2/221/10 ! 1 !1/2! 29 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
! ! 1,3! 11 ! 8 ! Indicated angle !ADC !06/2/221/10 ! 2 !1/2! 27 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!168! 1-4! 12 ! 12 ! LH spoiler #1 Position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!169! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!170! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!171! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 12 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!173! 1-4! 12 ! 1 ! Elevator position right !FCDC !6C/1/334/01 !1 !1 ! 29 !
! ! ! ! ! !FCDC !6C/2/334/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position right !FCDC !6C/1/334/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/334/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/10 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=017 SDI=10) !FWC !26/2/017/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC discrete status word !FWC !26/1/017/01 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=017 SDI=01) !FWC !26/2/017/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!175! 1-4! 12 ! 1 ! Capt pitch !FCDC !6C/1/305/01 ! 1 ! 2 ! 29 !
! ! ! ! ! command position !FCDC !6C/2/305/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch !FCDC !6C/1/305/01 ! 2 ! 2 ! 25 !
! ! ! ! ! command position !FCDC !6C/2/305/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 26 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 17 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 25 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!177! 1-4! 12 ! 1 ! F/O pitch command !FCDC !6C/1/306/01 ! 1 ! 2 ! 29 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command !FCDC !6C/1/306/01 ! 2 ! 2 ! 25 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 3 ! 1 ! WC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 29 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/10 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=10) !FWC !26/2/017/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/01 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=01) !FWC !26/2/017/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!178! 1-4! 12 ! 11 ! Approach speed target !FGC !01/1/304/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FGC !01/2/304/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!179! 1-4! 12 ! 4 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
! ! 1-4! 8 ! 7 ! DMC bus: Discrete status !DMC !25/1/301/01 ! 1 ! 1 ! 17 !
! ! ! ! ! word (label 300) !DMC !25/2/301/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: status word !DMC !25/1/300/01 ! 1 ! 1 ! 14 !
! ! ! ! ! !DMC !25/2/300/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!180! 1-4! 12 ! 10 ! GPWS discrete word #1 !GPWS !23/1/270/00 ! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 27 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!181! 1-4! 11 ! 11 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 25 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!183! 1-4! 12 ! 10 ! N2 Actual (high rotor !EIU !7B/1/344/xx ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 ! ! ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/307/01 ! 1 ! 1 ! 15 !
! ! ! ! ! word (label 307) !DMC !25/2/307/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!185! 1-4! 12 ! 12 ! Fuel mass flow rate !EIU !7B/1/244/xx ! 1 ! 1 ! 27 !
! ! ! ! ! engine #1 (in Kg) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!187! 1 ! 12 ! 9 ! WIND DIRECTION true !IRS !04/1/316/01 ! 1 !1/4! 29 !
! ! ! ! ! !IRS !04/2/316/10 ! ! ! !
! ! 1 ! 3 ! 3 ! DMC bus: Discrete status !DMC !25/1/307/01 ! 1 !1/4! 19 !
! ! ! ! ! (label 307) !DMC !25/2/307/10 ! ! ! !
! ! 2 ! 12 ! 12 ! Altitude baro setting F/O!DMC !25/1/223/01 ! 1 !1/4! 26 !
! ! ! ! ! !DMC !25/2/223/10 ! ! ! !
! ! 3 ! 12 ! 1 ! Drift angle !IRS !04/1/321/01 ! 1 !1/4! 29 !
! ! ! ! ! !IRS !04/2/321/10 ! ! ! !
! ! 3 ! 11 ! 9 ! Drift angle !IRS !04/1/321/01 ! 2 !1/4! 26 !
! ! ! ! ! !IRS !04/2/321/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!189! 1-4! 12 ! 7 ! FLAP actual position !SFCC !1B/1/137/01 ! 1 ! 1 ! 17 !
! ! ! ! ! -conf command system #1 ! ! ! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting F/O!DMC !25/1/223/01 ! 2 !1/4! 27 !
! ! ! ! ! !DMC !25/2/223/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!191! 1-4! 12 ! 1 ! Selected FPA !DMC !25/1/115/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/115/10 ! ! ! !
! ! 1-4! 11 ! 7 ! Selected FPA !DMC !25/1/115/01 ! 2 ! 1 ! 24 !
! ! ! ! ! !DMC !25/2/115/10 ! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 ! 1 ! 24 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
+---+----+----+----+--------------------------+------------------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!129! 1-4! 12 ! 12 ! Body axis roll rate !IRS !04/1/327/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/327/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!130! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!131! 1-4! 12 ! 10 ! RH spoiler #2 position !FCDC !6C/1/372/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/372/10 ! ! ! !
! ! 1 ! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 !1/4! 12 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 !1/4! 16 !
! ! ! ! ! (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 3 ! 1 ! 1 ! AC2 bus off !SDAC !29/1/002/10 ! 1 !1/4! 20 !
! ! ! ! ! !SDAC !29/2/002/10 ! ! ! !
! ! 4 ! 2 ! 1 ! DC2 bus off !SDAC !29/1/004/10 ! 1 !1/4! 29 !
! ! ! ! ! !SDAC !29/2/004/10 ! ! ! !
! ! 4 ! 1 ! 1 ! DC1 bus off !SDAC !29/1/004/01 ! 1 !1/4! 29 !
! ! ! ! ! !SDAC !29/2/004/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!132! 1-4! 12 ! 12 ! FD Roll Order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!133! 1-4! 12 ! 10 ! RH spoiler #3 position !FCDC !6C/1/373/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/373/10 ! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/272/01 ! 1 !1/4! 16 !
! ! ! ! ! word (label 272) !DMC !25/2/272/10 ! ! ! !
! ! 1 ! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 !1/4! 13 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 2 ! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 !1/4! 26 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 3 ! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/305/01 ! 1 !1/4! 29 !
! ! ! ! ! word (label 305) !DMC !25/2/305/10 ! ! ! !
! ! 4 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 25 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 26 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!134! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!135! 1-4! 12 ! 10 ! RH spoiler #5 position !FCDC !6C/1/375/01 ! 1 ! 1 ! 27 !
! ! ! ! ! !FCDC !6C/2/375/10 ! ! ! !
! ! 1 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 19 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 1 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 20 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 21 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 2 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 22 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 2 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 23 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 3 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 24 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
! ! 4 ! 1 ! 1 ! FCDC bus: !FCDC !6C/1/040/01 ! 1 !1/4! 29 !
! ! ! ! ! EFCS status word #1 !FCDC !6C/2/040/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!136! 1-4! 12 ! 12 ! FD Pitch Order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/143/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!137! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!139! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 1 ! Eng2 HP fuel valve closed!FWC !26/1/011/10 ! 1 ! 1 ! 14 !
! ! ! ! ! !FWC !26/2/011/10 ! ! ! !
! ! 1-4! 1 ! 1 ! Eng1 HP fuel valve closed!FWC !26/1/011/01 ! 1 ! 1 ! 14 !
! ! ! ! ! !FWC !26/2/011/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!140! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label-015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: !FCDC !6C/1/041/01 ! 1 ! 4 ! 20 !
! ! ! ! ! EFCS status word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!141! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 2 ! 1 ! Fuel fire valve engine #2!SDAC !29/1/001/10 ! 1 ! 1 ! 19 !
! ! ! ! ! fully closed !SDAC !29/2/001/10 ! ! ! !
! ! 1-4! 1 ! 1 ! Fuel fire valve engine #1!SDAC !29/1/001/01 ! 1 ! 1 ! 19 !
! ! ! ! ! fully closed !SDAC !29/2/001/01 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!143! 1-4! 12 ! 12 ! True heading !IRS !04/1/314/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/314/10 ! ! ! !
!---!----!----!----!--------------------------!-----!----------- !---!---!----!
!145! 1-4! 12 ! 1 ! Throttle resolver !ECU/ !7C/2/133/10 ! 1 ! 1 ! 29 !
! ! ! ! ! angle engine #2 !EEC ! ! ! ! !
! ! 1-4! 11 ! 5 ! Throttle resolver !ECU/ !7C/2/133/10 ! 2 ! 1 ! 27 !
! ! ! ! ! angle engine #2 !EEC ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!146! 1-4! 12 ! 12 ! FMGC discrete !FGC !01/1/273/00 ! 1 ! 1 ! 25 !
! ! ! ! ! status word #3 !FGC !01/2/273/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!147! 1-4! 12 ! 5 ! FMGC discrete !FGC !01/1/274/00 ! 1 ! 1 ! 27 !
! ! ! ! ! status word #1 !FGC !01/2/274/00 ! ! ! !
! ! 1-4! 2 ! 2 ! FMGC discrete !FGC !01/1/273/00 ! 1 ! 1 ! 13 !
! ! ! ! ! status word #3 !FGC !01/2/273/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!149! 1-4! 12 ! 10 ! N1 Actual (low rotor !ECU/ !7C/2/346/10 ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #2 !EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/11 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=11) !FWC !26/2/017/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/11 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=017 SDI=11) !FWC !26/2/017/11 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!151! 1-4! 12 ! 10 ! EGT LPT exit !ECU/ !7C/2/345/10 ! 1 ! 1 ! 27 !
! ! ! ! ! exit temp engine 2# !EEC ! ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/00 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=17 SDI=00) !FWC !26/2/017/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/00 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=17 SDI=00) !FWC !26/2/017/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!153! 1-4! 12 ! 10 ! EPR Actual engine #2 !EEC !7C/2/340//10! 1 ! 1 ! 27 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!155! 1-4! 12 ! 6 ! N1 vibration eng #2 !EVMU !3D/1/135/10 ! 1 ! 1 ! 28 !
! ! 1-4! 6 ! 6 ! N2 vibration eng #2 !EVMU !3D/1/136/10 ! 1 ! 1 ! 28 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!157! 1 ! 12 ! 12 ! City pair FROM !FGC !01/1/040 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/040 ! ! ! !
! ! 2 ! 9 ! 9 ! City pair FROM !FGC !01/1/040 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/040 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!159! 1 ! 12 ! 12 ! City pair FROM / TO !FGC !01/1/041 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/041 ! ! ! !
! ! 2 ! 9 ! 9 ! City pair FROM / TO !FGC !01/1/041 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/041 ! ! ! !
! ! 3 ! 12 ! 12 ! City pair TO !FGC !01/1/042 ! 1 !1/4! 20 !
! ! ! ! ! !FGC !01/2/042 ! ! ! !
! ! 4 ! 9 ! 9 ! City pair TO !FGC !01/1/042 ! 2 !1/4! 29 !
! ! ! ! ! !FGC !01/2/042 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!161! 1-4! 12 ! 12 ! Body axis YAW rate !IRS !04/1/330/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/330/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!162! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!163! 1-4! 12 ! 10 ! VC trends !DMC !25/1/262/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/262/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/271/11 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=11) ! ! ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/2/271/11 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=11) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!164! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!165! 1-4! 12 ! 10 ! Ground speed !IRS !04/1/312/01 ! 1 ! 1 ! 26 !
! ! ! ! ! !IRS !04/2/312/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 19 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!166! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!167! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 22 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 18 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1,3! 12 ! 1 ! Indicated angle !ADC !06/2/221/10 ! 1 !1/2! 29 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
! ! 1,3! 11 ! 8 ! Indicated angle !ADC !06/2/221/10 ! 2 !1/2! 27 !
! ! ! ! ! of attack system #2 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!168! 1-4! 12 ! 12 ! LH spoiler #1 Position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!169! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!170! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!171! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 12 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!173! 1-4! 12 ! 1 ! Elevator position right !FCDC !6C/1/334/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/334/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Elevator position right !FCDC !6C/1/334/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/334/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/10 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=017 SDI=10) !FWC !26/2/017/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC discrete status word !FWC !26/1/017/01 ! 1 ! 1 ! 14 !
! ! ! ! ! (Label=017 SDI=01) !FWC !26/2/017/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!175! 1-4! 12 ! 1 ! Capt pitch !FCDC !6C/1/305/01 ! 1 ! 2 ! 29 !
! ! ! ! ! command position !FCDC !6C/2/305/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Capt pitch !FCDC !6C/1/305/01 ! 2 ! 2 ! 25 !
! ! ! ! ! command position !FCDC !6C/2/305/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 26 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 17 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 25 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!177! 1-4! 12 ! 1 ! F/O pitch command !FCDC !6C/1/306/01 ! 1 ! 2 ! 29 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 11 ! 8 ! F/O pitch command !FCDC !6C/1/306/01 ! 2 ! 2 ! 25 !
! ! ! ! ! position !FCDC !6C/2/306/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 29 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/017/10 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=10) !FWC !26/2/017/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/017/01 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=017 SDI=01) !FWC !26/2/017/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!178! 1-4! 12 ! 11 ! Approach speed target !FGC !01/1/304/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FGC !01/2/304/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!179! 1-4! 12 ! 4 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
! ! 1-4! 8 ! 7 ! DMC bus: Discrete status !DMC !25/1/301/01 ! 1 ! 1 ! 17 !
! ! ! ! ! word (label 301) !DMC !25/2/301/10 ! ! ! !
! ! 1-4! 1 ! 1 ! DMC bus: Discrete status !DMC !25/1/300/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 300) !DMC !25/2/300/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!180! 1-4! 12 ! 10 ! GPWS discrete word #1 !GPWS !23/1/270/00 ! 1 ! 1 ! 20 !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 27 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!181! 1-4! 11 ! 11 ! DMC bus: Discrete status !DMC !25/1/302/01 ! 1 ! 1 ! 25 !
! ! ! ! ! word (label 302) !DMC !25/2/302/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!183! 1-4! 12 ! 10 ! N2 Actual (high rotor !ECU/ !7C/1/344/01 ! 1 ! 1 ! 27 !
! ! ! ! ! speed) engine #1 !EEC ! ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/307/01 ! 1 ! 1 ! 15 !
! ! ! ! ! word (label 307) !DMC !25/2/307/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!185! 1-4! 12 ! 12 ! Fuel mass flow rate !ECU/ !7C/1/244/01 ! 1 ! 1 ! 27 !
! ! ! ! ! engine #1 (in Kg) !EEC ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!187! 1 ! 12 ! 9 ! WIND DIRECTION true !IRS !04/1/316/01 ! 1 !1/4! 29 !
! ! ! ! ! !IRS !04/2/316/10 ! ! ! !
! ! 1 ! 3 ! 3 ! DMC bus: Discrete status !DMC !25/1/307/01 ! 1 !1/4! 19 !
! ! ! ! ! (label 307) !DMC !25/2/307/10 ! ! ! !
! ! 2 ! 12 ! 12 ! Altitude baro setting F/O!DMC !25/1/223/01 ! 1 !1/4! 26 !
! ! ! ! ! !DMC !25/2/223/10 ! ! ! !
! ! 3 ! 12 ! 1 ! Drift angle !IRS !04/1/321/01 ! 1 !1/4! 29 !
! ! ! ! ! !IRS !04/2/321/10 ! ! ! !
! ! 3 ! 11 ! 9 ! Drift angle !IRS !04/1/321/01 ! 2 !1/4! 26 !
! ! ! ! ! !IRS !04/2/321/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!189! 1-4! 12 ! 7 ! FLAP actual position !SFCC !1B/1/137/01 ! 1 ! 1 ! 17 !
! ! ! ! ! -conf command system #1 ! ! ! ! ! !
! ! 2 ! 1 ! 1 ! Altitude baro setting F/O!DMC !25/1/223/01 ! 2 !1/4! 27 !
! ! ! ! ! !DMC !25/2/223/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!191! 1-4! 12 ! 1 ! Selected FPA !DMC !25/1/115/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/115/10 ! ! ! !
! ! 1-4! 11 ! 7 ! Selected FPA !DMC !25/1/115/01 ! 2 ! 1 ! 24 !
! ! ! ! ! !DMC !25/2/115/10 ! ! ! !
! ! 1-4! 4 ! 1 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 ! 1 ! 24 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 27 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 11 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
! ! 1-4! 1 ! 1 ! FCDC bus: !FCDC !6C/1/043/01 ! 1 ! 2 ! 12 !
! ! ! ! ! EFCS status word #4 !FCDC !6C/2/043/10 ! ! ! !
+---+----+----+----+--------------------------+------------------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

I. DAR Frame Assignment (Word 193-256)
+---+----+----+----+---------------------------+-----------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! Z ! B !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!193! 1-4! 12 ! 12 ! Stall speed ! FAC!0A/1/246/00! 1 ! 2 ! 28 !
! ! ! ! ! ! FAC!0A/2/246/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!194! 1-4! 12 ! 12 ! Body axis pitch rate ! IRS!04/1/326/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/326/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!195! 1,3! 12 ! 12 ! Runway heading ! DMC!25/1/105/01! 1 !1/2! 29 !
! ! ! ! ! ! DMC!25/2/105/01! ! ! !
! ! 2,4! 12 ! 12 ! Landing speed ! DMC!25/1/245/01! 1 !1/2! 28 !
! ! ! ! ! ! DMC!25/2/245/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!196! 1-4! 12 ! 12 ! FD Roll Order ! FGC!01/1/140/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/140/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!197! 1-4! 12 ! 12 ! Track angle true ! IRS!04/1/313/01! 1 ! 1 ! 29 !
! ! ! ! ! ! IRS!04/2/313/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!198! 1-4! 12 ! 12 ! FD pitch Order ! FGC!01/1/141/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/141/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!199! 1-4! 12 ! 12 ! Flight path angle ! DMC!25/1/322/xx! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/322/xx! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!200! 1-4! 12 ! 12 ! FD pitch Order ! FGC!01/1/143/00! 1 ! 4 ! 29 !
! ! ! ! ! ! FGC!01/2/143/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!201! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!203! 1-4! 12 ! 1 ! Longitudinal acceleration ! SDAC!29/1/331/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration ! SDAC!29/1/331/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/331/01! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/270/01! 1 ! 1 ! 12 !
! ! ! ! ! ! DMC!25/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!204! 1-4! 12 ! 10 ! FWC Discrete status word ! FWC!26/1/015/10! 1 ! 4 ! 23 !
! ! ! ! ! ! FWC!26/2/015/10! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: ! FCDC!6C/1/041/01! 1 ! 4 ! 20 !
! ! ! ! ! EFCS status word #2 ! FCDC!6C/2/041/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!205! 1-4! 12 ! 1 ! Lateral acceleration ! SDAC!29/1/332/01! 1 ! 4 ! 29 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration ! SDAC!29/1/332/01! 2 ! 4 ! 27 !
! ! ! ! ! ! SDAC!29/2/332/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!206! 1-4! 2 ! 2 ! DMC bus: status word ! DMC!25/1/270/01! 1 ! 1 ! 14 !
! ! ! ! ! ! DMC!25/2/270/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!207! 1-4! 12 ! 1 ! Aileron position right ! FCDC!6C/1/330/01! 1 ! 1 ! 29 !
! ! ! ! ! ! FCDC!6C/2/330/10! ! ! !
! ! 1-4! 11 ! 9 ! Aileron position right ! FCDC!6C/1/330/01! 2 ! 1 ! 26 !
! ! ! ! ! ! FCDC!6C/2/330/10! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/271/00! 1 ! 1 ! 11 !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/2/271/00! 1 ! 1 ! 11 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!209! 1-4! 12 ! 12 ! DMC bus: status word ! DMC!25/1/306/01! 1 ! 1 ! 29 !
! ! ! ! ! ! DMC!25/2/306/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!210! 1-4! 12 ! 11 ! Low Target Speed Margin ! FGC!01/1/306/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FGC!01/2/306/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!211! 1-4! 12 ! 12 ! Brake 1 temperature ! BSCU!6E/1/114/01! 1 ! 1 ! 29 !
! ! ! ! ! ! BSCU!6E/2/114/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!212! 1-4! 12 ! 8 ! GPWS discrete word #1 ! GPWS!23/1/271/00! 1 ! 1 ! 25 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!213! 1-4! 12 ! 12 ! Brake 2 temperature ! BSCU!6E/1/115/01! 1 ! 1 ! 29 !
! ! ! ! ! ! BSCU!6E/2/115/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!215! 1-4! 12 ! 12 ! Brake 3 temperature ! BSCU!6E/1/116/01! 1 ! 1 ! 29 !
! ! ! ! ! ! BSCU!6E/2/116/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!217! 1-4! 12 ! 12 ! Brake 4 temperature ! BSCU!6E/1/117/01! 1 ! 1 ! 29 !
! ! ! ! ! ! BSCU!6E/2/117/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!221! 1-4! 12 ! 7 ! FLAP actual position ! SFCC!1B/2/137/10! 1 ! 1 ! 17 !
! ! ! ! ! -conf command system #2 ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!225! 1,3! 12 ! 1 ! Altitude (1013.25mb) ! ADC!06/1/203/01! 1 !1/2! 29 !
! ! ! ! ! (switched parameter) ! ADC!06/2/203/10! ! ! !
! ! 1,3! 11 ! 3 ! Altitude (1013.25mb) ! ADC!06/1/203/01! 2 !1/2! 27 !
! ! ! ! ! (switched parameter) ! ADC!06/2/203/10! ! ! !
! ! 1,3! 8 ! 8 ! FLAP actual position ! SFCC!1B/1/137/01! 1 !1/2! 29 !
! ! ! ! ! (FPPU angle value) ! SFCC!1B/2/137/10! ! ! !
! ! 2 ! 12 ! 12 ! DAR frame counter ! DMU! ! 1 !1/4! 12 !
! ! ! ! ! (DMU computed) ! ! ! ! ! !
! ! 4 ! 12 ! 6 ! UTC (Universal time ! FDIU!17/1/150/00! 1 !1/4! 23 !
! ! ! ! ! coordinated BNR) ! ! ! ! ! !
! ! 4 ! 6 ! 6 ! UTC (Universal time ! FDIU!17/1/150/00! 2 !1/4! 17 !
! ! ! ! ! coordinated BNR) ! ! ! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!226! 1-4! 12 ! 11 ! NWS reference angle ! BSCU!6E/1/336/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/336/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!227! 1-4! 12 ! 12 ! Altitude (1013.25mb) ! ADC!06/1/203/01! 1 ! 1 ! 25 !
! ! ! ! ! (switched parameter) ! ADC!06/2/203/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!228! 1-4! 12 ! 11 ! Steering command captain ! BSCU!6E/1/340/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/340/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!229! 2,4! 12 ! 1 ! Total air temperature ! ADC!06/1/211/01! 1 !1/2! 29 !
! ! ! ! ! (BNR)(switched parameter) ! ADC!06/2/211/10! ! ! !
! ! 2,4! 11 ! 9 ! Total air temperature ! ADC!06/1/211/01! 2 !1/2! 26 !
! ! ! ! ! (BNR)(switched parameter) ! ADC!06/2/211/10! ! ! !
! ! 1 ! 12 ! 11 ! Present position latitude ! IRS!04/1/310/ ! 3 !1/4! 20 !
! ! ! ! ! ! IRS!04/2/310/ ! ! ! !
! ! 1 ! 1 ! 1 ! gear lever selected up !LGCIU!6D/1/022/01! 1 !1/4! 14 !
! ! ! ! ! !LGCIU!6D/2/022/10! ! ! !
! ! 3 ! 12 ! 11 ! Present position longitude! IRS!04/1/311/ ! 1 !1/4! 21 !
! ! ! ! ! ! IRS!04/2/311/ ! ! ! !
! ! 3 ! 1 ! 1 ! Gear selected down !LGCIU!6D/1/020/01! 1 !1/4! 29 !
! ! ! ! ! (lever position) !LGCIU!6D/2/020/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!230! 1-4! 12 ! 11 ! Steering command F/O ! BSCU!6E/1/341/01! 1 ! 4 ! 29 !
! ! ! ! ! ! BSCU!6E/2/341/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!231! 1-4! 12 ! 6 ! FWC Discrete status word ! FWC!26/1/146/01! 1 ! 1 ! 25 !
! ! ! ! ! ! FWC!26/2/146/01! ! ! !
! ! 1-4! 6 ! 2 ! FWC Discrete status word ! FWC!26/1/126/11! 1 ! 1 ! 23 !
! ! ! ! ! ! FWC!26/2/126/11! ! ! !
! ! 1-4! 4 ! 2 ! FWC Discrete status word ! FWC!26/1/126/11! 1 ! 1 ! 15 !
! ! ! ! ! ! FWC!26/2/126/11! ! ! !
! ! 1-4! 2 ! 1 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 14 !
! ! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 273/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 13 !
! ! ! ! ! ! ! 273/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 273/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!232! 1-4! 12 ! 12 ! LH spoiler #1 position ! FCDC!6C/1/361/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/361/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!233! 1-4! 12 ! 12 ! Normal acceleration ! SDAC!29/1/333/01! 1 ! 8 ! 29 !
! ! ! ! ! ! SDAC!29/2/333/01! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!234! 1-4! 12 ! 12 ! RH spoiler #1 position ! FCDC!6C/1/371/01! 1 ! 4 ! 29 !
! ! ! ! ! ! FCDC!6C/2/371/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!235! 1-4! 12 ! 1 ! Pitch angle ! IRS!04/1/324/01! 1 ! 4 ! 29 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle ! IRS!04/1/324/01! 2 ! 4 ! 27 !
! ! ! ! ! ! IRS!04/2/324/10! ! ! !
! ! 1,3! 3 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 !1/2! 23 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1,3! 2 ! 2 ! FWC Discrete status word ! FWC!26/1/126/00! 1 !1/2! 25 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!237! 1-4! 12 ! 10 ! ROLL angle ! IRS!04/1/325/01! 1 ! 2 ! 29 !
! ! ! ! ! ! IRS!04/2/325/10! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 2 ! 16 !
! ! ! ! ! ! FWC!26/2/216/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!239! 1-4! 12 ! 1 ! Rudder position ! SDAC!29/1/312/00! 1 ! 2 ! 29 !
! ! ! ! ! ! SDAC!29/2/312/00! ! ! !
! ! 1-4! 11 ! 9 ! Rudder position ! SDAC!29/1/312/00! 2 ! 2 ! 26 !
! ! ! ! ! ! SDAC!29/2/312/00! ! ! !
! ! 1-4! 1 ! 1 ! EVENT button pressed ! FDIU!17/1/350/00! 1 ! 1 ! 16 !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!242! 1-4! 12 ! 11 ! HIgh Target Speed Margin ! FGC!01/1/307/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FGC!01/2/307/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!243! 1-4! 12 ! 12 ! FMC status word: ATS FMA ! FMC!02/1/271/00! 1 ! 1 ! 28 !
! ! ! ! ! ! FMC!02/2/271/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!244! 1-4! 12 ! 6 ! FMC status word: ATS FMA ! FMC!02/1/271/00! 1 ! 1 ! 16 !
! ! ! ! ! ! FMC!02/2/271/00! ! ! !
! ! 1-4! 3 ! 3 ! FMC status word: ATS FMA ! FMC!02/1/270/00! 1 ! 1 ! 13 !
! ! ! ! ! ! FMC!02/2/270/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!247! 1-4! 12 ! 9 ! Approach speed target ! DMC!25/1/304/01! 1 ! 1 ! 28 !
! ! 1-4! 3 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 20 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 11 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word ! FWC!26/1/126/00! 1 ! 1 ! 12 !
! ! ! ! ! ! FWC!26/2/126/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!249! 1-4! 12 ! 9 ! Selected Mach / Manual ! DMC!25/1/106/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC!25/2/106/10! ! ! !
! ! 1-4! 3 ! 1 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 19 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 2 ! 1 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 16 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word ! FCU!A1/1A/ ! 1 ! 1 ! 14 !
! ! ! ! ! ! ! 274/00! ! ! !
! ! ! ! ! ! FCU!A1/1B/ ! ! ! !
! ! ! ! ! ! ! 274/00! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!251! 1 ! 12 ! 8 ! DME 2 distance ! DMC!25/1/202/10! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/202/10! ! ! !
! ! 2 ! 12 ! 9 ! VOR 2 frequency ! DMC!25/1/034/10! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/034/10! ! ! !
! ! 2 ! 3 ! 3 ! VOR 2 frequency ! DMC!25/1/034/10! 2 !1/4! 17 !
! ! ! ! ! ! DMC!25/2/034/10! ! ! !
! ! 3 ! 12 ! 9 ! ILS 2 frequency ! DMC!25/1/033/10! 1 !1/4! 27 !
! ! ! ! ! ! DMC!25/2/033/10! ! ! !
! ! 3 ! 3 ! 3 ! ILS 2 frequency ! DMC!25/1/033/10! 2 !1/4! 17 !
! ! ! ! ! ! DMC!25/2/033/10! ! ! !
! ! 4 ! 12 ! 11 ! DME 2 frequency ! DMC!25/1/035/10! 1 !1/4! 28 !
! ! ! ! ! ! DMC!25/2/035/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!253! 1-4! 12 ! 9 ! PFD selected speed ! DMC!25/1/103/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC!25/2/103/10! ! ! !
! ! 1 ! 3 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 !1/4! 13 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: status word ! DMC!25/1/271/01! 1 !1/4! 22 !
! ! ! ! ! ! DMC!25/2/271/10! ! ! !
!---!----!----!----!---------------------------!-----!-----------!---!---!----!
!255! 1-4! 12 ! 10 ! FMC altitude constraint ! DMC!25/1/163/01! 1 ! 1 ! 28 !
! ! ! ! ! ! DMC!25/2/163/10! ! ! !
+---+----+----+----+---------------------------+-----------------+---+----+---+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

+---+----+----+----+--------------------------+------------------+---+---+----+
! W ! S ! T ! L ! ! Source ! P ! R ! S !
! O ! U ! G ! E ! ! S ! L ! A ! A ! C !
! R ! B ! T ! N ! ! Y ! A ! R ! T ! E !
! D ! ! ! G ! Parameter Description ! S ! B ! T ! E ! !
! ! F ! M ! T ! ! T ! E ! ! ! M !
! ! R ! S ! H ! ! E ! L ! ! H ! S !
! ! ! B ! ! ! M ! ! ! z ! B !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!193! 1-4! 12 ! 12 ! Stall speed !FAC !0A/1/246/00 ! 1 ! 2 ! 28 !
! ! ! ! ! !FAC !0A/2/246/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!194! 1-4! 12 ! 12 ! Body axis pitch rate !IRS !04/1/326/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/326/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!195! 1,3! 12 ! 12 ! Runway heading !DMC !25/1/105/01 ! 1 !1/2! 29 !
! ! ! ! ! !DMC !25/2/105/01 ! ! ! !
! ! 2,4! 12 ! 12 ! Landing speed !DMC !25/1/245/01 ! 1 !1/2! 28 !
! ! ! ! ! !DMC !25/2/245/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!196! 1-4! 12 ! 12 ! FD Roll Order !FGC !01/1/140/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/140/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!197! 1-4! 12 ! 12 ! Track angle true !IRS !04/1/313/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !IRS !04/2/313/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!198! 1-4! 12 ! 12 ! FD pitch Order !FGC !01/1/141/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/141/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!199! 1-4! 12 ! 12 ! Flight path angle !DMC !25/1/322/xx ! 1 ! 1 ! 29 !
! ! ! ! ! !DMC !25/2/322/xx ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!200! 1-4! 12 ! 12 ! FD pitch Order !FGC !01/1/143/00 ! 1 ! 4 ! 29 !
! ! ! ! ! !FGC !01/2/143/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!201! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!203! 1-4! 12 ! 1 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Longitudinal acceleration!SDAC !29/1/331/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/331/01 ! ! ! !
! ! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 ! 1 ! 12 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!204! 1-4! 12 ! 10 ! FWC Discrete status word !FWC !26/1/015/10 ! 1 ! 4 ! 23 !
! ! ! ! ! (Label=015 SDI=10) !FWC !26/2/015/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FCDC bus: !FCDC !6C/1/041/01 ! 1 ! 4 ! 20 !
! ! ! ! ! EFCS status word #2 !FCDC !6C/2/041/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!205! 1-4! 12 ! 1 ! Lateral acceleration !SDAC !29/1/332/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
! ! 1-4! 11 ! 9 ! Lateral acceleration !SDAC !29/1/332/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !SDAC !29/2/332/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!206! 1-4! 2 ! 2 ! DMC bus: Discrete status !DMC !25/1/270/01 ! 1 ! 1 ! 14 !
! ! ! ! ! word (label 270) !DMC !25/2/270/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!207! 1-4! 12 ! 1 ! Aileron position right !FCDC !6C/1/330/01 ! 2 ! 1 ! 29 !
! ! ! ! ! !FCDC !6C/2/330/10 ! ! ! !
! ! 1-4! 11 ! 9 ! Aileron position right !FCDC !6C/1/330/01 ! 2 ! 1 ! 26 !
! ! ! ! ! !FCDC !6C/2/330/10 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/271/00 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=00) ! ! ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/2/271/00 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=0271 SDI=00) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!209! 1-4! 12 ! 12 ! DMC bus: Discrete status !DMC !25/1/306/01 ! 1 ! 1 ! 29 !
! ! ! ! ! word (label 306) !DMC !25/2/306/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!210! 1-4! 12 ! 11 ! Low Target Speed Margin !FGC !01/1/306/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FGC !01/2/306/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!211! 1-4! 12 ! 12 ! Brake 1 temperature !BSCU !6E/1/114/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !BSCU !6E/2/114/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!212! 1-4! 12 ! 8 ! GPWS discrete word #1 !GPWS !23/1/271/00 ! 1 ! 1 ! 25 !
! ! ! ! ! (Label: 271 SDI:00) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!213! 1-4! 12 ! 12 ! Brake 2 temperature !BSCU !6E/1/115/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !BSCU !6E/2/115/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!215! 1-4! 12 ! 12 ! Brake 3 temperature !BSCU !6E/1/116/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !BSCU !6E/2/116/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!217! 1-4! 12 ! 12 ! Brake 4 temperature !BSCU !6E/1/117/01 ! 1 ! 1 ! 29 !
! ! ! ! ! !BSCU !6E/2/117/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!221! 1-4! 12 ! 7 ! FLAP actual position !SFCC !1B/2/137/10 ! 1 ! 1 ! 17 !
! ! ! ! ! -conf command system #2 ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!225! 1,3! 12 ! 1 ! Altitude (1013.25mb) !ADC !06/1/203/01 ! 1 !1/2! 29 !
! ! ! ! ! (switched parameter) !ADC !06/2/203/10 ! ! ! !
! ! 1,3! 11 ! 3 ! Altitude (1013.25mb) !ADC !06/1/203/01 ! 2 !1/2! 27 !
! ! ! ! ! (switched parameter) !ADC !06/2/203/10 ! ! ! !
! ! 1,3! 8 ! 8 ! FLAP actual position !SFCC !1B/1/137/01 ! 1 !1/2! 29 !
! ! ! ! ! (FPPU angle value) !SFCC !1B/2/137/10 ! ! ! !
! ! 2 ! 12 ! 12 ! DAR frame counter !DMU ! ! 1 !1/4! 12 !
! ! ! ! ! (DMU computed) ! ! ! ! ! !
! ! 4 ! 12 ! 6 ! UTC (Universal time !FDIU !17/1/150/00 ! 1 !1/4! 23 !
! ! ! ! ! coordinated BNR) ! ! ! ! ! !
! ! 4 ! 6 ! 6 ! UTC (Universal time !FDIU !17/1/150/00 ! 2 !1/4! 17 !
! ! ! ! ! coordinated BNR) ! ! ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!226! 1-4! 12 ! 11 ! NWS reference angle !BSCU !6E/1/336/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/336/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!227! 1-4! 12 ! 12 ! Altitude (1013.25mb) !ADC !06/1/203/01 ! 1 ! 1 ! 25 !
! ! ! ! ! (switched parameter) !ADC !06/2/203/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!228! 1-4! 12 ! 11 ! Steering command captain !BSCU !6E/1/340/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/340/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!229! 2,4! 12 ! 1 ! Total air temperature !ADC !06/1/211/01 ! 1 !1/2! 29 !
! ! ! ! ! (BNR)(switched parameter)!ADC !06/2/211/10 ! ! ! !
! ! 2,4! 11 ! 9 ! Total air temperature !ADC !06/1/211/01 ! 2 !1/2! 26 !
! ! ! ! ! (BNR)(switched parameter)!ADC !06/2/211/10 ! ! ! !
! ! 1 ! 12 ! 11 ! Present position latitude!IRS !04/1/310/ ! 3 !1/4! 20 !
! ! ! ! ! !IRS !04/2/310/ ! ! ! !
! ! 1 ! 1 ! 1 ! Gear lever selected up !LGCIU!6D/1/022/01 ! 1 !1/4! 14 !
! ! ! ! ! !LGCIU!6D/2/022/10 ! ! ! !
! ! 3 ! 12 ! 11 ! Present position !IRS !04/1/311/ ! 1 !1/4! 21 !
! ! ! ! ! longitude !IRS !04/2/311/ ! ! ! !
! ! 3 ! 1 ! 1 ! Gear selected down !LGCIU!6D/1/020/01 ! 1 !1/4! 29 !
! ! ! ! ! (lever position) !LGCIU!6D/2/020/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!230! 1-4! 12 ! 11 ! Steering command F/O !BSCU !6E/1/341/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !BSCU !6E/2/341/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!231! 1-4! 12 ! 6 ! FWC Discrete status word !FWC !26/1/146/01 ! 1 ! 1 ! 25 !
! ! ! ! ! (Label=146 SDI=01) !FWC !26/2/146/01 ! ! ! !
! ! 1-4! 6 ! 2 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 23 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 4 ! 2 ! FWC Discrete status word !FWC !26/1/126/11 ! 1 ! 1 ! 15 !
! ! ! ! ! (Label=126 SDI=11) !FWC !26/2/126/11 ! ! ! !
! ! 1-4! 2 ! 1 ! FCU Discrete status word !FCU !A1/1A/273/00! 1 ! 1 ! 14 !
! ! ! ! ! (Label=273 SDI=00) !FCU !A1/1B/273/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word !FCU !A1/1A/273/00! 1 ! 1 ! 13 !
! ! ! ! ! (Label=273 SDI=00) !FCU !A1/1B/273/00! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!232! 1-4! 12 ! 12 ! LH spoiler #1 position !FCDC !6C/1/361/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/361/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!233! 1-4! 12 ! 12 ! Normal acceleration !SDAC !29/1/333/01 ! 1 ! 8 ! 29 !
! ! ! ! ! !SDAC !29/2/333/01 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!234! 1-4! 12 ! 12 ! RH spoiler #1 position !FCDC !6C/1/371/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !FCDC !6C/2/371/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!235! 1-4! 12 ! 1 ! Pitch angle !IRS !04/1/324/01 ! 1 ! 4 ! 29 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1-4! 11 ! 8 ! Pitch angle !IRS !04/1/324/01 ! 2 ! 4 ! 27 !
! ! ! ! ! !IRS !04/2/324/10 ! ! ! !
! ! 1,3! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 !1/2! 23 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1,3! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 !1/2! 25 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!237! 1-4! 12 ! 10 ! ROLL angle !IRS !04/1/325/01 ! 1 ! 2 ! 29 !
! ! ! ! ! !IRS !04/2/325/10 ! ! ! !
! ! 1-4! 2 ! 2 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 2 ! 16 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!239! 1-4! 12 ! 1 ! Rudder position !SDAC !29/1/312/00 ! 1 ! 2 ! 29 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1-4! 11 ! 9 ! Rudder position !SDAC !29/1/312/00 ! 2 ! 2 ! 26 !
! ! ! ! ! !SDAC !29/2/312/00 ! ! ! !
! ! 1-4! 1 ! 1 ! EVENT button pressed !FDIU !17/1/350/00 ! 1 ! 1 ! 16 !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!242! 1-4! 12 ! 11 ! High Target Speed Margin !FGC !01/1/307/00 ! 1 ! 1 ! 28 !
! ! ! ! ! !FGC !01/2/307/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!243! 1-4! 12 ! 12 ! FMC status word: ATS FMA !FMC !02/1/271/00 ! 1 ! 1 ! 28 !
! ! ! ! ! (Label=271 SDI=00) !FMC !02/2/271/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!244! 1-4! 12 ! 6 ! FMC status word: ATS FMA !FMC !02/1/271/00 ! 1 ! 1 ! 16 !
! ! ! ! ! (Label=271 SDI=00) !FMC !02/2/271/00 ! ! ! !
! ! 1-4! 3 ! 3 ! FMC status word: ATS FMA !FMC !02/1/270/00 ! 1 ! 1 ! 13 !
! ! ! ! ! (Label=270 SDI=00) !FMC !02/2/270/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!247! 1-4! 12 ! 9 ! Approach speed target !DMC !25/1/304/01 ! 1 ! 1 ! 28 !
! ! 1-4! 3 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 20 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 2 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 11 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
! ! 1-4! 1 ! 1 ! FWC Discrete status word !FWC !26/1/126/00 ! 1 ! 1 ! 12 !
! ! ! ! ! (Label=126 SDI=00) !FWC !26/2/126/00 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!249! 1-4! 12 ! 9 ! Selected Mach / Manual !DMC !25/1/106/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/106/10 ! ! ! !
! ! 1-4! 3 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 19 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 2 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 16 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
! ! 1-4! 1 ! 1 ! FCU Discrete status word !FCU !A1/1A/274/00! 1 ! 1 ! 14 !
! ! ! ! ! (Label=274 SDI=00) !FCU !A1/1B/274/00! ! ! !
!---!----!----!----!--------------------------!--- -!------------!---!---!----!
!251! 1 ! 12 ! 8 ! DME 2 distance !DMC !25/1/202/10 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/202/10 ! ! ! !
! ! 2 ! 12 ! 9 ! VOR 2 frequency !DMC !25/1/034/10 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/034/10 ! ! ! !
! ! 2 ! 3 ! 3 ! VOR 2 frequency !DMC !25/1/034/10 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/034/10 ! ! ! !
! ! 3 ! 12 ! 9 ! ILS 2 frequency !DMC !25/1/033/10 ! 1 !1/4! 27 !
! ! ! ! ! !DMC !25/2/033/10 ! ! ! !
! ! 3 ! 3 ! 3 ! ILS 2 frequency !DMC !25/1/033/10 ! 2 !1/4! 17 !
! ! ! ! ! !DMC !25/2/033/10 ! ! ! !
! ! 4 ! 12 ! 11 ! DME 2 frequency !DMC !25/1/035/10 ! 1 !1/4! 28 !
! ! ! ! ! !DMC !25/2/035/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!253! 1-4! 12 ! 9 ! PFD selected speed !DMC !25/1/103/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/103/10 ! ! ! !
! ! 1 ! 3 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 !1/4! 13 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
! ! 1 ! 2 ! 1 ! DMC bus: Discrete status !DMC !25/1/271/01 ! 1 !1/4! 22 !
! ! ! ! ! word (label 271) !DMC !25/2/271/10 ! ! ! !
!---!----!----!----!--------------------------!-----!------------!---!---!----!
!255! 1-4! 12 ! 10 ! FMC altitude constraint !DMC !25/1/163/01 ! 1 ! 1 ! 28 !
! ! ! ! ! !DMC !25/2/163/10 ! ! ! !
+---+----+----+----+--------------------------+------------------+---+---+----+
Abbreviations: Target (TGT), Source (SCE), Frame (FR)

** ON A/C NOT FOR ALL
6. Component Description
A. Data Management Unit (DMU) FIN: 1-TV
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
F FDIMU - Housing ** ON A/C NOT FOR ALL
F FDIMU Internal Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Hardware Structure ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL

The DMU is a microprocessor-controlled unit with a module for collection and processing of digital parameters to monitor data by various aircraft systems. An expanded function is the creation of various A/C condition reports.
This monitoring is to derive maintenace relevant data. The internal SAR stores the result of specific trigger conditions. An optional function is the quicker access to the SAR stored data via the PCMCIA-Interface. An installed PCMCIA-Card is able to store the same data as the SAR.
The DMU-functional block diagram illustrates the internal connection of the functional modules of the DMU.
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
F FDIMU Internal Block Diagram ** ON A/C NOT FOR ALL
F FDIMU Internal Block Diagram ** ON A/C NOT FOR ALL
F FDIMU Internal Signal Flow ** ON A/C NOT FOR ALL
F FDIMU Interface ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU Interface ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL

The DMU is a microprocessor-controlled unit with a module for collection and processing of digital parameters to monitor data by various aircraft systems. An expanded function is the creation of various A/C condition reports.
This monitoring is to derive maintenace relevant data. The internal SAR stores the result of specific trigger conditions. An optional function is the quicker access to the SAR stored data via the PCMCIA-Interface. An installed PCMCIA-Card is able to store the same data as the SAR.
The DMU-functional block diagram illustrates the internal connection of the functional modules of the DMU.
B. Flight Data Interface and Management Unit (FDIMU)
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
F FDIMU - Housing ** ON A/C NOT FOR ALL
F FDIMU Internal Block Diagram ** ON A/C NOT FOR ALL
F FDIMU Internal Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Hardware Structure ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU Interface ** ON A/C NOT FOR ALL
F FDIMU Interface ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
F FDIMU - Functional Block Diagram ** ON A/C NOT FOR ALL
The FDIMU puts together the functions of the DFDRS and the AIDS. (For details refer to the System-Description of this topic.)
The FDIMU is a microprocessor-controlled unit, that is assembled from six different electronic modules. It has two separate microprocessor-units:
  • AMP1-1 controls the DFDRS (FDIU-part)
  • AMP1-2 controls the AIDS (DMU-part)
    (AMP - Acquisition Management Computer)
In this Component-Description only the general-part and the DMU-part of the FDIMU are described.
For the description of the FDIU-part refer to (Ref. AMM D/O 31-33-00-00).
C. Hardware Layout of the DMU
F FDIMU Internal Components ** ON A/C NOT FOR ALL
F FDIMU Internal Components ** ON A/C NOT FOR ALL
D. Hardware Layout of the FDIMU
F FDIMU Internal Components ** ON A/C NOT FOR ALL
F FDIMU Internal Components ** ON A/C NOT FOR ALL
(1) Physical Specification of the FDIMU
The FDIMU is a rectangular casing box according to standard ARINC 600 - 3MCU.
The unit box has cooling in/outlets on the top and on the bottom.
(2) Electrical Specification of the FDIMU
The FDIMU is supplied by main power 115 AC - 400 HZ. The power consumption of the unit depends on the P/N.
(3) Mechanical Description of the FDIMU
The front panel of the FDIMU consists of:
  • A carrying handle
  • A front door to get access to the test connector, PCMCIA insertion slot and the indication lights.
The test connector is used for:
  • PDL connection
  • Maintenance test equipment connection (dialogue with PC fitted with PTE software).
The rear has:
  • A connector with three blocks marked TP, MP, BP.
(4) Internal Components of the FDIMU
The FDIMU is equipped with a motherboard and separate cards. The configuration of the cards installed is related to the model of the FDIMU.
E. Hardware Structure of the FDIMU

The FDIMU consists of six major-assemblies as follows:
  • AMP1-1 Acquisition-/Management-Processor for DFDRS-function
  • AMP1-2 Acquisition-/Management-Processor for AIDS-function
  • PCMCIA Daughter-Board
  • Power-Supply Module
  • Motherboard
  • ARINC-Connector-Card with ARINC-600 Standard-Connector.
Both Acquisition-/Management-Processor, AMP1-1 and AMP1-2, consists of the same hardware-module named AMP1. AMP1-1 is used in slot-1. AMP1-2 is used in slot-2.

AMP1 Processor - Resources
---------------------------------------------------------------------------
! Resource ! Description ! Quantity !
!-------------------+--------------------------------------------+----------!
! CPU ! MPC8240 (Power PC) ! 1 !
!-------------------+--------------------------------------------+----------!
! Memory ! Boot EPROM !512 KByte !
! ! Flash EPROM ! 4 MByte !
! ! SRAM (Battery-Backed) ! 6 MByte !
!-------------------+--------------------------------------------+----------!
! Discrete Inputs ! ARINC 717 / Program-Pin Shunt ! 80 !
!-------------------+--------------------------------------------+----------!
! Discrete Outputs ! ABD0048 Medium-Power Shunt ! 3 !
! ! Contact Closure (Switches) ! 6 !
! ! A340 Discrete Multiplexer Selector (Shunt) ! 8 !
! ! Front-Panel LED Drivers ! 4 !
!-------------------+--------------------------------------------+----------!
! ARINC-429 Inputs ! Broadcast (Label-Buffered) ! 48 !
! ! Burst (Interrupt-Driven) ! 4 !
!-------------------+--------------------------------------------+----------!
! ARINC-429 Outputs ! Double-Buffered ! 4 !
! ! FIFO-Buffered ! 1 !
!-------------------+--------------------------------------------+----------!
! Recorder Inputs ! Harvard Bi-Phase (DFDR) ! 2 !
!-------------------+--------------------------------------------+----------!
! Recorder Outputs ! Harvard Bi-Phase (DFDR/QAR) ! 2 !
! ! Bipolar RZ (QAR) ! 1 !
! ! Audio (AMU-CVR) ! 1 !
!-------------------+--------------------------------------------+----------!
! Serial Ports ! UART + RS232 Interface (Analyzer + Spare) ! 3 !
! ! UART + RS422 Interface (QAR) ! 1 !
!-------------------+--------------------------------------------+----------!
! Real-Time-Clock ! Battery-Backed ! 1 !
!-------------------+--------------------------------------------+----------!
! PCMCIA *) ! ATA, Type II or Type III form-factor ! 1 !
!-------------------+--------------------------------------------+----------!
! Ethernet *) ! 10BaseT ! 1 !
---------------------------------------------------------------------------
*) only on AMP1-2



The FDIMU consists of six major-assemblies as follows:
  • AMP1-1 Acquisition-/Management-Processor for DFDRS-function
  • AMP1-2 Acquisition-/Management-Processor for AIDS-function
  • PCMCIA Daughter-Board
  • Power-Supply Module
  • Motherboard
  • ARINC-Connector-Card with ARINC-600 Standard-Connector.
Both Acquisition-/Management-Processor, AMP1-1 and AMP1-2, consists of the same hardware-module named AMP1. AMP1-1 is used in slot-1. AMP1-2 is used in slot-2.

AMP1 Processor - Resources
+---------------------------------------------------------------------------+
! Resource ! Description ! Quantity !
!-------------------+--------------------------------------------+----------!
! CPU ! MPC8240 (Power PC) ! 1 !
!-------------------+--------------------------------------------+----------!
! Memory ! Boot EPROM !512 KByte !
! ! Flash EPROM ! 6 MByte !
! ! SRAM (Battery-Backed) ! 6 MByte !
!-------------------+--------------------------------------------+----------!
! Discrete Inputs ! ARINC 717 / Program-Pin Shunt ! 80 !
!-------------------+--------------------------------------------+----------!
! Discrete Outputs ! ABD0048 Medium-Power Shunt ! 3 !
! ! Contact Closure (Switches) ! 6 !
! ! A340 Discrete Multiplexer Selector (Shunt) ! 8 !
! ! Front-Panel LED Drivers ! 4 !
!-------------------+--------------------------------------------+----------!
! ARINC-429 Inputs ! Broadcast (Label-Buffered) ! 48 !
! ! Burst (Interrupt-Driven) ! 4 !
!-------------------+--------------------------------------------+----------!
! ARINC-429 Outputs ! Double-Buffered ! 4 !
! ! FIFO-Buffered ! 1 !
!-------------------+--------------------------------------------+----------!
! Recorder Inputs ! Harvard Bi-Phase (DFDR) ! 2 !
!-------------------+--------------------------------------------+----------!
! Recorder Outputs ! Harvard Bi-Phase (DFDR/QAR) ! 2 !
! ! Bipolar RZ (QAR) ! 1 !
! ! Audio (AMU-CVR) ! 1 !
!-------------------+--------------------------------------------+----------!
! Serial Ports ! UART + RS232 Interface (Analyser + Spare) ! 3 !
! ! UART + RS422 Interface (QAR) ! 1 !
!-------------------+--------------------------------------------+----------!
! Real-Time-Clock ! Battery-Backed ! 1 !
!-------------------+--------------------------------------------+----------!
! PCMCIA *) ! ATA, Type II or Type III form-factor ! 1 !
!-------------------+--------------------------------------------+----------!
! Ethernet *) ! 10BaseT ! 1 !
+---------------------------------------------------------------------------+
*) only on AMP1-2


(1) AMP1-1 Acquisition-/Management-Processor for DFDRS-Function
The AMP1-1 does the FDIU-function of the FDIMU. Its primary function is to acquire and to process data for the mandatory DFDRS. The AMP1-1 is able to process and send data in frames to the DFDR and to the QAR (optional) at rates of 64, 128, 256, 512, 1024 or 2048 Words/s.

(2) AMP1-2 Acquisition-/Management-Processor for AIDS-Function
The AMP1-2 does the DMU-function of the FDIMU. It provides the fully programmable AIDS-functionality.
The AMP1-2 receives data from external A/C-systems through ARINC-429 broadcast-busses and discrete inputs. The AIDS generates reports based on specific trigger-conditions in the A/C-data. It provides data recording capabilities and programmable reporting-functions. The AMP1-2 also communicates with some external devices through dedicated ARINC-429 busses for the purposes of transferring files, messages or display information.

(3) PCMCIA Daughter-Board (optional)
The PCMCIA Daughter-Board provides a PCMCIA-interface for:
  • Storing/Recording of raw- and message-data.
  • Up- and Down-Loading of FDIMU-Software.
The PCMCIA Daughter-Board is placed on the AMP1-2. You have access to the PCMCIA-interface after you open the access-door at the front of the FDIMU.

Also there is an Ethernet-Interface on the PCMCIA Daughter-Board.

(4) Power-Supply Module
The FDIMU is supplied by the A/C 115VAC 400Hz single-phase power. It can tolerate a power-interrupt up to t=200ms without any bad operation. The power-consumption of the FDIMU depends on the FDIMU P/N.
The FDIMU power-supply module generates all voltages for the FDIMU internal use.

(5) Motherboard
The motherboard is the interface between the AMP1-1 Processor, the AMP1-2 Processor, the power-supply module and the ARINC-Connector-Card.
(The PCMCIA- and the Ethernet-Interface are placed on the AMP1-2.)

(6) ARINC-Connector-Card
The ARINC-Connector-Card is the interface between the Motherboard and the Input-/Output-Connectors.

(7) ARINC-600 Standard-Connector
The ARINC-600 Standard-Connector is placed on the ARINC-Connector-Card.

(8) Test-Connector
A test-connector is placed at the front of the FDIMU (behind the access-door). The test-connector provides:
  • 115V AC-power from the ARINC-Connector-Card
  • system test-signals
    The test-connector enables the connection of portable test-equipment and a data-loader to the FDIMU.
F. Hardware Determined Functions of the FDIMU
(1) ALFDIMU board
F FDIMU Internal Components ** ON A/C NOT FOR ALL
  • Generates +5V, 12V and -12V for printed circuit board
  • Generates system control signals such as: reset, power fail and A/C mains fail
  • Monitors the battery
  • Stores the energy for 200ms of operation after a shutdown of A/C mains
  • Holds the test connector
  • Operates as a battery switch.
(2) ED48-FDIU board
The ED48-FDIU board allocates:
  • Up to 32 ARINC 429 inputs including MDDU and CFDIU (low-speed or high-speed under software control for each input)
  • 4 ARINC 429 outputs including CFDIU, MDDU and 2 spares (speed for each output are under software control. All outputs can be isolated from the wiring also under software control)
  • Up to 80 discrete shunt inputs including DFDR bite, QAR fail and tape low, EVENT marker, MDDU select aircraft identification and spares
  • 2 interfaces to DFDR: two outputs and two playback inputs
  • 1 synchro CVR output
  • 1 QAR output
  • 1 FDIU BITE output
  • 1 input/output RS232 line (to/from test connector)
  • 1 hi-speed link with DMU
  • CPU MOTOROLA 68360; clock = 23 MHz
  • 1 bank of 2 MB of static RAM
  • 1 bank of 1 MB of flash memory (boot and BITE)
  • 1 bank of 2 MB of flash memory (program).
(3) ARIFDIMU board
The ARIFDIMU board gets all ARINC 429 busses as required for the DMU part-system:
  • 64 inputs
  • 6 outputs
  • Provision for growth of maximum 80 inputs and 7 outputs.

NOTE: Speed of all inputs and outputs can be individually selected under software control.
  • Interface to CPU of DMU board by a proprietary hi-speed bus.
(4) CPUDMU board
The CPUDMU board allocates:
  • Up to 25 shunt discrete inputs (with spares),
  • 1 bi-directional RS422 line (DAR control-in/control-out)
  • 1 ARINC 573 outputs (DAR data and sync out)
  • 6 electrically isolated discrete outputs (DAR speed and DAR run)
  • 3 discrete outputs (1 BITE and 2 spares)
  • 1 bi-directional RS232 line (to/from test connector)
  • 1 control and interface to external cards by a special hi-speed bus (default = ARIFDIMU board; all boards are mapped into CPU memory)
  • 1 link from ED48-FDIU board
  • Interface to PCMCIA flash memory PC card. PC cards Type II and III with a storage capacity higher or equal to 64 GBytes are recommended
  • CPU MPC860 family at 23/46 MHz (external/internal bus)
  • 1 bank of 6 M bytes of static RAM
  • 1 bank of 4 M bytes of boot ROM, flash type
  • 1 bank of 4 M bytes of user program ROM, flash type
  • 1 bank of 4 M bytes of database ROM, flash type
  • One bank of 4 M bytes of RAM; for report storage and SAR.
NOTE: This memory is backed-up by a battery.
  • 3 WEFA discrete inputs
  • 1 mezzanine to authorize the wireless emission of the SPC (Smart PCMCIA Card) with the 3 WEFA discrete inputs
  • 1 boost to supply the wireless emission of the SPC
  • 1 specific PCMCIA interface to match with a SPC.
(5) ALFDIMU board
F FDIMU Internal Components ** ON A/C NOT FOR ALL
The ALFDIMU board provides:
  • Generation of +5V, 12V and -12V for the printed circuit boards
  • Generation of system control signals such as: reset, power fail and A/C mains fail
  • Monitoring of battery
  • Energy storage for 200 ms of operation after shutdown of A/C mains
  • Support for test connector
  • Battery switch.
(6) ED48-FDIU board
The ED48-FDIU board provides:
  • Up to 32 ARINC 429 inputs including MDDU and CFDIU (low-speed or high-speed under software control for each input)
  • 4 ARINC 429 outputs including CFDIU, MDDU and 2 spares (speed for each output are under software control, any output can be isolated from the wiring also under software control)
  • Up to 80 discrete shunt inputs including DFDR bite, QAR fail and tape low, EVENT marker, MDDU select aircraft identification and spares
  • 2 interfaces to DFDR: two outputs and two playback inputs
  • 1 synchro CVR output
  • 1 QAR output
  • 1 FDIU BITE output
  • 1 input/output RS232 line (to/from test connector)
  • 1 hi-speed link with DMU
  • CPU MOTOROLA 68360, clock = 23 MHz
  • 1 bank of 2 Mbytes of static RAM
  • 1 bank of 1 Mbytes of flash memory (boot and BITE)
  • 1 bank of 2 Mbytes of flash memory (program).
(7) ARIFDIMU board
The ARIFDIMU board gets all ARINC 429 busses as required for the DMU part-system:
  • 64 inputs
  • 6 outputs.

NOTE: Speed of all inputs and outputs is individually selectable under software control.
  • Interface to CPU of DMU board by a proprietary hi-speed bus.
(8) CPUDMU board
The CPUDMU board provides:
  • Up to 25 shunt discrete inputs (with spares)
  • 1 bi-directional RS422 line (DAR control-in/control-out)
  • 1 ARINC 573 outputs (DAR data and sync out)
  • 6 electrically isolated discrete outputs (DAR speed and DAR run)
  • 3 discrete outputs (1 BITE and 2 spares)
  • 1 bi-directional RS232 line (to/from test connector)
  • 1 control and interface to external cards by a special hi-speed bus (default = ARIFDIMU board, all boards are mapped into CPU memory)
  • 1 link from ED48-FDIU board
  • Interface to PCMCIA flash memory PC card, PC cards Type I and II with a storage capacity higher or equal to 64 GBytes are recommended
  • Ethernet interface 10 BT (1 transmission/ 1 reception lines at 10 Mbps)
  • CPU MPC860 family at 23/46 MHz (external/internal bus)
  • 1 bank of 6 Mbytes of static RAM
  • 1 bank of 4 Mbytes of boot ROM, flash type
  • 1 bank of 4 Mbytes of user program ROM, flash type
  • 1 bank of 4 Mbytes of database ROM, flash type
  • 1 bank of 4 Mbytes of RAM, for report storage and SAR.
NOTE: This memory is backed-up by a battery.
G. Software Determined Functions
(1) Boot Software
The boot software enables the subsequent functions:
  • MDDU/PDL program load of DMU operational software
  • MDDU/PDL program load of DMU database
  • Determination of valid operational-software installed
  • GSE monitor/test functions
  • Built-In-Test (a part of it).
(2) Operational Software
The operational software enables the subsequent functions:
  • Task scheduling
  • Management of processing resources
  • I/O operations
  • BITE functions
  • Interpretation of the database
    * Report processing
    * SAR and DAR recording
    * Broadcast of selected parameters on the output Bus B (ACARS)
  • Parameter Call-Up
  • MCDU, Printer and ACARS communications
  • CFDS communications
  • Data acquisition
  • All MCDU menus
  • AIDS reports.
(3) DMU Database
The Database enables the subsequent functions:
  • Constants for AI Standard AIDS Reports
  • Report inhibit control
  • Programmable AIDS parameters
  • Programmable logic conditions
  • DAR functions
  • SAR functions
  • Trigger code 3000 for AI Standard Reports
  • Output rules
  • Remote print button
  • General broadcast output labels.
H. General Functions of the FDIMU
(1) Identification of Location
The design of the FDIMU allows its use in A/C with different input parameters and different tasks for data evaluation, if the appropriate programs are implemented. The unit is able to identify A/C type information on the internal FDIU-bus. In relation with the occurrence of specific conditions or events, the FDIMU (DMU-part) has trigger predefined actions. As a result of specific trigger conditions AIDS reports are generated or data are recorded on the DAR (optional) or stored in the FDIMU internal Smart Access Recorder (SAR). Print reports can be either printed out on the cockpit printer or transmitted through ACARS (optional).
SAR data is also retrieved through the Portable Data Loader (PDL).
Functions which are specific to A/C type (CFMI or IAE engines) are shown in the respective logic definition.
The A/C type coding, parameter 17.1.304.00, is shown below:
Engine Type ! Bit No
! 16 15 14 13 12 11
-------------------------------+----------------------------
For CFM 56-5 ! 0 1 0 0 1 1
For IAE V2500 ! 0 1 0 1 0 0
For P&W ! 0 1 1 1 0 0

If the code for no programming is received, the FDIMU works according to the A/C type code from the last flight. If there is no coding from the last flight, the FDIMU works with the CFMI type code.
(2) History Buffer
A history buffer is provided for the history data required by the AIDS reports and the DAR and SAR. It is the responsibility of the sampling task, to control this buffer and manage the history buffering. The management of the history buffer is determined by the parameter sampling table. It is possible to program additional parameters for history buffering through Ground Support Equipment (GSE).
(3) FDIMU Internal Parameter
Internally the FDIMU processed-parameters are referred to as "Internal Parameters". All internal parameters are identified by a parameter number consisting of the EQ/SYS/LABEL/SDI. For the FDIMU applications up to 400 internal parameters can be created. In addition the parameter can be assigned with an alpha call-up code for identification through GSE programming.
Internal parameters are provided for:
  • FDIMU internal counter and timer
  • Filtered Parameters
  • Flags for certain flight conditions
  • Report status words
  • SAR channel words
  • Additional global computed variables defined by the user.
(4) Parameter Label Call-Up
Each parameter (ARINC 429 data word) transmitted on one of the connected data buses is selectable, you use: EQ, source system, label, SDI and number of data bits for display on the MCDU. The number of data bits can be omitted. The displayed parameters are updated once per second. The menus are shown in 'AIDS PARAM LABEL CALL-UP'. Up to 2 parameters can be displayed on one page. 8 pages can be selected through slew up/slew down button, which leads to a maximum number of 16 parameters to be monitored simultaneously.
If there are additional parameters in the future, it is possible to call them up in the same way without having to change the software.
Example for Parameter Call-up: EQ/SYS/LAB/SDI = 1A/2/156/01
(5) Parameter Alpha Call-Up (ACU)
For all the parameters an alpha code is mentioned in the parameter list. The selection is performed by their alpha codes.
If parameters from two systems are available, both parameters are displayed on the MCDU upon a single alpha call-up code entry. The display values refresh once per second. All numeric type alpha call-up parameters show on the MCDU in engineering units. The display format is a floating point representation of max. 6 characters including the decimal point and the '-' sign, if applicable. In case of positive numbers without decimal points all 6 characters are available for digits. Display of leading zero is suppressed. The applicable units are displayed below the alpha call-up code on the MCDU screen.
Alpha call-up parameters, which consist of a combination of some discrete bits or packed discrete show in HEX.
Discrete alpha call-up parameters show on the MCDU by using English status indications of max. 6 characters together with the actual bit status. The unit indication on the MCDU screen is 'DISCRETE'.

(6) Additional Parameter Programming
If a new label (parameter) is used in the FDIMU (for other than a parameter label call-up) it must be programmed through the GSE.
(7) Test Input Parameters
The FDIMU DITS ports no 49 and 50 are dedicated test inputs. These ports are wired to the FDIMU rear connector and to the FDIMU test connectors. The test connector allows access to all ARINC 429 buses in the aircraft. The FDIMU DITS 'Test Inputs' are referenced with the GSE programmable equipment code.
(8) Additional Bus
If an additional ARINC 429 Bus is connected to one of the FDIMU ports, the characteristics of the new bus (transmission speed, equipment code, system number) is programmable through the GSE for the appropriate port number. The new parameter is used for the purpose of no limitation label call-up, trigger logics, data recording and reports.
(9) Engineering Unit Conversion (EUC)
The FDIMU provides an 'Engineering Unit Conversion Table' to convert a selected group of input parameters (same as supplied with alpha call-ups) into the applicable engineering units. The EUC table is associated to the alpha call-up table.
The GSE reconfiguration software lets you add or modify the conversion constants. Modifications are made by specifying a single scale constant, number of data bits and sign.
(10) Special Rules for Kg and Deg C
All parameters for which an alpha acronym is defined in the parameter list is available for alpha call-up. With a single call-up system 1 and 2 parameters are displayed in engineering units.
The FDIMU observe bit 18 and bit 27 of DMC label 305. If bit 18 = 1, then the parameter values are shown in print out and alpha call-up in the following units:
fuel flow (eng 1 and 2): lbs/hours instead of Kg/hours
(7C.1.244.01, 7C.2.244.10)
gross weight: lbs instead of Kg
(02.1.075.00, 02.2.075.00)
pack flow: lbs/sec instead of Kg/sec
(8E.1.126.11, 8E.2.126.00)
bleed air flow: lbs/sec instead of Kg/sec
(7A.1.123.01)
fuel quantity: lbs instead of Kg
(5A.2.256.10, 5A.2.257.10,
5A.2.260.10, 5A.2.261.10,
5A.2.262.10, 5A.2.247.10)
If bit 27 = 1, then the parameter values are shown in print out and alpha call-up in the following units:
comfort temperatures ckpt, cab temp: deg F instead of deg C
(29.1.242.01, 29.2.242.01,
29.1.244.01, 29.2.244.01,
29.1.245.01, 29.2.245.01)

(11) Flight Phase Detection
F AIDS Flight Phases - Table 11 ** ON A/C NOT FOR ALL
The FDIMU divides the flight leg into separate flight phases. The internal FDIMU flight-phase determination is mainly based on the FWC flight phases (Param. 26.1.126.01 or 26.2.126.01 Bits 14 to 11). The determination of a new flight phase is independent from the previously encountered flight phase. The coding of the FDIMU internal flight phases is as follows:
+--------------------------------------+
! Flight ! FDIMU Internal Flight Phase !
! Phase ! Coding !
! Number ! Bit: 14 ! 13 ! 12 ! 11 !
---------------------------------------!
! 1.0 ! 0 ! 0 ! 0 ! 1 !
! 1.1 ! 0 ! 0 ! 0 ! 1 !
! 2.0 ! 0 ! 0 ! 1 ! 0 !
! 3.0 ! 0 ! 0 ! 1 ! 1 !
! 4.0 ! 0 ! 1 ! 0 ! 0 !
! 5.0 ! 0 ! 1 ! 0 ! 1 !
! 5.1 ! 0 ! 1 ! 0 ! 1 !
! 6.0 ! 0 ! 1 ! 1 ! 0 !
! 7.1 ! 0 ! 1 ! 1 ! 1 !
! 7.0 ! 0 ! 1 ! 1 ! 1 !
! 8.0 ! 1 ! 0 ! 0 ! 0 !
! 9.0 ! 1 ! 0 ! 0 ! 1 !
! 10.0 ! 1 ! 0 ! 1 ! 0 !
+--------------------------------------+
The FDIMU internal flight phase is transmitted under label 00D.1.050.00 Bits 11-14.
(12) Data Filtering
The FDIMU contains software which does the data filtering for up to 300 parameters. The filtered parameters are used for logical decisions.
The filter characteristics are as shown below:
t
FO = OFV + ------- * (NRV - OFV)
T
Where: FO = Filter Output
OFV = Old Filtered Value
t = Samples/sec
T = Filter Time Constant
NRV = New Raw Value

The time constant T is modifiable through ground software.
For discrete words the appropriate bits are observed. Those bits must remain stable for at least 3 consecutive samples before incorporating the new status into logic decisions.
(13) Class 3 Failure Messages
If no data is received from one of the DITS ports for longer than 60 sec, a class 3 failure is reported to the CFDS. It is possible to enable/disable the bus monitoring one per bus basis through the GSE. Only enabled buses are reported with class 3 failures in the case that parameters are not updated.
The class 3 failure message shows the ATA-chapter, name, the FIN number of the source system and the FDIMU name and the FDIMU FIN number.
This example explains the message:
ATA-Chapter
I Source System Name
I I Source System FIN Number
I I I Name
I I I I FIN Number
I_____ I_____ I____ I__ I____
732534 EIVMU1 (1KS1) / FDIMU (10TV)

(14) Identification of Location
The design of the FDIMU allows its use in A/C with different input parameters and different tasks for data evaluation without hardware or software modifications. The unit is able to identify the following configurations:
  • A/C type (A318, A319, A320 or A321),
  • Engine type (different versions within the engine family) and
  • Air Conditioning Controller Configuration.

    In relation with the occurrence of specific conditions or events, the FDIMU (DMU-part) has trigger predefined actions. As a result of specific trigger conditions AIDS reports are generated or data are recorded on the DAR (optional) or stored in the FDIMU internal Smart Access Recorder (SAR). Print reports can be either printed out on the cockpit printer or transmitted through ACARS (optional).
    SAR data is also retrieved through the Portable Data Loader (PDL).
    Functions which are specific to A/C type (CFMI or IAE engines) are shown in the respective logic definition.
    The A/C type coding, parameter 17.1.304.00, is shown below:
    Engine Type ! Bit No
    ! 16 15 14 13 12 11
    -------------------------------+----------------------------
    For CFM 56-5 ! 0 1 0 0 1 1
    For IAE V2500 ! 0 1 0 1 0 0
    For P&W ! 0 1 1 1 0 0

    If the code for no programming is received, the FDIMU works related to the A/C type code from the last flight. If there is no coding from the last flight, the FDIMU works with the CFMI type code.

(15) History Buffer
A history buffer is provided for the history data required by the AIDS reports and the DAR and SAR. It is the responsibility of the sampling task, to control this buffer and manage the history buffering. The management of the history buffer is determined by the parameter sampling table. It is possible to program additional parameters for history buffering through Ground Support Equipment (GSE).

(16) FDIMU Internal Parameter
Internally the FDIMU processed-parameters are referred to as "Internal Parameters". All internal parameters are identified by a parameter number consisting of the EQ/SYS/LABEL/SDI. For the FDIMU applications up to 400 internal parameters can be created. In addition the parameter can be assigned with an alpha call-up code for identification through GSE programming.
Internal parameters are provided for:
  • FDIMU internal counter and timer
  • Filtered Parameters
  • Flags for certain flight conditions
  • Report status words
  • SAR channel words
  • additional global computed variables defined by the user.
(17) Parameter Label Call-Up
Each parameter (ARINC 429 data word) transmitted on one of the connected data buses is selectable, you use: EQ, source system, label, SDI and number of data bits for display on the MCDU. The number of data bits can be ignored. The displayed parameters are updated once per second. The menus are shown in 'AIDS PARAM LABEL CALL-UP'. Up to 2 parameters can be displayed on one page. 8 pages can be selected through slew up/slew down button, which leads to a maximum number of 16 parameters to be monitored simultaneously.
If there are additional parameters in the future, it is possible to call them up in the same way without having to change the software.
Example for Parameter Call-up: EQ/SYS/LAB/SDI = 1A/2/156/01

(18) Parameter Alpha Call-Up (ACU)
For all the parameters an alpha code is mentioned in the parameter list. The selection is done by their alpha codes.
If parameters from two systems are available, both parameters are displayed on the MCDU upon a single alpha call-up code entry.
The display values refresh once per second. All numeric type alpha call-up parameters show on the MCDU in engineering units. The display format is a floating point representation of max. 6 characters including the decimal point and the '-' sign, if applicable. In case of positive numbers without decimal points all 6 characters are available for digits. Display of leading zero is suppressed. The applicable units are displayed below the alpha call-up code on the MCDU screen.
Alpha call-up parameters, which consist of a combination of some discrete bits or packed discretes show in HEX.
Discrete alpha call-up parameters show on the MCDU by using English status indications of max. 6 characters together with the actual bit status. The unit indication on the MCDU screen is 'DISCRETE'.

(19) Additional Parameter Programming
If a new label (parameter) is used in the FDIMU (for other than a parameter label call-up) it must be programmed through the GSE.

(20) Test Input Parameters
The FDIMU DITS ports No 49 and 50 are dedicated test inputs. These ports are wired to the FDIMU rear connector and to the FDIMU test connectors. The test connector allows access to all ARINC 429 buses in the aircraft. The FDIMU DITS 'Test Inputs' are referenced with the GSE programmable equipment code.

(21) Additional Bus
If an additional ARINC 429 Bus is connected to one of the FDIMU ports, the characteristics of the new bus (transmission speed, equipment code, system number) is programmable through ground software for appropriate port number. The new parameter is used for the purpose of label call-up, trigger logics, data recording and reports.

(22) Engineering Unit Conversion (EUC)
The FDIMU provides an 'Engineering Unit Conversion Table' to convert a selected group of input parameters (same as supplied with alpha call-ups) into the applicable engineering units. The EUC table is associated to the alpha call-up table.
The GSE reconfiguration software lets you add or modify the conversion constants. Modifications are made by specifying a single scale constant, number of data bits and sign.

(23) Special Rules for Kg and Deg C
The FDIMU observe bit 18 and bit 27 of DMC label 305. If bit 18 = 1, then the parameter values are shown in print out and alpha call-up in the following units:
Fuel flow (eng 1 and 2): lbs/hours instead of Kg/hours
(7C.1.244.01, 7C.2.244.10)
Fuel Flow Feedback (eng 1 and 2) lbs/hours instead of Kg/hours
(7C.1.347.01 and 7C.2.347.10)
gross weight: lbs instead of Kg
(02.1.075.00, 02.2.075.00)
pack flow: lbs/sec instead of Kg/sec
(8E.1.126.11, 8E.2.126.00)
bleed air flow: lbs/sec instead of Kg/sec
(7A.1.123.01)
fuel quantity: lbs instead of Kg
(5A.2.256.10, 5A.2.257.10,
5A.2.260.10, 5A.2.261.10,
5A.2.262.10, 5A.2.247.10)

If bit 27 = 1, then the parameter values are shown in print out and alpha call-up in the following units:
comfort temperatures ckpt, cab temp: deg F instead of deg C
(29.1.242.01, 29.2.242.01,
29.1.244.01, 29.2.244.01,
29.1.245.01, 29.2.245.01)

If the label 305 from the DMC becomes invalid during flight or it is invalid at power-on, the switchable parameters will default set to Kg respectively deg C.

(24) Flight Phase Detection
F AIDS Flight Phases - Table 11 ** ON A/C NOT FOR ALL
The FDIMU divides the flight leg into separate flight phases. The internal FDIMU flight-phase determination is mainly based on the FWC flight phases (Param. 26.1.126.01 or 26.2.126.01 Bits 14 to 11).
The determination of a new flight phase is independent from the previously encountered flight phase. The coding of the FDIMU internal flight phases is as follows:
+--------------------------------------------+
! Flight ! FDIMU (DMU-part) Internal Flight !
! Phase ! Phase Coding Bit: !
! !-----------------------------------!
! ! 17 ! 16 ! 15 ! 14 ! 13 ! 12 ! 11 !
!--------------------------------------------!
! 1.0 ! 0 ! 0 ! 0 ! 1 ! 0 ! 1 ! 0 !
! 1.1 ! 0 ! 0 ! 0 ! 1 ! 0 ! 1 ! 1 !
! 2.0 ! 0 ! 0 ! 1 ! 0 ! 1 ! 0 ! 0 !
! 3.0 ! 0 ! 0 ! 1 ! 1 ! 1 ! 1 ! 0 !
! 4.0 ! 0 ! 1 ! 0 ! 1 ! 0 ! 0 ! 0 !
! 5.0 ! 0 ! 1 ! 1 ! 0 ! 0 ! 1 ! 0 !
! 5.1 ! 0 ! 1 ! 1 ! 0 ! 0 ! 1 ! 1 !
! 6.0 ! 0 ! 1 ! 1 ! 1 ! 1 ! 0 ! 1 !
! 7.1 ! 1 ! 0 ! 0 ! 0 ! 1 ! 1 ! 1 !
! 7.0 ! 1 ! 0 ! 0 ! 0 ! 1 ! 1 ! 0 !
! 8.0 ! 1 ! 0 ! 1 ! 0 ! 0 ! 0 ! 0 !
! 9.0 ! 1 ! 0 ! 1 ! 1 ! 0 ! 1 ! 0 !
! 10.0 ! 1 ! 1 ! 0 ! 0 ! 1 ! 0 ! 0 !
+--------------------------------------------+
The FDIMU internal flight phase is transmitted under label 00D.1.050.00 Bits 11-14.

(25) Data Filtering
The FDIMU contains software which does data filtering for up to 300 parameters. The filtered parameters are used for logical decisions.
The filter characteristics are as shown below:
t
FO = OFV + ------- * (NRV - OFV)
T
Where: FO = Filter Output
OFV = Old Filtered Value
t = Samples/sec
T = Filter Time Constant
NRV = New Raw Value

The time constant T is modifiable through ground software.
For discrete words the appropriate bits are observed. Those bits remain stable for at least 3 consecutive samples before you include the new status into logic decisions.

(26) Class 3 Failure Messages
The class 3 failure message shows the ATA-chapter, name, the 'FIN' number of the source system and the FDIMU name and the FDIMU 'FIN' number.
This example explains the message:
ATA-Chapter Reference of Source System
I Source System Name
I I Source System FIN Number
I I I FDIMU Name
I I I I FDIMU FIN Number
I_____ I_____ I____ I__ I____
773234 EVMU1 (2EV) / FDIMU (10TV)

For each failed system (missing valid parameters or bus activity) only one failure message is included in the list of reported class 3 failures, even if some busses of this system.
(27) Flight Phase Detection Logic - Description of Function Item
+----------------------------------------------------------------------+
! Log ! Item ! Description of Function Item !Prog !
! No ! No ! !MCDU !
!------+-------+------------------------------------------------+------!
! ! !The FDIMU uses the FWC flight phases (parameter ! !
! ! !26.1.126.01 bit 11 to 14 which does the AIDS ! !
! ! !flight phases as shown in Table 11) ! !
! ! ! ! !
! ! A ! Parameter ! !
! ! ! ! !
! ! B ! Logic algorithm ! !
! ! ! ! !
! ! B.1 ! ALT 1 = 10000 ft ! AI/C !
! ! ! ! !
! ! B.2 ! ALT 2 = 10000 ft ! AI/C !
! ! ! ! !
! ! B.3 ! IVV 1 = 400 ft/min ! AI/C !
! ! ! ! !
! ! B.4 ! IVV 2 = -400 ft/min ! AI/C !
! ! ! ! !
! ! B.5 ! IVV 3 = 400 ft/min ! AI/C !
! ! ! ! !
! ! B.6 ! SLAT1 = 5 deg ! AI/C !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

Flight Phase Detection Logic - Table 12

(28) Flight Phase Detection Logic - Description of Function Item
+---------------------------------------------------------------+
! Log. ! Item ! Description of Function Item !
! No ! No ! !
!------+-------+------------------------------------------------!
! ! !The FDIMU uses the FWC flight phases (parameter !
! ! !26.1.126.01 bit 11 to 14 to do the AIDS !
! ! !flight phases as shown in Table 11) !
! ! ! !
! ! A ! Parameter !
! ! ! !
! ! B ! Logic algorithm !
! ! ! !
! ! B.1 ! ALT 1 = 10 000 ft !
! ! ! !
! ! B.2 ! ALT 2 = 10 000 ft !
! ! ! !
! ! B.3 ! IVV 1 = 400 ft/min !
! ! ! !
! ! B.4 ! IVV 2 = -400 ft/min !
! ! ! !
! ! B.5 ! IVV 3 = 400 ft/min !
! ! ! !
! ! B.6 ! SLAT1 = 5 deg !
+------+-------+------------------------------------------------+

Flight Phase Detection Logic - Table 12

I. General AIDS Function
The AIDS functionality is divided into the following major functions:
  • AIDS Reports
  • Smart AIDS Recorder (SAR) Function
  • Digital AIDS Recorder (DAR) Function (if DAR is installed)
  • Input/Output User Function
  • GSE Readout Function
  • GSE Reconfiguration.
J. AIDS Reports
The AIDS Reports are AIDS monitor functions which have fixed trigger mechanism, fixed data collection and fixed output formatting. These reports perform the basic aircraft monitoring functions which are required. These monitoring functions collect parameters for trend analysis of the engines, the aircraft and the APU.
Aircraft data are also collected and automatically output during times of aircaft operational anomalies (e.g. engine over-temperature).
If a report is triggered manual by the remote print button, then the report is immediately generated (independent of any other trigger logic).
The manual or automatically generated reports (stored in the SSMM) can be transferred to the printer, the PDL/MDDU, the ACARS, PCMCIA (if installed) and the DAR/SAR.
Certain parameters for customer requirements are reprogrammable through the Application Generation Station (AGS), GSE, PDL/MDDU or MCDU.
Following AIDS Reports can be available (depends on A/C configuration):


(1) History Buffer
There is a 20 s history buffer (pre event buffer) for 1000 parameters with an average sampling rate of 4 per second. This buffer is intended to supply data for incorporation into the AIDS reports.

(2) Temporary Buffer for Manual Reports
For reports generated manually through the MCDU for printing or ACARS download a report buffer for one report is provided.

(3) Report Storage
A non-volatile memory for storage of at least 65 AIDS reports is provided.

(4) Overall Report Definition
The following definitions are basically applicable to each AIDS Report:
  • Report number (two digit)
  • Report name (18 alphanumeric string)
  • Print report format programable text (2 header lines)
  • Overall report inhibit (enable/disable)
  • Engine specific trigger inhibits
  • Maximum number of automatically generated reports per flight
  • Maximum number of SSMM stored reports
(5) Report Trigger Definition
For each AI Standard AIDS Report, general and specific trigger definition (Trigger Codes) are done (e.g. exceedance, stability, peak) and are GSE reprogrammable. Within fixed trigger logics only certain constants and limits are reprogrammable (refer to report definition).

(a) Manual Report Request
The FDIMU provides a report selection menu through the MCDU to enable manual selection of reports for immediate generation and output to one of the following destinations:
Output Device ! Output Rule
_______________!_________________________
- Printer ! Print Immediately
- ACARS ! Downlink Immediately
- MDDU ! Dump Immediately
- SAR/PCMCIA ! Store Immediately

(b) Manual Report Trigger through Remote Print Button
A remote print button function causes a generation of specified print reports as a function of flight phase. The respective report trigger logic and the information about incrementing or not incrementing the appropriate report counter is programmable through GSE.

(c) Programmable Report Trigger
Each trigger logic consists of:
  • A programmable trigger logic code
  • A programmable trigger logic tree
Trigger logic trees consist of parameter conditions. The following available combination of parameter conditions are possible:
'AND', 'NAND', 'OR', 'NOR', 'XOR' and 'NOT'

The number of parameter conditions per logic tree is variable, as long as the limitation of 256 parameter conditions is not exceeded.
Parameter conditions have numerical parameters, discrete parameters and hex parameters. In case of Numerical Parameters the result of the parameters condition are determined by a numerical composition, which results in either of the results 'TRUE' or 'FALSE'.

(6) Report Output
AIDS reports are retrieved by some different output devices (Printer, ACARS Down Link, MDDU).

(7) Output Rule
For each AIDS report it is possible to program the applicable output rule through GSE. It is also possible through GSE to define an individual output rule for each type of trigger condition of a report, which is identified by the 4 digit trigger code.

(a) Output Rule No 1.1
The report is stored in the non-volatile report buffer until there is a request for retrieval (e.g. print out, dump on PDL disk, ACARS downlink). After retrieval independent of selected output device the report is marked for deletion.
(b) Output Rule No 2.1
The report is stored in the non-volatile report buffer. As soon as the printer is ready to accept data, the report is printed out and marked for deletion.
(c) Output Rule No 2.2
The report is stored in the non-volatile report buffer and printed out at the end of the flight. After printout, the report is marked for deletion.
(d) Output Rules No 3.X
The report is stored in the non-volatile report buffer. As soon as the ACARS MU accepts the data report is marked for deletion.

(8) Report Format Definitions
(a) Value Presentation
The presentation of the values in the reports refer to the operational range as listed in the parameter list.
E.g. GW = 80000 Kg is printed as 80000.
Negative values begin with an '-'. For positive values the '-' is replaced by an '0' or a digit.
E.g EGT = -55.0 deg. C is printed out as -550,
EGT = +42.5 deg. C is printed out as 0425.

If there are more digits shown in the report layout than the number of digits shown in the parameter list then leading zeroes are included.
E.g. LCIT = 80 deg. C is printed as 0080,
LCIT = -70 deg. C is printed as -070.

A report parameter which is invalid or not updated is replaced with '_' or 'X' characters.

(9) Definition of Engine Hours (EHRS)
EHRS = time between "Main Landing Gear (LH and RH) Compressed/Decompressed".
The EHRS is set to zero when an engine serial number change is recognized.

(10) Definition of Engine Cycle (ECYC)
ECYC = each climb = 1 ECYC
ECYC is incremented by one each time PH 5 is reached.
The ECYC is set to zero when an engine serial number change is recognized.

(11) Definition of Engine Running Time (ERT)
ERT = parameter 7C.1.050.01 engine 1
parameter 7C.2.050.10 engine 2


(12) General Rules for Data Line Identifiers
Each data line in a print report has a two character data line identifier in the most left position (e.g. CC, C1, CE, EC, EE, ...). This identifier is used mainly for data identification on ground. Which data line identifiers are defined in the various reports is shown in the report figures.
(13) History Buffer
There is a 20 s history buffer (pre event buffer) for 1000 parameters with an average sampling rate of 4 per second. This buffer is intended to supply data for incorporation into the AIDS reports.

(14) Temporary Buffer for Manual Reports
For reports generated manually through the MCDU for printing or ACARS download a report buffer for one report is provided.

(15) Report Storage
A non-volatile memory for storage of at least 65 AIDS reports is provided.

(16) Overall Report Definition
The following definitions are basically applicable to each AIDS Report:
  • Report number (two digit)
  • Report name (18 alphanumeric string)
  • Print report format programmable text (2 header lines)
  • Overall report inhibit (enable/disable)
  • Engine specific trigger inhibits
  • Maximum number of automatically generated reports per flight
  • Maximum number of SSMM stored reports
(17) Report Trigger Definition
For each AI Standard AIDS Report, general and specific trigger definition (Trigger Codes) are performed (e.g. exceedance, stability, peak) and are GSE reprogrammable. Within fixed trigger logics only certain constants and limits are reprogrammable (refer to report definition).

(a) Manual Report Request
The FDIMU provides a report selection menu through the MCDU to enable manual selection of reports for immediate generation and output to one of the following destinations:
Output Device ! Output Rule
_______________!_________________________
- Printer ! Print Immediately
- ACARS ! Downlink Immediately
- PDL ! Dump Immediately
- SAR/PCMCIA ! Store Immediately

(b) Manual Report Trigger through Remote Print Button
A remote print button function causes a generation of specified print reports as a function of flight phase. The respective report trigger logic and the information about incrementing or not incrementing the appropriate report counter is programmable through GSE.

(c) Programmable Report Trigger
Each trigger logic consists of:
  • A programmable trigger logic code
  • A programmable trigger logic tree
Trigger logic trees consist of parameter conditions. The following available combination of parameter conditions are possible:
'AND', 'NAND', 'OR', 'NOR', 'XOR' and 'NOT'

The number of parameter conditions per logic tree is variable, as long as the limitation of 256 parameter conditions is not exceeded.
Parameter conditions have numerical parameters, discrete parameters and hex parameters. In case of Numerical Parameters the result of the parameters condition are determined by a numerical composition, which results in either of the results 'TRUE' or 'FALSE'.

(18) Report Output
AIDS reports are retrieved by several different output devices (Printer, ACARS Down Link, PDL).

(19) Output Rule
For each AIDS report it is possible to program the applicable output rule through GSE. It is also possible through GSE to define an individual output rule for each type of trigger condition of a report, which is identified by the 4 digit trigger code.

(a) Output Rule No 1.1
The report is stored in the non-volatile report buffer until there is a request for retrieval (e.g. print out, dump on PDL disk, ACARS downlink). After retrieval independent of selected output device the report is marked for deletion.
(b) Output Rule No 2.1
The report is stored in the non-volatile report buffer. As soon as the printer is ready to accept data, the report is printed out and marked for deletion.
(c) Output Rule No 2.2
The report is stored in the non-volatile report buffer and printed out at the end of the flight. After printout, the report is marked for deletion.
(d) Output Rules No 3.X
The report is stored in the non-volatile report buffer. As soon as the ACARS MU accepts the data report is marked for deletion.

(20) Report Format Definitions
(a) Value Presentation
The presentation of the values in the reports is according to the operational range as listed in the parameter list.
E.g. GW = 80000 Kg is printed as 80000.
Negative values begin with an 'N'. For positive values the 'N' is replaced by an '0' or a digit.
E.g EGT = -55.0 deg. C is printed out as N550,
EGT = +42.5 deg. C is printed out as 0425.

If there are more digits shown in the report layout than the number of digits shown in the parameter list then leading zeroes are included.
E.g. LCIT = 80 deg. C is printed as 0080,
LCIT = -70 deg. C is printed as N070.

A report parameter which is invalid or not updated is replaced with '_' or 'X' characters.

(21) Definition of Engine Hours (EHRS)
EHRS = time between "Main Landing Gear (LH and RH) Compressed/Decompressed".
The EHRS is set to zero when an engine serial number change is recognized.

(22) Definition of Engine Cycle (ECYC)
ECYC = each climb = 1 ECYC
ECYC is incremented by one each time PH 5 is reached.
The ECYC is set to zero when an engine serial number change is recognized.

(23) Definition of Engine Running Time (ERT)
ERT = parameter 7C.1.050.01 engine 1
parameter 7C.2.050.10 engine 2


(24) General Rules for Data Line Identifiers
Each data line in a print report has a two character data line identifier in the most left position (e.g. CC, C1, CE, EC, EE, ...). This identifier is used mainly for data identification on ground. Which data line identifiers are defined in the various reports is shown in the report figures.
K. Standard Header for Print Reports
F Standard Header ** ON A/C NOT FOR ALL
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible (0, 1),
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9,
'.' = checksum.


The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and no. !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID ! means A/C Ident,param. 17.1.301.00, 17.1.302.00, !
! XXXXXX ! 17.1.303.00 !
! ! If the A/C Ident is longer than 6 digits, the first!
! ! digit is not printed out in the AIDS reports. !
! ! If the 7th digit is a blank, then digit 1 to 6 is !
! ! printed instead of 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! DATE (Month/Day) decoded from param. 17.1.260.00 !
! AAA99 ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OCT, 11=NOV, 12=DEC !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! param. 17.1.150.000 !
!--------------!------------------------------------------------------!
! FROM TO ! Identification of City Pair !
! AAAA AAAA ! param. 01.1.040.00, 01.1.041.00, 01.1.042.00 !
!--------------!------------------------------------------------------!
! FLT ! Flight Number (actual) !
! XXXX ! param. 01.1.233.00, 01.2.233.00, 01.1.234.00, !
! ! param. 01.2.234.00, 01.1.235.00, 01.2.235.00 !
! ! param. 01.1.236.00, 01.2.236.00. !
+---------------------------------------------------------------------+
Line 12:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Phase: 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07, 7.1, !
! ! 08, 09 and 10 !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger condition !
! 9999 ! !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !___ 8E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!!_____ 29.1.001.00.18 RH Wing AI/V Pos!
! ! ! !!!! ! !!! 29.2.001.00.18 Closed = 0 !
! ! ! !!!! ! !!!______ 5D.2.061.10.27 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!_______ 6F.2.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 6F.2.066.10.17 Fully Closed = 0!
! ! ! !!!! ! !________ 6F.2.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 6F.2.066.10.15 Fully Closed = 0!
! ! ! !!!! !__________ 29.1.055.01.16 Cross Feed Valve!
! ! ! !!!! 29.2.055.01.16 Pos Fully Clo.=0!
! ! ! !!!!____________ 6F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 6F.1.067.10.15 Fully Close = 0 !
! ! ! !!!_____________ 6F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 6F.2.067.10.17 Fully Closed = 0!
! ! ! !!______________ 5D.2.061.10.28 Eng.1 Nacelle AI!
! ! ! ! Pos. Open = 1 !
! ! ! !_______________ 29.1.001.11.18 LH Wing AI/V Pos!
! ! ! 29.2.001.11.18 Closed = 0 !
! ! !_________________ 8E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! !
+---------------------------------------------------------------------+
! 1 ! APU Bleed V. State param. 7A.1.037.01.11 !
! ! APU Bleed Valve Open =1 !
+---------------------------------------------------------------------+
Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature !
! X999 ! For positive values 'N' is replaced by '0'. !
! ! param. 06.1.211.01 !
! ! 06.2.211.10 !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! param. 06.1.203.01 !
! ! 06.2.203.10 !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! param. 06.1.206.01 !
! ! 06.2.206.10 !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! param. 06.1.205.01 !
! ! 06.2.205.10 !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! param. 02.1.075.00 !
! ! 02.2.075.00 !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! param. 02.1.077.00 !
! ! 02.2.077.00 !
!--------------!------------------------------------------------------!
! DMU/SW ! DMU Ident Code !
! XXXXXX ! X = Engine Type C = CFMI, I = IAE !
! ! X = Engine Version 1 ...8 !
! ! XX = Hardware Vers. A100, A200 !
! ! XX = Software Version (001 ...999) !
+---------------------------------------------------------------------+

F Standard Header ** ON A/C NOT FOR ALL
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible (0, 1),
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9,
'.' = checksum.


The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and no. !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID ! means A/C Ident,param. 17.1.301.00, 17.1.302.00, !
! XXXXXX ! 17.1.303.00 !
! ! If the A/C Ident is longer than 6 digits, the first!
! ! digit is not printed out in the AIDS reports. !
! ! If the 7th digit is a blank, then digit 1 to 6 is !
! ! printed instead of 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! DATE (Month/Day) decoded from param. 17.1.260.00 !
! AAA99 ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OCT, 11=NOV, 12=DEC !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! param. 17.1.150.000 !
!--------------!------------------------------------------------------!
! FROM TO ! Identification of City Pair !
! AAAA AAAA ! param. 01.1.040.00, 01.1.041.00, 01.1.042.00 !
!--------------!------------------------------------------------------!
! FLT ! Flight Number (actual) !
! XXXX ! param. 01.1.233.00, 01.2.233.00, 01.1.234.00, !
! ! param. 01.2.234.00, 01.1.235.00, 01.2.235.00 !
! ! param. 01.1.236.00, 01.2.236.00. !
+---------------------------------------------------------------------+
Line 12:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Phase: 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07, 7.1, !
! ! 08, 09 and 10 !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger condition !
! 9999 ! !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !___ 8E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!!_____ 29.1.001.00.18 RH Wing AI/V Pos!
! ! ! !!!! ! !!! 29.2.001.00.18 Closed = 0 !
! ! ! !!!! ! !!!______ 5D.2.061.10.27 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!_______ 6F.2.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 6F.2.066.10.17 Fully Closed = 0!
! ! ! !!!! ! !________ 6F.2.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 6F.2.066.10.15 Fully Closed = 0!
! ! ! !!!! !__________ 29.1.055.01.16 Cross Feed Valve!
! ! ! !!!! 29.2.055.01.16 Pos Fully Clo.=0!
! ! ! !!!!____________ 6F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 6F.1.067.10.15 Fully Close = 0 !
! ! ! !!!_____________ 6F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 6F.2.067.10.17 Fully Closed = 0!
! ! ! !!______________ 5D.2.061.10.28 Eng.1 Nacelle AI!
! ! ! ! Pos. Open = 1 !
! ! ! !_______________ 29.1.001.11.18 LH Wing AI/V Pos!
! ! ! 29.2.001.11.18 Closed = 0 !
! ! !_________________ 8E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! !
+---------------------------------------------------------------------+
! 1 ! APU Bleed V. State param. 7A.1.037.01.11 !
! ! APU Bleed Valve Open =1 !
+---------------------------------------------------------------------+
Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature !
! X999 ! For positive values 'N' is replaced by '0'. !
! ! param. 06.1.211.01 !
! ! 06.2.211.10 !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! param. 06.1.203.01 !
! ! 06.2.203.10 !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! param. 06.1.206.01 !
! ! 06.2.206.10 !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! param. 06.1.205.01 !
! ! 06.2.205.10 !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! param. 02.1.075.00 !
! ! 02.2.075.00 !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! param. 02.1.077.00 !
! ! 02.2.077.00 !
!--------------!------------------------------------------------------!
! DMU/SW ! DMU Ident Code !
! XXXXXX ! X = Engine Type C = CFMI, I = IAE !
! ! X = Engine Version 1 ...8 !
! ! XX = Hardware Vers. A100, A200 !
! ! XX = Software Version (001 ...999) !
+---------------------------------------------------------------------+

F Standard Header ** ON A/C NOT FOR ALL
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible (0, 1),
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9,
'#' = alternate parameter.

Used description for parameters:
EVM 3D.1.035.10.11
! -- ! --- -- --
! ! ! ! ! !
! ! ! ! ! !
! ! ! ! ! !____ Bit position (if necessary)
! ! ! ! !_______ SDI
! ! ! !__________ Label (Octal)
! ! !______________ System Number
! !________________ Equipment Identifier
!____________________ Name of Computer

The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and number !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID ! Aircraft Identification (Tail Number) !
! XXXXXX ! FDIU 17.1.301.00 characters 1, 2, 3 !
! ! 17.1.302.00 characters 4, 5, 6 !
! ! 17.1.303.00 characters 7 !
! ! If the A/C Ident is longer than 6 digits, the first!
! ! digit is not printed out in the AIDS reports. !
! ! If the 7th digit is a blank, then digit 1 to 6 is !
! ! printed instead of 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! DATE (Month/Day) !
! AAA99 ! MMMDD !
! ! FDIU 17.1.260.00 !
! ! Month is shown with 3 characters: !
! ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OKT, 11=NOV, 12=DEC !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! hh.mm.ss !
! ! FDIU 17.1.150.00 !
!--------------!------------------------------------------------------!
! FROM TO ! Identification of CITY PAIR !
! AAAA AAAA ! 8 characters and the first is left aligned !
! ! FMGC 01.1.040.XX characters 1, 2, 3 of FROM !
! ! 01.2.040.XX# !
! ! !
! ! 01.1.041.XX fourth character of FROM, !
! ! 1 character blank !
! ! 01.2.041.XX# first character of TO !
! ! !
! ! 01.1.042.XX characters 2, 3, 4 of TO !
! ! 01.2.042.XX# !
!--------------!------------------------------------------------------!
! FLT ! Flight Number !
! XXXX ! 10 characters but only the last four numbers are !
! ! used. The number is printed right aligned. Only !
! ! numbers are possible and not used positions contain!
! ! '0'. !
! ! FMGC 01.1.233.00 characters 1, 2 !
! ! 01.2.233.00# !
! ! !
! ! 01.1.234.00 characters 3, 4 !
! ! 01.2.234.00# !
! ! !
! ! 01.1.235.00 characters 5, 6 !
! ! 01.2.235.00# !
! ! !
! ! 01.1.236.00 characters 7, 8 !
! ! 01.2.236.00# !
+---------------------------------------------------------------------+

Line 12:
+----------------------------------------------------------------------+
! Value ! Content Description !
!--------------!-------------------------------------------------------!
! EXSWPN ! Extended Software Part Number !
! ! AA X99 XXXXX 99 99 !
! ! !! --- ----- -- -- !
! ! !! ! ! ! ! !
! ! !! ! ! ! !_ 2 digits of the minor version 2 !
! ! !! ! ! !____ 2 digits of the minor version 1 !
! ! !! ! !_______ Last 5 character of the !
! ! !! ! software PN !
! ! !! !_____________ Last character of the engine !
! ! !! type in the software PN and 2 !
! ! !! characters of the version of the!
! ! !! software PN !
! ! !!_________________ Engine Type: !
! ! ! "C"=CFM, "I"=IAE, "P"=PW !
! ! !__________________ Vendor: "T"=Teledyne !
+----------------------------------------------------------------------+

Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Phase: 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07, 7.1, !
! ! 08, 09 and 10 !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger Condition !
! 9999 ! !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !__ 8E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!!____ 29.1.001.00.18 RH Wing AI/V Pos !
! ! ! !!!! ! !!! 29.2.001.00.18# Closed = 0 !
! ! ! !!!! ! !!!_____ 5D.2.061.10.27 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!______ 6F.2.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 6F.2.066.10.17# Fully Closed = 0!
! ! ! !!!! ! !_______ 6F.2.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 6F.2.066.10.15# Fully Closed = 0!
! ! ! !!!! !_________ 29.1.055.01.16 Cross Feed Valve !
! ! ! !!!! 29.2.055.01.16# Pos Fully Clo.=0!
! ! ! !!!!___________ 6F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 6F.1.067.10.15# Fully Close = 0 !
! ! ! !!!____________ 6F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 6F.2.067.10.17# Fully Closed = 0!
! ! ! !!_____________ 5D.2.061.10.28 Eng.1 Nacelle AI !
! ! ! ! Pos. Open = 1 !
! ! ! !______________ 29.1.001.11.18 LH Wing AI/V Pos !
! ! ! 29.2.001.11.18# Closed = 0 !
! ! !________________ 8E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! !
!--------------!------------------------------------------------------!
! APU ! APU Bleed Valve State !
! 1 ! Bit Status 1 = APU Bleed Valve Open !
! ! ECB 7A.1.037.01.11 !
+---------------------------------------------------------------------+
Line 18:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature !
! X999 ! Negative values are shown with '-' on the first !
! ! position. If not, the first position contains '0'. !
! ! ADIRU 06.1.211.01 !
! ! 06.2.211.10# !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! Negative values are shown with '-' on the first !
! ! position. If not, the first position is used for !
! ! the value. !
! ! ADIRU 06.1.203.01 !
! ! 06.2.203.10# !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! ADIRU 06.1.206.01 !
! ! 06.2.206.10# !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! ADIRU 06.1.205.01 !
! ! 06.2.205.10# !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! FMGC 02.1.075.00 !
! ! 02.2.075.00# !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! FMGC 02.1.077.00 !
! ! 02.2.077.00# !
!--------------!------------------------------------------------------!
! DMU/SW ! DMU and Software Identification !
! XXXXXX ! X = Engine Type C = CFMI, I = IAE, P = PW !
! ! X = Engine Version 1 ...9 !
! ! X = Hardware Vers. 2234320-0X-0X !
! ! XXX = Database Version XXXXXXXXXXXXXXX !
+---------------------------------------------------------------------+

F Standard Header
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible (0, 1),
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9,
'#' = alternate parameter.

Used description for parameters:
EVM 3D.1.035.10.11
! -- ! --- -- --
! ! ! ! ! !
! ! ! ! ! !
! ! ! ! ! !____ Bit position (if necessary)
! ! ! ! !_______ SDI
! ! ! !__________ Label (Octal)
! ! !______________ System Number
! !________________ Equipment Identifier
!____________________ Name of Computer

The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and number !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID ! Aircraft Identification (Tail Number) !
! XXXXXX ! FDIU 17.1.301.00 characters 1, 2, 3 !
! ! 17.1.302.00 characters 4, 5, 6 !
! ! 17.1.303.00 characters 7 !
! ! If the A/C Ident is longer than 6 digits, the first!
! ! digit is not printed out in the AIDS reports. !
! ! If the 7th digit is a blank, then digit 1 to 6 is !
! ! printed instead of 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! DATE (Month/Day) !
! AAA99 ! MMMDD !
! ! FDIU 17.1.260.00 !
! ! Month is shown with 3 characters: !
! ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OCT, 11=NOV, 12=DEC !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! hh.mm.ss !
! ! FDIU 17.1.150.00 !
!--------------!------------------------------------------------------!
! FROM TO ! Identification of CITY PAIR !
! (FRTO) ! 8 characters and the first is left aligned !
! AAAA AAAA ! FMGC 01.1.040.XX characters 1, 2, 3 of FROM !
! ! 01.2.040.XX# !
! ! !
! ! 01.1.041.XX fourth character of FROM, !
! ! 1 character blank !
! ! 01.2.041.XX# first character of TO !
! ! !
! ! 01.1.042.XX characters 2, 3, 4 of TO !
! ! 01.2.042.XX# !
!--------------!------------------------------------------------------!
! FLT ! Flight Number !
! XXXX ! 10 characters but only the last four numbers are !
! ! used. The number is printed right aligned. Only !
! ! numbers are possible and not used positions contain!
! ! '0'. !
! ! FMGC 01.1.233.00 characters 1, 2 !
! ! 01.2.233.00# !
! ! !
! ! 01.1.234.00 characters 3, 4 !
! ! 01.2.234.00# !
! ! !
! ! 01.1.235.00 characters 5, 6 !
! ! 01.2.235.00# !
! ! !
! ! 01.1.236.00 characters 7, 8 !
! ! 01.2.236.00# !
+---------------------------------------------------------------------+

Line 12:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Phase: 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07, 7.1, !
! ! 08, 09 and 10 !
! ! DMU (based on flight phase from FWC) !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! DMU !
! ! 99999 !
! ! -- -- !
! ! ! !____ Report type number of the previously !
! ! ! generated report. !
! ! !_______ Total number of previously generated !
! ! reports. Automatically or via !
! ! REMOTE PRINT button. !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger Condition !
! 9999 ! !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !__ 8E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!! (refer to remark)!
! ! ! !!!! ! !!!!____ 29.1.001.00.18 RH Wing AI/V Pos !
! ! ! !!!! ! !!! 29.2.001.00.18# Closed = 0 !
! ! ! !!!! ! !!!_____ 5D.2.061.10.27 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!______ 6F.1.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 6F.2.066.10.17# Fully Closed = 0!
! ! ! !!!! ! !_______ 6F.1.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 6F.2.066.10.15# Fully Closed = 0!
! ! ! !!!! !_________ 6F.1.055.01.16 Cross Feed Valve !
! ! ! !!!! 6F.2.055.10.16# Pos Fully Clo.=0!
! ! ! !!!!___________ 6F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 6F.1.067.10.15# Fully Close = 0 !
! ! ! !!!____________ 6F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 6F.2.067.10.17# Fully Closed = 0!
! ! ! !!_____________ 5D.2.061.10.28 Eng.1 Nacelle AI !
! ! ! ! Pos. Open = 1 !
! ! ! !______________ 29.1.001.11.18 LH Wing AI/V Pos !
! ! ! 29.2.001.11.18# Closed = 0 !
! ! !________________ 8E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! (refer to remark) !
! ! Remark: If the RH or LH Pack Flow is desplayed in !
! ! lbs/sec, the range is 0.0 to 9.9 lbs/sec. !
! ! If the RH or LH Pack Flow value is greater !
! ! than the range display "EE". !
!--------------!------------------------------------------------------!
! APU ! APU Bleed Valve State !
! 1 ! Bit Status 1 = APU Bleed Valve Open !
! ! ECB 7A.1.037.01.11 !
+---------------------------------------------------------------------+
Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature !
! X999 ! Negative values are shown with 'N' on the first !
! ! position. Otherwise the first position contains !
! ! '0'. !
! ! -60.0 to 99.9 deg. C !
! ! ADIRU 06.1.211.01 !
! ! 06.2.211.10# !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! Negative values are shown with 'N' on the first !
! ! position. Otherwise the first position is used for !
! ! the value. !
! ! ADIRU 06.1.203.01 !
! ! 06.2.203.10# !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! 30 to 450 kts !
! ! 06.1.206.01 !
! ! 06.2.206.10# !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! 0.100 to 0.999 !
! ! ADIRU 06.1.205.01 !
! ! 06.2.205.10# !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! 0 to 9000 * 10 kg (0 to 1980 * 100 lbs) !
! ! 02.1.075.00 !
! ! 02.2.075.00# !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! 0 to 35.0 %MAC !
! ! FMGC 02.1.077.00 !
! ! 02.2.077.00# !
!--------------!------------------------------------------------------!
! DMU/SW ! DMU and Software Partnumber !
! XXXXXX ! XXXXXX !
! ! !!---- !
! ! !! ! !___ Database Version XXXX-XXXX !
! ! !! !_____ Hardware Vers. A100, A200 !
! ! !!_______ Engine Version 1...8 !
! ! !________ Engine type C=CFMI, I=IAE !
+---------------------------------------------------------------------+

F Standard Header ** ON A/C NOT FOR ALL
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible : 0, 1,
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9.

Used description for parameters:
EVM 3D.1.035.10.11 #
--- -- - --- -- -- -
! ! ! ! ! ! !
! ! ! ! ! ! !__ Alternate Parameter (if necessary)
! ! ! ! ! !____ Bit position (if necessary)
! ! ! ! !_______ SDI
! ! ! !__________ Label (Octal)
! ! !______________ System Number
! !________________ Equipment Identifier
!____________________ Name of Computer

The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and number !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID (ACID)! Aircraft Identification (Tail Number) !
! XXXXXX ! Source: CFDIU 017.1.301.00 characters 1, 2, 3 !
! ! 017.1.302.00 characters 4, 5, 6 !
! ! 017.1.303.00 characters 7 !
! ! Format: 6 digits are printed, the first digit is !
! ! left aligned. !
! ! If the A/C Ident is longer than 6 digits, !
! ! the first digit is not printed out in the !
! ! AIDS reports. If the 7th digit is a blank, !
! ! then digit 1 to 6 is printed instead of !
! ! 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! Date (Month/Day) !
! AAA99 ! Format: MMMDD !
! ! Month is shown with 3 characters: !
! ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OKT, 11=NOV, 12=DEC !
! ! Source: FDIU 017.1.260.00 !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! Format: hh.mm.ss !
! ! Source: FDIU 17.1.150.00 !
!--------------!------------------------------------------------------!
!FROM TO (FRTO)! Identification of CITY PAIR !
!AAAA AAAA ! Format: 8 characters, the first is left aligned. !
! ! Source: FMGC001.1.040.XX characters 1, 2, 3 of !
! ! FROM !
! ! 001.2.040.XX# !
! ! 001.1.041.XX fourth character of FROM,!
! ! 1 character blank !
! ! 001.2.041.XX# first character of TO !
! ! !
! ! 001.1.042.XX characters 2, 3, 4 of TO !
! ! 001.2.042.XX# !
!--------------!------------------------------------------------------!
! FLT ! Flight Number !
! XXXX ! Format: 10 digits but only the last four numbers !
! ! are used. The number is printed right !
! ! aligned. Only numbers are possible and not!
! ! used positions contain '0'. !
! ! Source: FMGC 001.1.233.00 characters 1, 2 !
! ! 001.2.233.00# !
! ! !
! ! 001.1.234.00 characters 3, 4 !
! ! 001.2.234.00# !
! ! !
! ! 001.1.235.00 characters 5, 6 !
! ! 001.2.235.00# !
! ! !
! ! 001.1.236.00 characters 7, 8 !
! ! 001.2.236.00# !
+---------------------------------------------------------------------+

Line 12:
+----------------------------------------------------------------------+
! Value ! Content Description !
!--------------!-------------------------------------------------------!
! EXSWPN ! Extended Software Part Number !
! ! Format: !
! ! AA X99 XXXXX 99 99 !
! ! !! --- ----- -- -- !
! ! !! ! ! ! ! !
! ! !! ! ! ! !_ 2 digits of the minor version 2 !
! ! !! ! ! !____ 2 digits of the minor version 1 !
! ! !! ! !_______ Last 5 character of the !
! ! !! ! software PN !
! ! !! !_____________ Last character of the engine !
! ! !! type in the software PN and 2 !
! ! !! characters of the version of the!
! ! !! software PN !
! ! !!_________________ Engine Type: "W"-PW !
! ! ! !
! ! !__________________ Vendor: "S"- Sagem !
! ! !
! ! Remark: Example EXSWPN for SAGEM !
! ! SW 030 03410 0001 !
! ! !! --- ----- ---- !
! ! !! ! ! ! !
! ! !! ! ! !____ 3410/0001 version of the data- !
! ! !! ! ! ---- base !
! ! !! ! ! !
! ! !! ! !_______ 0 + 3410/0001 DB Number with !
! ! !! ! ---- leading "0" !
! ! !! !_____________ PN: 360-04020-030 !
! ! !! --- !
! ! !!_________________ W PW Engine PW1100G !
! ! ! - !
! ! !__________________ Sagem !
! ! - !
! ! !
+----------------------------------------------------------------------+

Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Format: Phase 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07,!
! ! 7.1, 08, 09 and 10 !
! ! !
! ! Source: FDIMU (based on flight phase from FWC) !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! 99999 !
! ! -- -- !
! ! Total number of generated reports._______! ! !
! ! Automatically or through REMOTE PRINT ! !
! ! button. ! !
! ! ! !
! ! Report type number of the report __________! !
! ! generated before. !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger Condition !
! 9999 ! Format: Logical code number which has triggered !
! ! the report. !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !__ 08E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!! (refer to remark)!
! ! ! !!!! ! !!!!____ 029.1.001.00.18 RH Wing AI/V Pos!
! ! ! !!!! ! !!! 029.2.001.00.18# Closed = 0 !
! ! ! !!!! ! !!!_____ 07B.2.105.XX.18 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!______ 06F.2.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 06F.2.066.10.17# Fully Closed =0!
! ! ! !!!! ! !_______ 06F.2.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 06F.2.066.10.15# Fully Closed =0!
! ! ! !!!! !_________ 029.1.055.01.16 Cross Feed Valve!
! ! ! !!!! 029.2.055.01.16# Pos Fully Clo=0!
! ! ! !!!!___________ 06F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 06F.1.067.10.15# Fully Close = 0!
! ! ! !!!____________ 06F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 06F.2.067.10.17# Fully Closed =0!
! ! ! !!_____________ 07B.1.105.XX.18 Eng.1 Nacelle AI!
! ! ! ! Pos. Open = 1 !
! ! ! !______________ 029.1.001.11.18 LH Wing AI/V Pos!
! ! ! 029.2.001.11.18# Closed = 0 !
! ! !________________ 08E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! (refer to remark)!
! ! !
! ! Remark: If the RH or LH Pack Flow is displayed in !
! ! lbs/sec, the range is 0.0 to 9.9 lbs/sec. !
! ! If the RH or LH Pack Flow value is more !
! ! than the range display 'EE'. !
!--------------!------------------------------------------------------!
! APU ! APU Bleed Valve State !
! 1 ! Format: Bit Status 1 = APU Bleed Valve Open !
! ! Source: ECB 07A.1.037.01.11 !
+---------------------------------------------------------------------+
Line 18:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature from the aircraft !
! X99.9 ! Format: Negative values are shown with a special !
! ! sign character on the first position. !
! ! If not, the first position is filled by '0'!
! ! -60.0 to 99.9 ??C !
! ! Source: ADIRU 006.1.211.01 !
! ! 006.2.211.10# !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013 mbar) !
! X9999 ! Format: Negative values are shown by a special sign!
! ! character on the first position. !
! ! If not, first position contains a '0'. !
! ! !
! ! Source: ADIRU 06C.1.310.01 !
! ! 06C.2.310.10# !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! Format: 30to 450 kts !
! ! !
! ! Source: ADIRU 006.1.206.01 !
! ! 006.2.206.10# !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! Format: 0.100 to 0.999 !
! ! !
! ! Source: ADIRU 006.1.205.01 !
! ! 006.2.205.10# !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! Format: 0 to 9000 * 10 kg (0 to 1980 * 100 lbs) !
! ! !
! ! Source: FMGC 002.1.075.00 !
! ! 002.2.075.00# !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 99.9 ! Format: 0.0 to 35.0 % MAC !
! ! !
! ! Source: FMGC 002.1.077.00 !
! ! 002.2.077.00# !
!--------------! -----------------------------------------------------!
! DMU/SW ! DMU and Software Identification !
! XXXXXX ! Format: XXXXXX !
! ! !!!--- !
! ! Engine Type W = PW ________________!!! ! !
! ! !! ! !
! ! Engine Version 1 ...9 _______________!! ! !
! ! ! ! !
! ! Hardware Vers. 2234320-02-02 _________! ! !
! ! Database Version XXXXXXXXXXXXXXX _______! !
! ! !
! ! Source: FDIMU !
! ! Remark: Example for DMU/SW Sagem !
! ! W 1 2 01 !
! ! PW Engine: ___________________! ! ! -- !
! ! PW Engine Type 1 _____________________! ! ! !
! ! H/W A200 _______________________! ! !
! ! Databa Version __________________________! !
! ! 0001-0001 !
+---------------------------------------------------------------------+

F Standard Header ** ON A/C NOT FOR ALL
A standard header to be printed on each report is installed.
The header data is taken at the time when the related report is generated. These symbols are used for the value fields:

'A' = any character in the range from A..Z,
'1' = digits possible (0, 1),
'9' = any digit in the range from 0..9,
'X' = any character or digit in the range from A..Z,
and 0 .. 9,
'#' = Alternate parameter.

Used description for parameters:
EVM 3D.1.035.10.11
! -- ! --- -- --
! ! ! ! ! !
! ! ! ! ! !
! ! ! ! ! !____ Bit position (if necessary)
! ! ! ! !_______ SDI
! ! ! !__________ Label (Octal)
! ! !______________ System Number
! !________________ Equipment Identifier
!____________________ Name of Computer

The content of a header is as below:
Line 1, 3, 5:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! The content is free-programmable to enable air- !
! ! line specific messages. !
+---------------------------------------------------------------------+

Line 7:
+---------------------------------------------------------------------+
! Value ! Content Description !
!------------!--------------------------------------------------------!
! ! Report identification title and number !
+---------------------------------------------------------------------+

Line 9:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! A/C ID ! Aircraft Identification (Tail Number) !
! XXXXXX ! FDIU 17.1.301.00 characters 1, 2, 3 !
! ! 17.1.302.00 characters 4, 5, 6 !
! ! 17.1.303.00 characters 7 !
! ! 6 digits are printed, the first digit is left !
! ! aligned. !
! ! If the A/C Ident is longer than 6 digits, the first!
! ! digit is not printed out in the AIDS reports. !
! ! If the 7th digit is a blank, then digit 1 to 6 is !
! ! printed instead of 2 to 7. !
!--------------!------------------------------------------------------!
! DATE ! DATE (Month/Day) !
! AAA99 ! MMMDD !
! ! FDIU 17.1.260.00 !
! ! Month is shown with 3 digits: !
! ! 01=JAN, 02=FEB, 03=MAR, 04=APR, 05=MAY, 06=JUN, !
! ! 07=JUL, 08=AUG, 09=SEP, 10=OCT, 11=NOV, 12=DEC !
! ! Parameter 'DATE' is defined for WEFA Report <90> in!
! ! a different way as for all other reports. !
!--------------!------------------------------------------------------!
! UTC ! Universal Time Coordinated (Hours/Minutes/Seconds) !
! 999999 ! hh.mm.ss !
! ! FDIU 17.1.150.00 !
!--------------!------------------------------------------------------!
! FROM TO ! Identification of CITY PAIR !
! (FRTO) ! 8 characters and the first is left aligned !
! AAAA AAAA ! FMGC 01.1.040.XX characters 1, 2, 3 of FROM !
! ! 01.2.040.XX# !
! ! !
! ! 01.1.041.XX fourth character of FROM, !
! ! 1 character blank !
! ! 01.2.041.XX# first character of TO !
! ! !
! ! 01.1.042.XX characters 2, 3, 4 of TO !
! ! 01.2.042.XX# !
!--------------!------------------------------------------------------!
! FLT ! Flight Number !
! XXXX ! 10 characters but only the last four numbers are !
! ! used. The number is printed right aligned. Only !
! ! numbers are possible and not used positions are !
! ! filled with zeros. !
! ! FMGC 01.1.233.00 characters 1, 2 !
! ! 01.2.233.00# !
! ! !
! ! 01.1.234.00 characters 3, 4 !
! ! 01.2.234.00# !
! ! !
! ! 01.1.235.00 characters 5, 6 !
! ! 01.2.235.00# !
! ! !
! ! 01.1.236.00 characters 7, 8 !
! ! 01.2.236.00# !
+---------------------------------------------------------------------+

Line 12:
+---------------------------------------------------------------------+
! Value ! Content Description !
!---------------!------------------------------------------------------!
! EXSWPN(ESWPN) ! Extended Software Part Number !
! AAX99XXXXX9999! (Extende Software Identification) !
! ! DMU !
! ! !
! ! A A X99 XXXXX 9999 !
! ! - - --- ----- ---- !
! ! ! ! ! ! ! !
! ! ! ! ! ! ! !
! ! ! ! ! ! !____4 digits of the version of the !
! ! ! ! ! ! database !
! ! ! ! ! !__________4 digits of the Database Number!
! ! ! ! ! with a leading '0" !
! ! ! ! !________________Last 3 digits of the system !
! ! ! ! software PN !
! ! ! !___________________Engine Type 'C'= CFMI 'I'= IAE !
! ! ! 'P' = PW. !
! ! !_____________________Vendor 'S' = SAGEM !
! ! !
+----------------------------------------------------------------------+

Line 15:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! PH ! DMU Flight Phase !
! 99 ! Phase: 01, 1.1, 02, 03, 04, 05, 5.1, 06, 07, 7.1, !
! ! 08, 09 and 10 !
! ! DMU (based on flight phase from FWC) !
!--------------!------------------------------------------------------!
! CNT ! Report Counter and Previous Report Number !
! 99999 ! DMU !
! ! 99999 !
! ! -- -- !
! ! ! !____ Report type number of the previously !
! ! ! generated report. !
! ! !_______ Total number of previously generated !
! ! reports. Automatically or through !
! ! REMOTE PRINT button. !
!--------------!------------------------------------------------------!
! CODE ! Code number for the respective trigger Condition !
! 9999 ! !
!--------------!------------------------------------------------------!
! BLEED STATUS ! Discrete and numeric coded information !
! ! 99 1111 1 1111 99 !
! ! ^^ !!!! ! !!!! ^^ !
! ! ! !!!! ! !!!! !__ 8E.2.126.00 RH Pack Flow !
! ! ! !!!! ! !!!! 0 to 1.0 kg/sec.!
! ! ! !!!! ! !!!! (refer to remark)!
! ! ! !!!! ! !!!!____ 29.1.001.00.18 RH Wing AI/V Pos !
! ! ! !!!! ! !!! 29.2.001.00.18# Closed = 0 !
! ! ! !!!! ! !!!_____ 5D.2.061.10.27 Eng.2 Nascelle !
! ! ! !!!! ! !! AI Pos. Open = 1!
! ! ! !!!! ! !!______ 6F.1.066.01.17 Eng.2 PRV Pos. !
! ! ! !!!! ! ! 6F.2.066.10.17# Fully Closed = 0!
! ! ! !!!! ! !_______ 6F.1.066.01.15 Eng.2 HPV Pos. !
! ! ! !!!! ! 6F.2.066.10.15# Fully Closed = 0!
! ! ! !!!! !_________ 6F.1.055.01.16 Cross Feed Valve !
! ! ! !!!! 6F.2.055.10.16# Pos Fully Clo.=0!
! ! ! !!!!___________ 6F.1.067.01.15 Eng.1 HPV Pos. !
! ! ! !!! 6F.1.067.10.15# Fully Close = 0 !
! ! ! !!!____________ 6F.1.067.01.17 Eng.1 PRV Pos. !
! ! ! !! 6F.2.067.10.17# Fully Closed = 0!
! ! ! !!_____________ 5D.2.061.10.28 Eng.1 Nacelle AI !
! ! ! ! Pos. Open = 1 !
! ! ! !______________ 29.1.001.11.18 LH Wing AI/V Pos !
! ! ! 29.2.001.11.18# Closed = 0 !
! ! !________________ 8E.1.126.11 LH Pack Flow !
! ! 0 to 1.0 kg/sec.!
! ! (refer to remark) !
! ! Remark: If the RH or LH Pack Flow is desplayed in !
! ! lbs/sec, the range is 0.0 to 9.9 lbs/sec. !
! ! If the RH or LH Pack Flow value is greater !
! ! than the range display "EE". !
!--------------!------------------------------------------------------!
! APU ! APU Bleed Valve State !
! 1 ! Bit Status 1 = APU Bleed Valve Open !
! ! ECB 7A.1.037.01.11 !
+---------------------------------------------------------------------+
Line 18:
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! TAT ! Total Air Temperature !
! X999 ! Negative values are shown with 'N' on the first !
! ! position. If not, the first position contains '0'. !
! ! -60.0 to 99.9 deg. C !
! ! ADIRU 06.1.211.01 !
! ! 06.2.211.10# !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! Negative values are shown with 'N' on the first !
! ! position. If not, the first position is used for !
! ! the value. !
! ! ADIRU 06.1.203.01 !
! ! 06.2.203.10# !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! 30 to 450 kts !
! ! 06.1.206.01 !
! ! 06.2.206.10# !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! 0.100 to 0.999 !
! ! ADIRU 06.1.205.01 !
! ! 06.2.205.10# !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! 0 to 9000 * 10 kg (0 to 1980 * 100 lbs) !
! ! 02.1.075.00 !
! ! 02.2.075.00# !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! 0 to 35.0 %MAC !
! ! FMGC 02.1.077.00 !
! ! 02.2.077.00# !
!--------------!------------------------------------------------------!
! DMU/SW ! DMU and Software Partnumber !
! XXXXXX ! XXXXXX !
! ! !!---- !
! ! !! ! !___ Database Version XXXX-XXXX !
! ! !! !_____ Hardware Vers. A100, A200 !
! ! !!_______ Engine Version 1...8 !
! ! !________ Engine type C=CFMI, I=IAE !
+---------------------------------------------------------------------+

(1) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! AC I/D ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! DATE ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! UTC ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! FROM TO ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! FLT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! EXSWPN ! Extended Software Part Number. !
!--------------!------------------------------------------------------!
! PH ! Actual PH at the moment of trigger. !
!--------------!------------------------------------------------------!
! CNT ! Is calculated by DMU when the report is !
! ! triggered. !
!--------------!------------------------------------------------------!
! CODE ! Actual trigger code. !
!--------------!------------------------------------------------------!
! BLEED STATUS! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! APU ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! TAT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! ALT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! CAS ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! MN ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! GW ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! CG ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! DMU/SW ! Current Software number. !
+---------------------------------------------------------------------+

L. AIDS Data Recording
The FDIMU is able to record AIDS data on a external Digital AIDS Recorder (DAR) and on an FDIMU integrated Smart AIDS Recorder (SAR) or on the PCMCIA card. For the purpose of data recording the FDIMU provide 16 independent SAR recording channels on the SSMM. In addition 8 DAR Recording channels are provided. All record channels can be processed simultaneous. The recording is triggered either automatically from the report or manually from the MCDU or remote print button. The trigger condition is programmable through the GSE.
The FDIMU records AIDS data on an external DAR (Digital AIDS Recorder) and/or a SAR (Smart AIDS Recorder, integrated in the FDIMU). The storage medium of the DAR is a magnetic tape cartridge or an optical disk. The SAR uses solid state mass memory (SSMM) for data storage.

Continuous, intermittent (only DAR) or event controlled data-recording is possible. Thus, a set of start and stop triggers are individually user programmable for each recording channel.

A SAR file contains the data of an SAR data collection that starts from the occurrence of an associated start trigger and ends at the occurrence of an associated stop trigger.

Due to the limited storage capacity of the FDIMU internal solid state mass memory (SSMM) used by the SAR, SAR recording data must be compressed with an appropriate data compression.

SAR or DAR recording is done independent of the SSM status of the parameters to be recorded.
M. Smart Access Recorder
The SAR is a part of the DMU. External ARINC-429 or internal parameters from the FDIMU can store in compressed form. The memory is a 2.0 MByte Solid State Mass Memory (SSMM).

Four different recording functions are possible:

Data Recording

  • Storage of up to four user predefined datasets (each up to 128 samples per second) with pre event between a start event and a stop event.
  • 25 start/stop events are supplied.
  • The data is collected for each trigger event with up to 5 minutes of history data.
Extended Troubleshooting

  • Storage of up to four user predefined datasets (each up to 128 samples per second) with pre event data between a start event and a stop event.
  • 25 events are supplied.
  • The data is collected for each event of up to 5 minutes of history data.
Event Recording

  • Storage, when an event is found, of a user predefined data set (15 selectable parameters) specific for each event.
  • Up to 50 different events are supplied.
General Purpose Recording

  • Storage up to 8 user defined datasets between a start event and a stop event and, if selected, pre event data of up to 1 minute for each recording.
  • 50 start/stop events are supplied.
  • This function is only available with insertion of an appropriate PCMCIA card.
(1) SAR History Buffer
For each recording channel a history buffer is provided to facilitate pre-event recording. With the appropriate selection of the sampling rate and number of parameters, the history buffer provides pre-event recording. It is possible to enable/disable individually and independently each event through GSE or through ACARS uplink.
(2) SAR Start/Stop Control
(a) Manual Start/Stop Control

It is possible to start or stop the SAR recording channel manually through the MCDU. A menu for manual request of SAR recording is supplied. This menu provides selective Run/Stop control for each SAR recording function.

Manual start/stop control of the SAR is independent from the GSE programmed automatically trigger conditions.

It is possible to start the SAR recording manually even if automatically triggered recording is active. In this case the recording may not be stopped until both, the manual stop command and all affected automatic stop trigger conditions have become true.

If an automatically trigger becomes true during manually triggered recording, the recording also continues, until both, the manual stop command and all affected automatic stop trigger conditions have become true.

A manually initiated recording is only be stopped by:
  • Manual stop command
  • DMU power interrupt more than 60 seconds.
  • Max. recording time limit of SAR channel is exceeded.

(b) Automatic Start/Stop Trigger

The start and stop trigger condition for the SAR is programmable on the GSE and supplied to the DMU by the setup data base.
An automatically triggered recording is stopped by:
  • The associated stop trigger condition
  • Max. recording time limit of SAR channel is exceeded.
(3) Data Retrieval
A download of AIDS reports and SAR files, which are stored on the SSMM or recorded on the PCMCIA card (if installed) through the MDDU or PDL is possible. For data retrieval the disk must be prepared by the AGS / GSE. The data dump is started manually through the MCDU menu or automatically.
The recording is aborted in case of following conditions:
  • Recording time exceeds AGS / GSE defined limit
  • To be downloaded data exceeds disc memory space.
N. Digital AIDS Recorder (DAR)
F Wireless Ground Link (WGL)-Digital AIDS Recorder (DAR) ** ON A/C NOT FOR ALL
F WGL-DAR Functional Block Diagram ** ON A/C NOT FOR ALL
F WGL-DAR - Interface ** ON A/C NOT FOR ALL
O. Wireless Ground Link - Digital AIDS Recorder (WGL-DAR)
F Wireless Ground Link (WGL)-Digital AIDS Recorder (DAR) ** ON A/C NOT FOR ALL
F WGL-DAR Functional Block Diagram ** ON A/C NOT FOR ALL
F WGL-DAR - Interface ** ON A/C NOT FOR ALL
(1) General
The WGL-DAR is used to record data from different aircraft systems on standard Compact Flash (CF) cards for on ground performance, maintenance tasks or condition monitoring tasks. The WGL-DAR can also transmit these data through a wireless ground link to a ground station.
(2) WGL-DAR Construction
(a) Major Component Characteristics
The WGL-DAR form factor is 4 MCU in accordance with ARINC 600 specification. The weight is less than 4.5 kg. The WGL-DAR uses up to 19 watts during flight phase, when radios are off and 21-23 watts when radios are on (ground link transmission).
(b) Front Panel
The front panel of the WGL-DAR has:
  • A 32 character alphanumeric display
  • A fail indicator
  • Four function buttons (MODE, +, - and SEL)
  • A RJ-11 Serial port
  • A RJ-45 Ethernet port
  • A CF card slot
  • A Removable SIM Module (RSM)
  • Two antenna interfaces.
(c) Storage Media
All the data supplied by different aircraft systems is recorded on 1 standard CF card (2TV1). The storage capacity of this card is 8GB.
A different CF card (2TV2) contains the operational software (2TVSW2) of the WGL-DAR. The media disk (2TVMD2) must be kept in the disk storage box in the cockpit as a back-up of the operational software of the WGL-DAR.
(3) WGL-DAR Functions
(a) WGL-DAR Recording
The FDIMU sends HARVARD BIPHASE data to the WGL-DAR. The interface board of the WGL-DAR receives the data and extracts the clock data. The Central Processing Unit (CPU) of the WGL-DAR converts the data and stores them on the CF card.
(b) Wireless Data Transmission
The wireless transmission mode of the WGL-DAR for recorded data is active when the aircraft is on the ground. When the wireless transmission mode is enabled the WGL-DAR first checks whether there are any recorded data in need of transmission. The WGL-DAR sends the data in the subsequent order to the ground station:
1 Any data that were previously abnormally transmitted in the middle of a data transmission.
2 Any new recorded data from the last transmission time.
(c) Data Compression
Prior to the transmission, the WGL-DAR compresses the recorded flight data. Each recording of the flight data is stored into different compressed files.
(d) Data Encryption
After the compression, the data are encrypted for the wireless transmission.
(e) Data Transfer
The WGL-DAR sends the encrypted data to the ground station. The transmission starts as soon as the connection between the WGL-DAR and the ground station is done.
The WGL-DAR uses the 3G, EDGE and GPRS networks all around the world to transmit the recorded flight data. It automatically selects the cellular frequencies related to the location of the aircraft at the moment of the data transmission.
(f) BITE
The WGL-DAR contains a BITE to do self-tests, qualitative diagnostics collection and test status reports. In case of discrepancies, the WGL-DAR sends a status signal to the FDIMU.
(4) Controls and Indicators
(a) Manual Start/Stop Control
It is possible to start or stop the recording of aircraft data on the WGL-DAR manually via the MCDU in the cockpit.
(b) Automatic Start/Stop Control
It is also possible to start or stop the recording of aircraft data on the WGL-DAR automatically by special trigger conditions. You can program the trigger conditions on a Ground Support Equipment (GSE) and supply them to the FDIMU by the FDIMU setup data base. The FDIMU then controls the recording of aircraft data on the WGL-DAR.
(c) WGL-DAR Front-Panel Controls and Indicators
The WGL-DAR has different controls and indicators on the front panel to show or modify its status:

  • LCD Display
    The 32-character display shows WGL-DAR low level failures, status messages and gives control/guidelines for the menu/mode functions of the WGL-DAR.
  • FAIL Indicator
    The amber indicator on the front panel comes on when a major failure occurs in the WGL-DAR (hardware fault, missing configuration files or the CF card is full).
  • MODE button
    The MODE button returns the display to the primary display mode that the WGL-DAR is currently in, or the next highest menu display.
  • SEL button
    The SEL button is used to enter into the selected menu. It is also used to confirm any changes made to the WGL-DAR.
  • + and - buttons
    The + (PLUS) and - (MINUS) buttons are used to step through the different menus.
P. AGS Functions
The Ground Support Equipment (GSE) for the FDIMU is based on an IBM-PC compatible computer with the operational software WINDOWS. The GSE computer is able to read 3.5 inch double-side high-density magnetic-disks with formatted data of at least 1.44 Mbytes.
The FDIMU vendor supplies appropriate FDIMU ground support software for the GSE, which has these functions:
  • Generation and editing of the FDIMU setup data base
  • Retrieval of compressed SAR data
  • Retrieval of stored AIDS Reports
  • Configuration Management Control and load history status.

The Ground Support Equipment (GSE) for the FDIMU (DMU-part) is based on an IBM-PC compatible computer with the operating system Microsoft Windows 95. The GSE computer is able to read 3.5 inch double-side high-density magnetic-disks with formatted data of minimum 1.44 Mbytes.
The FDIMU vendor supplies appropriate FDIMU ground support software for the GSE, which has these functions:
  • Generation and editing of the FDIMU setup data base
  • Retrieval of compressed SAR data
  • Retrieval of stored AIDS Reports
  • Configuration Management Control and load history status.

(1) GSE Readout
The GSE readout function is a ground-based software application that provides the display and printout of AIDS collected information (AIDS reports and SAR files) using a DMU / FDIMU external IBM compatible personal computer. AIDS data dump disks are provided to extract AIDS reports and/or compressed SAR files for decompression and for display/printout.
(2) GSE Reconfiguration
The GSE reconfiguration function is a ground-based software application that is used for the reprogramming of certain aspects of the AIDS functions using a DMU / FDIMU external IBM compatible personal computer.
Q. MDDU/PDL Functions
The DMU / FDIMU has an interface to the MDDU (if installed), which is compatible to the Airborne-Computer High-Speed Data-Loader according to ARINC 615. The MDDU is provided either by an Airborne Data Loader (ADL) or a Portable Data Loader (PDL).
In case of the ADL option, the MDDU is permanently installed in the aircraft cockpit. If a PDL is used for the MDDU, only a connector is installed in the cockpit.
The PDL is connected to this connector only on demand. A discrete signal indicates, that the MDDU is available for the DMU / FDIMU. Each time a plug from a PDL is connected to the DMU / FDIMU, the specific signal pin is connected to ground. This indicates the DMU / FDIMU, that a communication for up- and download from and to the PDL is possible.
It is possible to connect a PDL directly to the test connector on the front of the DMU / FDIMU by the use of an adapter cable.
The MDDU provides the following tasks:
  • Download of SAR channels
  • Download of AIDS reports, which are stored in the DMU / FDIMU internal solid state memory
  • Upload of the DMU / FDIMU system software
  • Upload of the setup data base.

R. ACARS Functions
The DMU / FDIMU is able to manage different functions to send data through ACARS to the ground (Downlink) or to receive data through ACARS from the ground (Uplink).
The following functions for downlink and uplink messages are given as below:
Downlink (manually and automatically):
* AIDS Reports
either manual or automatically initiated reports
* Advisory Messages
- due to SAR trigger condition
>> Data recording
>> Extended troubleshooting
>> Event recording
- due to SAR memory dump status
>> Data recording - memory dump successful
>> Data recording - memory dump unsuccessful
>> Event recording - memory dump successful
>> Event recording - memory dump unsuccessful
>> Extended troubleshooting - memory dump successful
>> Extended troubleshooting - memory dump unsuccessful
response on uplink request:
* AIDS reports
- immediately initiated
* List of data
- List of temporary changes
- SAR statistic
- SW configuration load status.
* Acknowledgement of
- Temporary changes on uplink request
- Temporary changes return to default
- Activation of predefined function
- Modification of Eng. and APU data (ESN, Eng. Cycle Counter)
- Enable/Disable of SAR trigger messages

Uplink:
* Downlink of reports
- Activation of immediate generation and downlink
* Request for downlink of list of data
- List of temporary changes
- SAR statistic
- SW configuration load status.
* Activation of predefined functions
- Reports due to predefined logic
- Reset delta EGT
* Activation/Inhibit of Messages
- SAR trigger messages
* Reprogramming of functions
- Temporary changes of limits and constants
- Temporary changes return to default
- Change of APU and engine serial number and associated hours and cycle
counters.


(1) Format of AIDS Reports for ACARS Downlink

All reports transmitted to ACARS are stripped of information which is not necessary for ACARS. Thus only the data lines shown by Line Identifier are transmitted.

You must provide a GSE programmable switch to select if you want to ignore the line checksums for ACARS downlink.
Default Setting: Omit Checksums in Downlink message.

You must provide a GSE programmable switch to select if you want to ignore the Line Identifiers for ACARS downlink.
Default Setting: Transmit Line Identifiers.

Each report value is separated by a comma.
Each data line must end with a "/".
Each report is terminated with the character ":".
(2) Format of AIDS Reports for ACARS Downlink

All reports transmitted to ACARS are stripped of information which is not necessary for ACARS. Thus only the data lines that are shown by Line Identifier are transmitted.

The checksums must not be shown in the ACARS downlink messages.

The Line Identifiers in ACARS downlink must be available for transmission.

Each report value is separated by a comma.
Each data line must end with a "/".
Each report is terminated with the character ":".
(3) Report Content Reducing to Data Lines
All reports transmitted to ACARS are stripped off from information which is not necessary for ACARS.
(4) ACARS Downlink Functions

The DMU must do ACARS downlink functions related to the communication protocol described below:
  • the system that transmits the data is called "the source"
  • the system that receives the data is called "the sink".
(5) DMU/MU message Structure for report downlink data

(a) Control/Accountability Header for report downlink data

The first five characters in each block transmitted to or from the Management Unit (MU) constitute the control/accountability header.

(b) Downlink Message Sequence Code for report downlink data

In the transmissions from the AIDS DMU to the MU, the first four characters that came after the control/accountability header constitute the downlink message sequence code as follows:
1 The first character of the downlink message sequence code is D for AIDS DMU
2 The three other characters show a number in range 000 through 999 which is incremented for each new block transmitted to the MU. This number must not reset to 000 in case of power interrupt or a new flight leg.

(c) Optional Ground Header for report downlink data

The DMU must set bit 17 or the data follow word (STX) to '0' to indicate the MU to insert the Optional Ground Header after the Downlink Message Sequence Code. The DMU will not supply an Optional Ground Header.

(d) Message Descriptor for report downlink data

The message descriptor for report downlink data is put in front of the report data in each message block.
The message descriptor for report downlink data has:
  • a Fragmentation Header for report downlink data and a Message Header for report downlink data (first message block) or
  • only a Fragmentation Header (the second block and the message blocks that follow).

1 Fragmentation Header for report downlink data

Each message block has a fragmentation header. The fragmentation header has some elements that are separated by a field delimiter. The fragmentation header always ends with an 'End of line delimiter'.
The total length of the fragmentation header is a fixed length of 25 characters.

The fragmentation header consists of the following elements:

a A/C-Type

  • Description : Type of the aircraft with send the ACMS report
  • Length : 4 characters
  • Permitted characters : ['A'...'Z'] ['0'...'9']
  • Possible values : A318, A319, A320, A321
b Message identifier

  • Description : Message identifier is a number from 000001 to 999999. This message identifier starts at 1 and is incremented for each new complete message transmitted.
  • Length : 6 character
  • Permitted characters : ['0'...'9']
  • Possible values : 000000 up to 999999
  • Remarks: The message identifier must not reset after a power cycle. A new software load resets the counter. After it reaches 999999 the next value is 000001. There must be one counter for all reports.
c Fragmentation downlink part counter

  • Description : Number of the actual message block of the current data that was transmitted (Number of current report downlink part)
  • Length : 1 character
  • Permitted characters : ['0'...'9']
  • Possible values : '1' up to '9'
d Fragmentation total number of downlink block

  • Description : Total number of message blocks of the currently data that is transmitted (Total number of report downlink parts)
  • Length : 1 character
  • Permitted characters : ['0'...'9']
  • Possible values : '1' up to '9'
e Identifier of the Tie back code

  • Description : Identifier of the Tie back code
  • Length : 2 characters
  • Permitted characters : Fixed string
  • Possible values : "TB"
f Tie back code

  • Description :
    In case of an automatically downlinked message, this field is set to "000000"
    In case an ACARS uplink to the A/C, is used to request an ACARS downlink (e.g. triggering an ACMS report), the same tie back code as in the uplink message is used in the downlink message (future extension)
    In case the uplink message contains no tie back code, this field is set to "000000" in the downlink.
  • Length : 6 characters
  • Permitted characters : ['A' ... 'Z'] ['0'...'9']
  • Possible values : ['A' ... 'Z'] ['0'...'9']
  • Remarks: For SA the tie back code is always "000000".
g Field delimiter

  • Description : The Field delimiter separates two fields.
  • Length : 1 character
  • Permitted characters : Fixed character
  • Possible values : Comma (',').
h End of line delimiter

  • Description : The End of line delimiter is the last character of the fragmentation header
  • Length : 1 character
  • Permitted characters : Fixed character
  • Possible values : Solidus ('/').
2 Message Header for report downlink data

The first message block always has the Message-Report Header, all other message blocks of the report have no Message-Report header. The elements of the Message-Report Header are separated by a field delimiter, but there is no field delimiter between message type and report number.
The Message Report Header for report downlink data always ends with an "End of line delimiter" and has a fixed length of 15 characters.

The Message report header has the following elements:

a Message-Type (IMI)

  • Description : Identification of data type (IMI) here: Report
  • Length : 3 character
  • Permitted characters : ['A'..'Z'] ['0'..'9']
  • Possible values : 'REP'
  • Remarks: Fixed for ACMS-reports.
b Report Number

  • Description : Number of the ACMS Report
  • Length : 3 character
  • Permitted characters : ['0'..'9']
  • Possible values : '001' up to '999'.
c Report Layout identifier

  • Description : The Report Layout identifier is used to identify the different layouts/formats of a report (if exists), if not, is always "01"
  • Length : 2 character
  • Permitted characters : ['0'..'9']
  • Possible values : '01' up to '99'
  • Remarks: The name of the parameter must be RxxxRLID (xxx = Report-No with leading zeros). In case the value is not defined or the parameter does not exist, the default value must be "00".
    It must not be possible for the customer to change this value through the Ground Programming Tool (GPT), but it must be possible to show the value in the GPT.
    For customer reports the value "00" must be valid. If the customer created the related Parameter "RxxxRLID" in the GPT, the value of this parameter must be valid for the Report Layout identifier.
d Report layout issue

  • Description : Report layout issue is always incremented if the report layout changes in case of a new software version
  • Length : 2 character
  • Permitted characters : ['0'..'9']
  • Possible values : '01' up to '99'
  • Remarks: The name of the parameter must be "RxxxRLIS" (xxx = Report-No with leading zeros). In case the value is not defined or the parameter does not exist, the default value must be "00".
    It must not be possible for the customer to change this value through the Ground Programming Tool (GPT), but it must be possible to show the value in the GPT. For customer reports the value "00" must be valid. If the customer created the related Parameter "RxxxRLIS" in the GPT, the value of this parameter must be valid for the Report Layout issue.
e Unit Switching Indicator

  • Description : Shows which units (imperial or metric) are used in reports
  • Length : 1 character
  • Permitted characters : ['0'..'9']
  • Possible values :
    '0' - values are displayed as received from source system
    '1' - kg and deg C
    '2' - lbs and deg C
    '3' - kg and deg F
    '4' - lbs and deg F

  • Remarks: The FDIMU must calculate this value by the information which is used for unit switching (refer to Special Rules for Kg and Deg C).
f Special Rules for Kg and Deg C

The DMU must observe bit 18 and bit 27 of DMC label 305.

If bit 18=1, then the parameter values will appear in printouts and alpha call ups in the following units:

  • Fuel flow (Engine 1 and 2) : lbs/hours and not Kg/hours
    (7C.1.244.01, 7C.1.244.10)

  • Fuel Flow Feedback (Engine 1 and 2) : lbs/hours and not Kg/hours
    (7C.1.347.01, 7C.2.347.10)

  • Gross weight : lbs and not Kg
    (02.1.075.00, 02.2.075.00)

  • Pack flow : lbs/sec and not Kg/sec
    (8E.1.126.11, 8E.2.126.00)

  • Bleed air flow : lbs/sec and not Kg/sec
    (7A.1.123.01)

  • Fuel quantity : lbs and not kg
    (5A.2.256.10, 5A.2.257.10)
    (5A.2.260.10, 5A.2.261.10)
    (5A.2.262.10, 5A.2.247.10)

    If bit 27=1, then the parameter values will appear in printouts and alpha call ups in the following units:

  • comfort temperatures ckpt, cab temp : deg F and not deg C
    (29.1.242.01, 29.2.242.01)
    (29.1.244.01, 29.2.244.01)
    (29.1.245.01, 29.2.245.01)

    If label 305 from the DMC becomes invalid during flight or it is invalid at power-on, the switchable parameters will be set by default to Kg and deg C.
** ON A/C NOT FOR ALL
7. Operation/Control and Indicating
A. Energization
During normal operation the AIDS is automatically in normal mode at the power-on condition.
The FDIMU is supplied directly from busbar 202XP (115VAC). The DAR (optional) is supplied from the busbar 204PP (28VDC) and the busbar 202XP (115VAC).
B. Control and Indication through MCDU
The communication with the aircraft systems is done through a Multipurpose Control Display Unit (MCDU) related to ARINC-739. The control of the FDIMU is done by an interactive and menu controlled user interface.
C. Remote Print Button
(1) Remote Print Button Function
A remote print button function causes generation of specified print reports as a function of flight phase. The 'trigger' is reprogrammable through the GSE.
The definition about which print report in which flight phase has to be generated, is defined in the respective report trigger logic.
(2) Remote Print Button Installation
The print button is installed on the pedestal assy on panel 112VU in the cockpit.
D. MCDU Functions and Rules

F MCDU and MCDU Menu ** ON A/C NOT FOR ALL
Some of the AIDS functions are controlled by the MCDU.
The MCDU display has 14 lines, each line has 24 characters. Line 1 is used as a title line or to show data to which the operator does not have access. Line 14 is used as a scratchpad line for entering data into the system.
Lines 2 through 13 are data lines arranged into six pairs (lines 2-3, 4-5, 6-7, 8-9, 10-11, 12-13). Each pair of lines has a label line and a data line. The data lines are adjacent to the Line Select Keys (LSK), and the label line is above the data line.
The line pairs are referenced by LSKs as shown below and in the menu figures:
LSK CRT Lines
1L and 1R 2 and 3
2L and 2R 4 and 5
3L and 3R 6 and 7
4L and 4R 8 and 9
5L and 5R 10 and 11
6L and 6R 12 and 13


The LSKs allow entry of data into a field and access to a data or a function identified by that field.

(1) MCDU Keys
The keyboard has the following alphanumeric keys:
Activating an alphanumeric key (0 through 9, A through Z, ., +, -, ° and / ) enters that character into the scratchpad of the MCDU.

If you push the MCDU MENU the display shows the MCDU menu. The other mode keys are not used for AIDS.
Function keys
'NEXT PAGE' = shows the next page or to a option
'ARROW up' = scrolls the displayed page up
'ARROW down' = scrolls the displayed page down
'CLR' = clears the scratchpad and data
fields.
' ° OVFY' = enters a ° into the scratchpad (not used
for AIDS).
There are three annunciators on the MCDU front panel:
'MCDU MENU' : This annunciator illuminates white when a system
linked to the MCDU requests the display.
'FAIL' : Not used for AIDS
'FMGC' : Not used for AIDS

(2) General Display Rules
No-valid and Missing Data
For all display fields, only valid data will be shown. If a new update of a parameter was not received since the last sampling, then the parameter is marked as "Not Transmitted" ("XXX"). If a parameter is received with SSM indicating "not Normal Operation", then the parameter is marked with dashes ("---").
If the length of the parameter is too large (overflow) the display field shows Es. The possible length of parameters is between one and six characters (for example: "E", "EE", ...).
When a new page is accessed, or data are entered, it can require the computer to do calculations before all the data to be shown are available. In these cases, the screen is cleared. Then the portion of the display that is available and can be shown is presented to the operator immediately. However, the data fields that are not available can be left as dashes and filled in as the data become available.

Small and Large Front Panels
The MCDU has two sizes of front panel. Generally all data on the data line are shown on a large front panel. But data on the label line are shown on a small front panel.
However, the following are exceptions:
  • Data with default values (or computer calculated values)
    which can be changed by the operator are shown on a
    small front panel.
  • If two data entries are dependent upon each other, the
    independent data (those defaulted to or latest input by
    the operator) are shown on a large front panel and
    the dependent data are on a small front panel.
  • For additional exceptions for AIDS which ensure more
    clarification in some menus.

(3) MCDU Special Symbols
There are special symbols on MCDU displays that indicate certain functions to the operator. Certain symbols show the operator what is available or if there is more information than is already shown.
The following symbols are used in the displays:
< or > If this symbol shows next to an LS key, it indicates
that the activating line select key will only cause
the MCDU to display a different page (it is the
call-up of a page). Its name is shown beside the symbol.
* If this symbol shows beside an LS key, it indicates that
the key causes the activation of a function (it is
the call-up of a function). The page shown can also
change as a result. If the DMU or FDIMU needs some time to react,
during this time the star can disappear to show
that the signal was registered. As long as the star is
not shown, the related function can not be activated.
If an arrow shows beside an LSK, it shows
that the operator can press the key to set
data, without activating a function.
(,) This indicates that the user can enter data here
(optional). Occasionally this data can be computed
and entered by the computer as a result of another
operator action.
() This indicates that the data are necessary for the user
to input in order for the computer does the specific
function.
----- This indicates that the data will be shown by the
computer when it has enough information to do so. The
user does not normally enter this information.
However, under certain circumstances he can be able
to alter the data.
Two vertical arrows (up or down) in columns 23 and 24
of the scratchpad show that vertical slewing is available.
A horizontal arrow in column 24 of the title line show that
horizontal slewing is available from this page.
Activating the NEXT PAGE key will slew the page
horizontally.

(4) MCDU Color Coding
The color code is as follows:
+--------------------------------------------------------------+
! DATA ! MCDU COLOUR !
!-----------------------------------------+--------------------!
! Titles, comments, symbols of slewing ! White !
! dashes, minor messages, call-up of ! !
! page, scratchpad data entry ! !
!-----------------------------------------!--------------------!
! Operator modifiable data, selectable ! Cyan !
! data, brackets call-up of function ! !
!-----------------------------------------!--------------------!
! Operator non modifiable data-active ! Green !
! data ! !
!-----------------------------------------!--------------------!
! - Mandatory data (boxes) mandatory ! !
! operator action required ! Amber !
! - Important messages ! !
!-----------------------------------------!--------------------!
! Constraints max altitude ! Magenta !
!-----------------------------------------!--------------------!
! Temporary situation ! Yellow !
!--------------------------------------------------------------!

(5) MCDU Vertical Slewing
Certain pages in the computer contain more data than will fit on a single page (a page longer than the six pairs of lines available on the display).
In these cases, data are arranged on a 'drum'. In these instances vertical slewing can be used to scroll the display up or down. Each press of a vertical slew key scrolls the MCDU display by one line pair, or by one block. A line pair is a line adjacent to an LS key and its label line. Holding the vertical slew key down scrolls the MCDU display at a rate of 2 line pairs per second. The arrows will be shown in columns 23 and 24 of the scratchpad when vertical slewing is available.

(6) General Display of a Page
  • Only the selectable functions or page call-ups are shown.
  • On a page, some prompts are shows following logic dependent on external parameters. In such cases the prompt is added or deleted.
  • Prompts that are used on some pages must be shown at the same place on the different pages.
    e.g.: RETURN at 6L
    PRINT at 6R

(7) Acknowledgement of User Action
Each time the MCDU user activates an LS key or a mode key, he receives an acknowledgement of his action.
The new page also shows an acknowledgement of the operator (insertion of a value in a line, message, etc ...).
Examples:
  • if the user wants to enter a value into a field, he will have the following messages:
    'OUT OF RANGE' if the value is not within the range as expected by the system.
    'FORMAT ERROR' if the value does not have the correct format.
  • the message 'NOT ALLOWED' is shown if an incorrect LS key is activated.
In case of the call-up of a function, the acknowledgement is made by deletion of the star '*'. This is next to the function name when the call-up is taken into account by the system.
If the system is not available a message is shown (e.g 'Printer Busy').

(8) MCDU Data Entry
Data are entered into the computer through the keyboard.
First the data are entered from left to right into the scratchpad by activating the alphanumeric keys on the keyboard (similar to that of a type-writer). Only 22 characters can be entered into the scratchpad. If more than 22 are entered, they will be ignored. The 23rd key press will not be accepted by the computer and the computer will give no response.
After entry of the data into the scratchpad, the date are moved from the scratchpad into the correct data field. By activating the adjacent LS key, the scratchpad is cleared.

The computer checks the data for format and acceptability (out of range, entry not allowed into the field, etc ...).
If the data are incorrect, the system will leave the previous data in the data field and then shows the associated message indicating the error in the scratchpad. To enter the correct data, the operator must do either of the following:
  • Clear the message from the scratchpad by activating the CLR key. The data that was incorrect will show in the scratchpad. The operator can then correct the data or clear it out.
  • Enter new data into the scratchpad. This automatically clears the message being shown and replaces the previous (incorrect) scratchpad data with the new data.
If the entry was rejected because an incorrect LS key was activated, the entry will be accepted if the correct LS key is activated.
To clear the scratchpad of entered or incorrect data, the CLR key can be used. One press of the CLR key erases the last character entered in the scratchpad. A second press of the CLR key erases the second last character. At the third press of the CLR key, all data in the scratchpad are deleted. The same process applies if the CLR key is held pressed.
Immediately the last character is cleared, one second later, the second character is cleared, after 2 seconds the entire scratchpad will be cleared of any data.
Certain data entries into a field also cause the shown page to be changed automatically. In these cases, any scratchpad data are deleted. If not, scratchpad data is retained when the shown page is changed. During a page change, scratchpad entries are ignored.

(9) Clearing Data Fields
Data fields on the MCDU can be cleared using the CLR key.
Activating the CLR key when the scratchpad is empty results in CLR being shown. This shows the columns 6 to 8 of the scratchpad. Then, activating the LS key adjacent to the data field results in clearing that data and the scratchpad line is cleared.
If the data have a default or computer calculated value, the data revert to this value. If the default value is cleared, the clearing has no effect and there is no message shown.
To remove a CLR prompt from the scratchpad, the CLR key can be activated again once. Or any alphanumeric key can be activated erasing the CLR in the scratchpad and entering the alphanumeric. The computer must distinguish between the CLR key and C-L-R being entered into the scratchpad through alphanumeric keys. C-L-R does not enable the clearing function.

(10) MCDU Data Field Display
Generally, a data is shown on two lines:
  • the label line above the data line,
  • the data line next to the LSK.
On the data line there are five kinds of display:
  • Cyan data if the data is already in the computer and the operator can modify it.
  • Green data if the data is already in the computer but it cannot be modified by an operator entry.
  • Cyan brackets (- -) if no value is defined and the operator can enter the data.
  • Amber boxes ( ) if no value is defined. Then the data entry is mandatory for the correct functioning of the system. Or for the achievement of the function described on the page or on the label line.
  • White dashes ( --- ) if the field is filled by the computer but not yet available. Due to lack of information or a computation has not yet been or a computation has no yet been achieved.
The entry format of data is described by the number of boxes or the place occupied by the brackets, or the spaces between brackets. On one data line, some data can be shown and entered : the different fields are separated by a slash ('/').
Each field can be entered separately. It is identified by the number of slashes in front of the entered data:
e.g.: EQ/SYS/LAB/SDI
to modify the label, the operator has to enter into the scratchpad : '//label'.

(11) Clearing Messages
Any message that is shown can be cleared by activating the CLR key. Messages are automatically cleared under the following conditions:
  • When data are entered into the scratchpad
  • When LS or MODE key is activated
  • When the reason is no longer valid.

(12) Use of more than one MCDU at the same Time
The FDIMU communicates with one MCDU only at the same time. If MCDU communication is requested from any of these MCDU's while communication is already active on another MCDU, the FDIMU responds with the message: "AIDS (TIMEOUT)".
F Some MCDU's ** ON A/C NOT FOR ALL
E. MCDU Operation
The MCDU is controlled by line select keys, mode keys and function keys.

(1) Entering the AIDS Mode
F AIDS Main Menu ** ON A/C NOT FOR ALL
F AIDS Main Menu ** ON A/C NOT FOR ALL
To get access to the AIDS functions, push the 'MCDU MENU' mode key. The MCDU shows the 'MCDU MENU' page.
If the operator pushes the line select key adjacent to 'AIDS', he get access to the AIDS Main Menu.

(2) MCDU Return Function
F MCDU Return Function (Example) ** ON A/C NOT FOR ALL
F MCDU Return Function (Example) ** ON A/C NOT FOR ALL
If you push the line select key adjacent to 'RETURN', the MCDU display shows the next higher or previous MCDU page.

(3) MCDU Display Print
F MCDU Display Print (Example) ** ON A/C NOT FOR ALL
F MCDU Display Print (Example) ** ON A/C NOT FOR ALL
If you push the line select key adjacent to PRINT*, the display content of the MCDU is sent to the cockpit printer. A print out is transmitted with a header to the printer. The header contains the A/C identification, the print date, UTC, city pair and the flight number.
F. MCDU Controlled DMU Function
The AIDS main menu gives access to these functions:
* Parameter Call-up:
- Parameter Label Call-Up
- Parameter Alpha Call-Up
- Alpha Call-Up Help
- Parameter Menus
- Z.B. FLIMOD
* DMU Software Load
- Load Status
* Report Functions
- List of Previous Reports
- List of Stored Reports
- Manual Report Request
* SAR/DAR Functionality
- SAR Summary
- List of SAR stored Records
- SAR Manual Request
- DAR PCM
* Print Button
- Assignment of Remote Print
* Reprogramming
- Programming
* DMU Programming
- Report Inhibit
- Report Limits
- Report Counters
- Statistic Counters
- Ethernet Parameter Init
* PCMCIA
- Disk Ident
- Disk Directory
- DAR Record
- WEFA
* User Screen (user programmable functions on user SW partition).
These functions are selectable by the DMU Main Menu, which is issued by the
DMU after 'AIDS' was selected by the operator on the MCDU.

The AIDS main menu gives access to these functions:
* Parameter Callup:
- Parameter Label Call-Up
- Parameter Alpha Call-Up
- Parameter Menus
* Load Status Display
* List of Previous Reports
* List of Stored Reports
* Manual Report Request
* Assignment of Remote Print
* SAR/DAR Functionality
- SAR Summary
- List of SAR stored Records
- SAR Manual Request
- DAR PCM
- DAR Run Control Switch
* DMU Programming
- Report Inhibition
- Report Limits
- Report Internal Counters
- Statistic Counters
* User Screen (user programmable functions on user SW partition)
These funstion are selectable by the DMU main menu, which is issued by the DMU
after 'AIDS' has been selected by the operator on the MCDU.

G. AIDS DMU Programming
(1) Print Out Stored Reports are Sent to ACARS by Manual Request
F Print Out and Send Stored Reports to ACARS by Manual Request ** ON A/C NOT FOR ALL
AIDS reports which are stored in the print report buffer (maximal 10 reports), can be printed and/or transmitted to ACARS by manual request through the MCDU.
The procedure is as follows:
  • select 'AIDS' on MCDU Menu,
  • select 'STORED REPORTS>' on the AIDS Main Menu,
  • the AIDS STORED REPRTS page comes into view.
The displayed output status will indicate the status related to the 'Immediate Output Rule'.
Some remarks can be displayed described for output status as follows:
  • 'EOF' is displayed if the 'Immediate Output Rule' is 'Storage Only' and the 'End-Of' Flight (EOF) Output Rule' is different than 'Storage Only'.
  • 'WPR' is displayed if the printer is not available or not ready.
  • 'PRT' is displayed if the report is completely transferred to the printer related to the 'Immediate Output Rule' OR 'End-Of-Flight Output Rule'.
  • 'WDL' is displayed if the 'ACARS MU' is not available or not ready to receive data.
  • 'DLK' means that the report was successfully downlinked by ACARS.
  • 'ACS' means that the report was sent completely from 'AIDS' to the 'ACARS MU' related to 'Immediate Output Rule' OR 'End-Of-Flight Output Rule', but reception from the ground station was not yet confirmed.
  • 'WDR' is displayed if the DAR/WGL-DAR is not available or not ready to receive data.
  • 'DAR' is displayed if the report is completely transferred to the DAR/WGL-DAR through RS-422 interface refer to the 'End-Of-Flight Output Rule'.
  • 'PRINT DUMP SEND' indication causes immediate printout, transmission to the 'ACARS' or dump on the MDDU diskette of the selected report. The selected output depends on the selection of the LS key function on the left side of the screen.
    After a manual request of a PRINT, SEND or DUMP of a stored report, the asterix will disappear for one second.
    The name of the report selected for output will change temporarily to green until the report output is finished.
(2) Print Out Stored Reports are Sent to ACARS by Manual Request
F Print Out and Send Stored Reports to ACARS by Manual Request ** ON A/C NOT FOR ALL
F Print Out and Send Stored Reports to ACARS by Manual Request ** ON A/C NOT FOR ALL
AIDS reports which are stored in the print report buffer (maximal 10 reports), may be printed and/or transmitted to ACARS by manual request via the MCDU.
The procedure is as follows:
  • select 'AIDS' on MCDU Menu,
  • select 'STORED REPORTS>' on the AIDS Main Menu,
  • the AIDS STORED REPORT Page comes on,
  • select the key adjacent to a wanted report,
  • the AIDS STORED REPRT page comes into view.

Some remarks can be displayed described as follows:
  • 'DNLKD' means that the report was successfully downlinked by ACARS.
  • 'INACS' means that the report was sent automatically from 'AIDS' to the 'ACARS MU' but reception from the ground station was not yet confirmed.
    Start the print out of the desired report by activating the appropriate LS key on the right side of the screen (below 'PRINT').
    Initiate sending a report to ACARS by activating the appropriate LS key on the left of the screen (below 'SEND'). The asterix then disappear from the screen as long as the printer or ACARS are occupied.
(3) Print Out Stored Reports are Sent to ACARS by Manual Request
F Print Out and Send Stored Reports to ACARS by Manual Request ** ON A/C NOT FOR ALL
AIDS reports which are stored in the print report buffer (maximal 10 reports), may be printed and/or transmitted to ACARS by manual request via the MCDU.
The procedure is as follows:
  • select 'AIDS' on MCDU Menu,
  • select 'STORED REPORTS>' on the AIDS Main Menu,
  • the AIDS STORED REPRTS page comes into view.
The displayed output status will indicate the status according the 'Immediate Output Rule'.
Some remarks can be displayed described for output status as follows:
  • 'EOF' is displayed if the 'Immediate Output Rule' is 'Storage Only' and the 'End-Of' Flight (EOF) Output Rule' is different than 'Storage Only'.
  • 'WPR' is displayed if the printer is not available or not ready.
  • 'PRT' is displayed if the report is completely transferred to the printer according to the 'Immediate Output Rule' OR 'End-Of-Flight Output Rule'.
  • 'WDL' is displayed if the 'ACARS MU' is not available or not ready to receive data.
  • 'DLK' means that the report was successfully downlinked by ACARS.
  • 'ACS' means that the report was sent completely from 'AIDS' to the 'ACARS MU' according to 'Immediate Output Rule' OR 'End-Of-Flight Output Rule', but reception from the ground station was not yet confirmed.
  • 'WDR' is displayed if the DAR/WGL-DAR is not available or not ready to receive data.
  • 'DAR' is displayed if the report is completely transferred to the DAR/WGL-DAR via RS-422 interface according to the 'End-Of-Flight Output Rule'.
  • 'PRINT DUMP SEND' indication causes immediate printout, transmission to the 'ACARS' or dump on the PDL diskette or mass memory, if available, of the selected report. The selected output depends on the selection of the LS key function on the left side of the screen.
    After a manual request of a PRINT, SEND or DUMP of a stored report, the asterix will disappear for one second.
    The name of the report selected for output will change temporarily to green until the report output is finished.
H. Print Button
(1) Remote Print Button Function
A remote print button function causes generation of specified print reports as a function of flight phase. The 'trigger' is reprogrammable through the GSE.
The definition of which print report, in which flight phase, has to be generated, is defined in the respective report trigger logic.
The definition about which print report in which flight phase is generated is defined in the respective report trigger logic.
The remote print button is connected to FDIMU through the rear connector middle plug pin 13G.
The passive state of the remote print button is a connection to ground. Each push of the remote print button causes opening the button contacts. A single report is triggered, when the remote print button is pushed for longer than 200 msec. Before a further report can be triggered with the remote print button, the button must be released for minimum 1 second (Ground Connection).
I. AIDS MCDU Functions
The AIDS main menu gives access to the functions as follows:
  • Parameter Label Call-Up Menu
  • Parameter Alpha Call-Up Menu
  • Special Functions / Reprogramming Submenus
  • Manual DAR Recording Control (if installed)
  • List of Stored SAR Data
  • Manual Request of SAR Recording
  • Systems Data Menus
  • PCMCIA
  • Airline Functions (option)
  • List of Stored Reports
  • Manual Request of Reports
  • Help Menus.
(1) Parameter Call-Up Menus
The Parameter call-up menus allow direct access to all parameters transmitted on the ARINC 429 DITS buses connected to the FDIMU for online display.
Additional the user can define, store, record and delete Parameter Call-up contents.
For this purpose there are two menus:
  • The Parameter Label Call-Up Menu
  • The Parameter Alpha Call-Up Menu.

(a) Parameter Label Call-Up Menu
F AIDS - Parameter Call-Up (Label) ** ON A/C NOT FOR ALL
After entry of Equipment Code (EQ), System Number (SYS), Label Number (LAB), Source/Destination Identifier (SDI) and Databits (if necessary) the parameter with their values shows online on the display. Furthermore a port list shows the connected ARINC 429 inputs with information about Port Number, System, EQID and SYSID. The system provides also a menu to display Parameter Labels from the DFDRS.

1 Display of Label Call-Up Parameter
Access:
  • Set AIDS on the MCDU MENU menu
  • Set LABEL on the AIDS main menu
  • Set DISPLAY on the AIDS Label Call-Up Control menu.
Entry:
Enter with the alphanumeric keys EQ, SYS, LAB, SDI and DATABITS (if necessary) isolated with a slash (e.g. 116/1/344/01/12) into the scratch pad and push the line select key 1L or 4L to take over into the data field.
8 Label Call-Up menu pages are provided and each menu page can display two Label Parameter.
Valid Label Parameter entries:
-----------------------------------------------------------------------------
! Entry: ! Digits ! Description ! Valid entry !
!----------!--------!---------------------------!---------------------------!
! EQ ! 3 ! Equipment Identifier ! see Parameter or Port list!
!----------!--------!---------------------------!---------------------------!
! SYS ! 1 ! System Number ! 1, 2, 3 or 4 !
!----------!--------!---------------------------!---------------------------!
! LAB ! 3 ! Label Number ! see Parameter list !
!----------!--------!---------------------------!---------------------------!
! SDI ! 2 ! Source/Destination Ident. ! 00, 01, 10 or 11 !
!----------!--------!---------------------------!---------------------------!
! DATABITS ! 2 ! LSB used for calculation ! see Parameter list (opt. !
! ! ! of the decimal value ! data), default = 18 !
-----------------------------------------------------------------------------

Display / Result:
The line below the parameter contains the label and SDI from the parameter, which the FDIMU has found on the bus. In addition the decimal presentation of the DATABITS value starting with bit 28 is displayed. In the next line the the SSM bits and the binary data of the parameter shows.
The values of the selected parameters updates once per second. If the selected parameter not received or updated within one second the parameter is marked with > indication.
2 Label Port List
Access:
  • Set AIDS on the MCDU MENU
  • Set LABEL on the AIDS main menu
  • Set PORT LIST on the AIDS Label Call-Up Control menu.
Display:
The Label Port list shows the connected FDIMU ARINC 429 inputs with Port Number, connected System, Equipment Number and System Number.
3 Define, Select, Store, Delete and Clear of Label Call-Up Contents
Access:
  • Set AIDS on the MCDU MENU
  • Set LABEL on the AIDS main menu.
Entry:
  • Define/Select of Setup Name:
    Enter with the alphanumeric keys 5 character into the scratchpad and push the line select key (2L) below SETUP NAME indication. Does the entered Setup Name exist in the stored Label Menu Setups the content of this is now active. If not, a new Setup Name is defined.
  • Store:
    Push the line key adjacent to STORE indication to save the Setup Name with the contents.
  • Delete:
    Push the line key adjacent to DELETE indication to erase the Setup Name with the contents.
  • Clear:
    Push the line key adjacent to CLEAR indication to clear all parameters in current (selected/active) Label Call-Up Setup.
Display:
The current Setup Name shows below the SETUP NAME indication if one is selected or defined. The stored Label Menu Setups shows below the STORED LABEL MENU SETUPS indication.
4 Print Record of an Online Parameter Trace
This function allows to record the parameter from the current Label Call-Up Menu Setup on the printer. The printout starts immediately after selection.
Access:
  • Set AIDS on the MCDU MENU
  • Set LABEL on the AIDS main menu.
Entry:
Enter with the alphanumeric keys the number of seconds (3 digits) into the scratchpad and push the line key adjacent to START indication.
Result:
For the entered time the printer prints the values of the current Label Call-Up Menu with a rate of 1 Hz.
5 Display of DFDRS Labels
For verification of correct FDIMU ARINC 717 input/output the DFDRS Label Call-Up menu is provided.
Access:
  • Set AIDS on the MCDU MENU
  • Set LABEL on the AIDS main menu
  • Set DFDR/LABEL on the AIDS Label Call-Up Control menu.
Entry:
Enter with the alphanumeric keys DFDRS Word (3 digits) into the scratchpad and push the line key adjacent to the WORD indication.
Display/Result:
The SYNC WORDS SF#1, SF#2, SF#3 and SF#4 for DFDR and Playback shows on the display.
6 Possible Scratchpad Messages
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ENTER PARAMETER NUMBER ! - Default message at menu call-up !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Up, Down, Left, Right Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Equipment Identification (EQ) is not a valid !
! ! 3 character hex number or !
! ! - System Number (SYS) not within 1, 2, 3 or 4 or!
! ! - Label (LAB) is not a valid 3 character octal !
! ! number within 000 to 377 or !
! ! - SDI code is not within 00, 01, 10, 11, XX or !
! ! - Number of Databits is not a valid 2 digit !
! ! decimal number within 0 to 20 or !
! ! - At least one of the mandatory parameter number !
! ! parts EQ, SYS, LAB, SDI is missing and has not !
! ! been entered previously or !
! ! - Invalid delimeter character (/) or !
! ! - Any further undefined characters !
!------------------------!--------------------------------------------------!
! UNKNOWN EQ/SYS IDENT ! - ARINC 429 Equipment Identification (EQ) !
! ! in the ACMS Setup Database or !
! ! - Entered System Number (SYS) is not defined in !
! ! the Setup Database for related Equipment !
! ! Identification (EQ) !
!---------------------------------------------------------------------------!

(b) Parameter Alpha Call-Up Menu
F AIDS - Parameter Call-Up (Alpha) ** ON A/C NOT FOR ALL
After entry of an Alpha Code the alpha code, source and values shows online on the display. Furthermore an Alpha list shows the available Alpha Codes. In the Parameter list the available Alpha Codes are described.
1 Display of Alpha Call-Up Parameter
Access:
  • Set AIDS on the MCDU MENU
  • Set ALPHA on the AIDS main menu
  • Set DISPLAY on the AIDS Alpha Call-Up Control menu.
Entry:
Enter with the alphanumeric keys the Alpha Code (e.g. UTC) into the scratchpad and push the line select key 1L, 2L, 3L, 4L or 5L to take over into the data field. The line select key 5L can show only alpha codes with not more than two values.
8 Label Call-Up menu pages are provided and each menu page can display 5 Alpha Codes Parameter.
Display / Result:
The display of alpha call-up parameter contains the content as follows:
  • ALPHA : The entered Alpha Code
  • SOURCE : Name of source bus/system from the selected alpha call-up
  • POS : Position Number of the associated alpha call-up value. If a : is displayed after the position number that shows the selected parameter is valid. If the field for the value is filled with XXX the selected parameter is not updated within 1 second. If the field for the value filled with --- the selected parameter is received with invalid SSM.
The values of the selected parameters updates once per second. If parameters from two or four systems are available, both respective four parameters shows by one call-up code entry.
2 AIDS Alpha List
Access:
  • Set AIDS on the MCDU MENU
  • Set ALPHA on the AIDS main menu
  • Set LIST on the AIDS Alpha Call-Up Control menu.
Display:
The Alpha List shows all available Alpha Codes.
To find a certain Alpha Code the menu has a filter function by entry of the first character.
3 Define, Select, Store, Delete and Clear of Alpha Call-Up Contents
Access:
  • Set AIDS on the MCDU MENU
  • Set ALPHA on the AIDS main menu.
Entry:
  • Define/Select of Setup Name:
    Enter with the alphanumeric keys 5 character into the scratchpad and push the line select key (2L) below SETUP NAME indication. Does the entered Setup Name exist in the stored Alpha Menu Setups the content of this is now active. If not, a new Setup Name is defined.
  • Store:
    Push the line key adjacent to STORE indication to save the Setup Name with the contents.
  • Delete:
    Push the line key adjacent to DELETE indication to erase the Setup Name with the contents.
  • Clear:
    Push the line key adjacent to CLEAR indication to clear all parameters in current (selected/active) Alpha Call-Up Setup.
Display:
The current Setup Name shows below the SETUP NAME indication if one is selected or defined. The stored Alpha Menu Setups shows below the STORED ALPHA MENU SETUPS indication.
4 Print Record of an Online Parameter Trace
This function allows to record the parameter from the current Alpha Call-Up Menu Setup on the printer. The printout starts immediately after selection.
Access:
  • Set AIDS on the MCDU MENU
  • Set ALPHA on the AIDS main menu.
Entry:
Enter with the alphanumeric keys the number of seconds (3 digits) into the scratchpad and push the line key adjacent to START indication.
Result:
For the entered time the printer prints the values of the current Alpha Call-Up Menu with a rate of 1 Hz.
5 Possible Scratchpad Messages
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ENTER ALPHA CALL-UP ! - Default message at menu call-up !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or OVFY -Key or !
! ! - Up, Down, Left, Right Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID ENTRY ! - No valid Alpha Call-Up ASCII code of up to !
! ! 4 characters or !
! ! - Any further undefined characters !
!------------------------!--------------------------------------------------!
! UNKNOWN ALPHA CODE ! - Alpha Call-Up code is not defined within the !
! ! ACMS Setup Database !
!------------------------!--------------------------------------------------!
! TOO MANY ENTRIES ! - 4 - system parameters is selected and there is !
! ! no space for 4 parameters (next line is !
! ! occupied) !
-----------------------------------------------------------------------------

(2) Parameter Call-Up

The parameter call-up functions are a part of the DMU operational software. The
operation of the alpha call-up function depends on the availability of an alpha call-up table and associated EUC table.

(a) Parameter Label Call-Up Menu
F AIDS - Parameter Call-Up (Label) ** ON A/C NOT FOR ALL

Each parameter transmitted on one of the up to 64 ARINC 429 connected data buses are selectable for display on the MCDU screen. The selection are made using EQ, source system, label and SDI. Additionally the number of data bits to be used for decimal representation are selectable. The parts of the parameter number are isolated with a slash '/'.
The number of the data bits can be ignored. The default value is 18. The displayed parameters are updated once per second. Up to 2 parameters are displayed on one page. 8 pages can be selected through slew up/slew down button, which leads to a maximum number of 16 parameters to be monitored simultaneously.
Example : Parameter Call-Up with EQ and System Number
EQ/SYS/LAB/SDI = 1A/2/156/01


1 The procedure to select the Parameter Label Call-Up Menu is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'PARAM LABEL CALL-UP' on the AIDS Param Call-Up Menu.
  • Enter the parameter (e.g. 1C/1/344/01/12) on the scratchpad
  • Set the 1L key

2 Menu Definitions:
+---------------------------------------------------------------------------+
! EQ ! ARINC 429 equipment identification: !
! ! two-digit hexadecimal character e.g. 1B (for SFCC) !
!-----------!---------------------------------------------------------------!
! SYS ! System Number: !
! ! one character (only 1 to 4) !
!-----------!---------------------------------------------------------------!
! LAB ! ARINC 429 Label: !
! ! three-digit octal character (valid entries 000 - 377) !
!-----------!---------------------------------------------------------------!
! SDI ! Source Destination Identifier: !
! ! valid entries 00, 01, 10, 11 and XX (XX represents a case in !
!-----------!---------------------------------------------------------------!
! DATABITS ! Identifies which ARINC 429 bits to extract from the label !
! ! call-up parameter and show as decimal value (valid entries !
! ! 1 to 20) !
!-----------!---------------------------------------------------------------!
! VALIDITY ! Validity of the requested parameter: !
! ! '>' parameter has not been transmitted/updated. !
! ! 'Blank' parameter was updated. !
!-----------!---------------------------------------------------------------!
! SSM ! Sign Status Matrix: !
! ! is taken from bits 31 to 29 of the parameter and shows in !
! ! binary form. !
!-----------!---------------------------------------------------------------!
! DECIMAL ! Decimal value of the parameter calculated using the 'DATABITS'!
! VALUE ! entry to specify the number of bits to use as data. The !
! ! decimal value is calculated assuming the extracted data bits !
! ! as a whole represent a 2's complement value. For example !
! ! 'DATABITS' of 12 results in the decimal display of ARINC 429 !
! ! bits 28 to 17 . A 'DATABITS' entry of 20 results in a decimal !
! ! display of ARINC 429 bits 28 to 09. If bit 29=0, then the !
! ! decimal equivalent of the two complement of the 'DATABIT' !
! ! value will be preceded with a negative sign. !
!-----------!---------------------------------------------------------------!
! BINARY ! Binary Data (bits 28 to 11) of the parameter are shown on the !
! DATA ! on the line below the label 'DATABITS 28-11'. !
+---------------------------------------------------------------------------+

3 Possible Scratchpad Messages:
+----------------------------------------------------------------------------+
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Equipment Identification (EQ) is not a !
! ! valid 2 character hex number !
! ! or - System Number (SYS) not within 1, 2 !
! ! or - Label (LAB) is not a valid 3 character octal!
! ! number within 000 to 377 !
! ! or - SDI code is not within '00', '01', '10', !
! ! '11', 'XX' !
! ! or - Number of databits is not a valid 2 digit !
! ! decimal number within 01 to 20 !
! ! or - At least one of the mandatory parameter !
! ! number parts EQ, SYS, LAB, SDI is missing !
! ! and has not been entered previously !
! ! or - Invalid delimeter character ('/') !
! ! or - Any further undefined characters !
!-------------------------!--------------------------------------------------!
! UNKNOWN EQ/SYS IDENT ! - ARINC-429 Equipment Identification (EQ) is !
! ! not defined in the DMU Setup Database !
! ! or - Entered System Number (SYS) is not defined !
! ! in the Setup Database for related Equipment !
! ! Identification (EQ). !
+----------------------------------------------------------------------------+

(b) Parameter Alpha Call-Up Menu
F AIDS - Parameter Call-Up (Alpha) ** ON A/C NOT FOR ALL

For all the parameters, which are listed in the alpha call-up table. The selection is possible by their alpha codes. If parameters from two systems are available, both parameters are displayed on the MCDU upon a single alpha call-up code entry. The displayed parameter values are refreshed once per second.

All numeric type alpha call-up parameters are displayed on the MCDU in engineering units. The display format is a floating point representation of max. 6 characters including the decimal point and the '-' sign if applicable.

In case of positive numbers without decimal point all 6 characters are available for digits. Display of loading zeros are suppressed. The applicable units are shown below the alpha call-up code on the MCDU screen.

Alpha call-up parameters, which consist of a combination of several discrete bits or packed discretes are displayed in hexadecimal representation. In this case the indication of the applicable units of the parameter are 'HEX'. Codes Parameter.

1 The procedure to select the Parameter Alpha Call-Up Menu is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'PARAM ALPHA CALL-UP' on the AIDS Parameter Call-Up Menu.
  • Enter the Alpha Call-Up Code on the adjacent LSK
  • Set the adjacent line key

  • Set 'CLEAR ALL'
  • All entries are deleted.

2 Display indications:
+---------------------------------------------------------------------------+
! ALPHA ! Alphanumeric name for specific aircraft parameter !
!-----------------!---------------------------------------------------------!
! SOURCE ! Name and system number of the source computer of !
! ! subsystem !
!-----------------!---------------------------------------------------------!
! POSITION ! Position identifier referenced to the aircraft !
!-----------------!---------------------------------------------------------!
! VALIDITY ! Validity of Alpha Call-up parameter: !
! ! - ':' (white) parameter was updated and contains !
! ! valid SSM !
! ! - '>' (green) parameter was not updated !
! ! - '<' (green) parameter contains invalid SSM !
!-----------------!---------------------------------------------------------!
! VALUE ! Value of parameter in engineering units. !
!-----------------!---------------------------------------------------------!
! UNITS ! Units associated with parameter !
+---------------------------------------------------------------------------+


3 Possible Scratchpad Messages:
+----------------------------------------------------------------------------+
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! UNKNOWN ALPHA CODE ! - No valid Alpha Call-Up ASCII code up to !
! ! 5 characters. !
! ! or - Any further undefined characters !
! ! - Alpha Call-Up code is not defined within !
! ! the DMU Database Software !
+----------------------------------------------------------------------------+

(c) AIDS Parameter Menu
F AIDS - Parameter Menu ** ON A/C NOT FOR ALL
The Parameter Menus are programmable through the GSE.

1 The procedure to select the Parameter Menus is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'MENUS' on the AIDS Parameter Call-Up Menu.
    The display shows this sub menu:
    <FLIMOD
    <REPORT1
    <DIVERGENCE
    <RETURN
  • PRINT*
2 Possible Scratchpad Messages:
+----------------------------------------------------------------------------+
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
+----------------------------------------------------------------------------+

(3) AIDS Special Functions / Reprogramming Menus
The Special Functions / Reprogramming menu contains:
  • Password Entry
  • Call-Up of Statistic Counter Submenu
  • Call-Up of Documentary Data
  • Call-Up of Report Inhibit Submenu
  • Call-Up of Report Reset Submenu
  • Call-Up of Report Constants Programming Submenu
  • Call-Up of Dump Status
  • Call-Up of Reprogrammable Reports Submenu.
(a) Password Entry
The access to any AIDS functions are protected through a password.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu.
Entry:
Enter the 8 character Security Access User identification into the scratchpad. For each character a star (*) shows on the scratchpad. Push the line select key adjacent to ENTER PASSWORD indication to change the User Access Level.
Display/Result:
After correct password entry the message ANYBODY next to the USER ACCESS indication changes into LINEMTCE or ENGINEER.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Up, Down, Left, Right - Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID PASSWORD ! - Entered Password is not correct !
-----------------------------------------------------------------------------

(b) Statistic Counters
F AIDS - Statistic Counter ** ON A/C NOT FOR ALL
F AIDS - Statistic Counter ** ON A/C NOT FOR ALL
The AIDS maintains the Statistic Counter for Engine Flight Hours (EHRS) and Engine Cycles (ECYC). The Statistic Counter allows a manually preset of EHRS and ECYC.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Set COUNTER on the AIDS : SPECIAL FUNC/REPROG menu.
Entry:
To preset EHRS or/and ECYC enter the new value into the scratchpad and push the line select key adjacent to the data field, which must be changed.
Display:
On the Statistic Counter page 1/2 menu page the Engine Flight hours and on the page 2/2 the Engine Cycles are displayed. For change of the menu page use the up or down - arrow key.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! SCROLL ! - Default message at menu call-up !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Left, Right - Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Invalid decimal integer number !
!------------------------!--------------------------------------------------!
! OUT OF RANGE ! - Negative Number !
! ! - Number > 999999 !
-----------------------------------------------------------------------------

(c) AIDS Dump Disk Status Information
F AIDS - Dump Disk Status ** ON A/C NOT FOR ALL
The Dump Disk Status Information menu page shows which SAR reports are dumped from the Solid State Mass Memory (SSMM).
Display:
The Dump Disk Status Information page indicates DISK TYPE (MANUALLY, AUTO, ONLINE or NONE), Number of REPORTS, Number of SAR files and the Number of TOTAL dumped items. Additional the Number of free Dump disk spaces in Bytes shows next to the BYTES LEFT indication.
(d) AIDS Documentary Data
F AIDS - Documentary Data ** ON A/C NOT FOR ALL
The AIDS Documentary Data page displays data about Aircraft identification and AIDS software.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Set DOC DATA on the AIDS : SPECIAL FUNC/REPROG menu.
Display:
  • A/C TAIL-NO
  • A/C TYPE (Engine Type appended)
  • ENG Type
  • FLEET IDENT
  • P/N (software)
  • S/N (serial number)
  • LOAD-EN.
(e) AIDS Report Inhibit
F AIDS - Report Inhibit ** ON A/C NOT FOR ALL
F AIDS - Report Inhibit ** ON A/C NOT FOR ALL
The AIDS Report Inhibit menu allows to suppress or activate report generation.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Enter LINEMTCE or ENGINEER level user access password
  • Set INHIBIT on the AIDS SPECIAL FUNC/REPROG menu
  • Use the scroll arrows to get access to the next pages.
Disable/Enable:
  • Push the line key adjacent to ENABLE or DISABLE indication below the related report line.
Display:
On the multiple menu pages the available reports are displayed. Below each displayed report line the enabled/disabled status shows.
The indication ENABLED changes into DISABLED or DISABLED changes into ENABLED after selection of the line select key.
(f) AIDS Report Constant Reprogramming
F AIDS - Report Constants Reprogramming ** ON A/C NOT FOR ALL
Any constants of an AIDS report is changeable through the MCDU.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Enter LINEMTCE or ENGINEER level user access password
  • Set CONSTANTS on the AIDS SPECIAL FUNC/REPROG menu.
Enter/Change:
  • Enter the report number and push the line select key 1L to call-up the constants of the selected report.
  • Enter the new value and push the line select key adjacent to the constant to change the related constant value.
  • Push the CLR mode key and push the line select key adjacent to the constant to call-up the GSE programmed constant value.
Display:
Next to the selected REPORT indication the change - status shows:
  • CHANGED: NO displays that none of the listed constants of the selected report was changed through MCDU (or ACARS)
  • CHANGED: YES displays that al least one of the listed constants of the selected report was changed
  • CHANGED: --- displays that no MCDU programmable constants are defined.
The green displayed values of constants (AI reserved constants or inappropriate password) can not changed by the user.
All changed constants are marked with an exclamation mark (!).
If there is no programmable constants in the selected report the message NO MCDU PROGRAMMABLE CONSTANTS shows.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ENTER/INCR REPORT ! - Default message at menu call-up !
! NUMBER ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Left, Right - Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID ENTRY ! - LSK-1L: Entered character do not represent a !
! ! a valid integer number !
! ! - LSK-2L...5L: Entered characters do not !
! ! represent valid decimal number !
!------------------------!--------------------------------------------------!
! OUT OF RANGE ! - LSK-2L...5L: Entered number fits not into the !
! ! valid constant value range !
!------------------------!--------------------------------------------------!
! UNKNOWN REPORT ! - LSK-1L: Invalid report number !
! NUMBER ! !
-----------------------------------------------------------------------------


(g) Report Counter / Logic Reset
F AIDS - Report Counter / Logic Reset ** ON A/C NOT FOR ALL
This submenu resets or changes the report counter.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Enter LINEMTCE or ENGINEER level user access password
  • Set RESET on the AIDS: SPECIAL FUNC/REPROG menu
  • Use the scroll arrows to get access to the next pages.
Reset/Change:
  • To reset the report counter (reset to the GSE programmed value) push the CLR mode key and push the line select key adjacent to the associated report.
  • To change the report counter number enter the new value into the scratchpad and push the line key adjacent to the associated report.
Display:
On the multiple AIDS: REPORT RESET pages show the reports with the counter data as follows:
  • Report number and Report name (upper line)
  • Report Counter Name with current counter state (lower line)
  • Name of the counter re-initialization constant with the GSE programmed value (lower line in brackets).
If a counter is not changeable (no or wrong user access code) the current counter value shows in green color.
(h) Reprogrammable Reports
F AIDS - Reprogrammable Reports ** ON A/C NOT FOR ALL
This submenu shows a set of menus to define more reports, other than the baseline standard reports. These menus make possible the programming of the report names, triggering logics, contents and routing.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Enter LINEMTCE or ENGINEER level user access password
  • Set REPORTS on the AIDS: SPECIAL FUNC/REPROG menu
  • Set DEFINE on the AIDS: REPROGRAMMABLE RPTS menu.
Display:
  • LOGIC
  • CONTENTS
  • ROUTING.
The entry of the trigger(s) creates the REPORT LOGIC, defined with 4 fields:
  • ALPHA (parameter alphamnemonic)
  • OPER (operator)
  • VALUE (the value of the parameter that triggers the report, based on the operator)
  • CONN (connector).
It is possible to enter the report parameters in the REPORT CONTENTS submenu.
It is possible to set the status for routing to external devices in the REPORT ROUTING submenu. The default routing status must be 'NO'.
(4) AIDS Reprogramming Menus
  • Password Entry
  • Call-Up of Statistic Counter Submenu
  • Call-Up of Documentary Data
  • Call-Up of Report Inhibit Submenu
  • Call-Up of Report Reset Submenu
  • Call-Up of Report Constants Programming Submenu
  • Call-Up of Dump Status
  • Call-Up of Reprogrammable Reports Submenu.
(a) Password Entry
The access to any AIDS functions are protected through a password.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu.
Entry:
Enter the 8 character Security Access User identification into the scratchpad. For each character a asterisk (*) shows on the scratchpad. Push the line select key adjacent to ENTER PASSWORD indication to change the User Access Level.

Display/Result:
After correct password entry the message ANYBODY next to the USER ACCESS indication changes into LINEMTCE or ENGINEER.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
! ! !
!------------------------!--------------------------------------------------!
! ACCESS DENIED ! - Entered Password is not correct !
-----------------------------------------------------------------------------

(b) Statistic Counters
F AIDS - Statistic Counter ** ON A/C NOT FOR ALL
F AIDS - Statistic Counter ** ON A/C NOT FOR ALL
The AIDS maintains the Statistic Counter for Engine Flight Hours (EHRS) and Engine Cycles (ECYC). The Statistic Counter lets a manually preset of EHRS and ECYC.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Set COUNTERS on the AIDS : REPROG menu.
Entry:
To preset EHRS or/and ECYC enter the new value into the scratchpad and push the line select key adjacent to the data field, which must be changed.
Display:
On the Statistic Counter page 1/2 menu page the Engine Flight hours and on the page 2/2 the Engine Cycles are displayed. For change of the menu page use the up or down - arrow key.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! SCROLL ! - Default message at menu call-up !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Left, Right - Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Negative Number or !
! ! - LSK 1L Number > 9999 or !
! ! - LSK 2L Number > 99 or !
! ! - LSK 2R Number > 9999999999 !
-----------------------------------------------------------------------------

(c) AIDS Report Inhibit
F AIDS - Report Inhibit ** ON A/C NOT FOR ALL
The AIDS Report Inhibit menu allows to suppress or activate report generation.
Access:
  • Set AIDS on the MCDU main menu.
  • Set PROGRAMMING on the AIDS menu.
  • Enter LINEMTCE or ENGINEER level user access password.
  • Set PROGRAMMING MENUS on the AIDS DMU PROGRAMMING menu.
  • Set REPORT INHIBIT on the AIDS DMU PROGRAMMING menu.
    The AIDS REP INHIBIT ALL menu contains:
  • The asterisk (next to the YES or NO indication) indicates that the option is selectable. When no asterisk is present, the option is already selected.
  • YES PRINT NO* means PRINT allowed (for example there is no inhibit for print). The reports will therefore be printed if they have been defined in the database for print.
  • *YES PRINT NO means NO PRINT (for example printing is inhibited).
  • YES LINK NO* means ACARS allowed (for example there is no inhibit for ACARS).
  • *YES LINK NO means NO ACARS downlink (for example ACARS transmission is inhibited).
    The selection of PRINT or LINK inhibit functions is valid during the current flight, until next DMU power off.
(d) Report Counter / Logic Reset
This submenu resets or changes the report counter.
Access:
  • Set AIDS on the MCDU main menu
  • Set REPROGRAMMING on the AIDS menu
  • Enter LINEMTCE or ENGINEER level user access password
  • Set RESET on the AIDS: SPECIAL FUNC/REPROG menu
  • Use the scroll arrows to get access to the next pages.
Reset/Change:
  • To reset the report counter (reset to the GSE programmed value) push the CLR mode key and push the line select key adjacent to the associated report.
  • To change the report counter number enter the new value into the scratchpad and push the line key adjacent to the associated report.
Display:
On the multiple AIDS: REPORT RESET pages show the reports with the counter data as follows:
  • Report number and Report name (upper line)
  • Report Counter Name with current counter state (lower line)
  • Name of the counter re-initialization constant with the GSE programmed value (lower line in brackets).
If a counter is not changeable (no or wrong user access code) the current counter value shows in green color.
(5) List of Stored Reports
F AIDS - List of Stored Reports ** ON A/C NOT FOR ALL
As long as a report is stored in the report storage the respective report title and report number is listed. These reports are available for print out or for download or for downlink through ACARS.
Access:
  • Set AIDS on the MCDU main menu
  • Set STORED REPORTS on the AIDS menu
  • Use the scroll arrows to get access to the next pages.
Selection:
  • Push the NEXT PAGE key to change the output function.
  • Enter the Report number into the scratchpad and push the line select key 1L to find the related Report. To show all stored Reports enter XX into the scratchpad.
  • To clear pending output requests push the line select key adjacent to the asterix behind the displayed report (user access key necessary).
Display:
Above the listed reports the output selection shows. The current selected output device is on the left side and the alternate devices shows in the brackets.
The listed stored reports contain:
  • Flight leg number of report generation
  • Trigger code, trigger logic, which triggered the report
  • UTC of the report generation
  • Date of the report generation
  • Output status according the 'Immediate Output Rule'
  • Report number and
  • Report name.
If no reports are stored the message NO REPORTS shows.
Possible Output Status:
  • EOF : Waiting for End-Of-Flight
  • WPR : Waiting for printing
  • PRT : Printed
  • WDL : Waiting for downlink
  • ACS : In ACARS
  • DLK : Downlinked
  • WDR : Waiting for storage on DAR/WGL-DAR
  • DAR : Stored on DAR/WGL-DAR
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ?? SCROLL ! - Default message at menu call-up !
! ?? SELECT ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
!------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative --> Print out aborted !
!------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system --> Waiting for !
! ! Print out !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful print attempt --> Print out !
! PRTR ! aborted !
!------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU non operative --> Downlink aborted !
!------------------------!--------------------------------------------------!
! ACARS BUSY ! - ACARS-MU is busy with other system --> FDIMU !
! ! waits for downlink !
!------------------------!--------------------------------------------------!
! LINK NOT AVAILABLE ! - Link is currently not available --> Downlink !
! ! aborted !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful downlink attempt --> Downlink !
! ACARS ! aborted !
!------------------------!--------------------------------------------------!
! MDDU/DISK NOT ! - No AIDS Manual Dump Disk inserted or !
! AVAILABLE ! - No PDL connected or !
! ! - PDL/ADL not operative !
!------------------------!--------------------------------------------------!
! INSUFFICIENT DISK ! - Remaining disk space is not sufficient for !
! SPACE ! selected report --> Dump aborted !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful dump attempt --> Dump aborted !
! MDDU ! !
!------------------------!--------------------------------------------------!
! DISK SPACE: XXXX KBYTE ! - Remaining Disk space after successful report !
! ! dump !
-----------------------------------------------------------------------------


(6) List of Stored Reports
F AIDS - List of Stored Reports ** ON A/C NOT FOR ALL

As long as a report is stored in the report storage the respective report title and report number is listed related with the flight legs in which the report was given the related trigger code and a print, downlink and dump information is included in the list of the stored reports.

The list is on the MCDU request in menu form. The menu lets report call for printing, downlink through ACARS and dumping. Printing, dumping and downlinking is possible independent of previously done output functions.

Access:
  • Set AIDS on the MCDU main menu
  • Set STORED REPORTS on the AIDS menu
  • Use the scroll arrows to get access to the next pages.
Selection:
  • Push the NEXT PAGE key to change the output function.
  • Enter the Report number into the scratchpad and push the line select key 1L to find the related Report. To show all stored Reports enter XX into the scratchpad.
  • To clear pending output requests push the line select key adjacent to the asterisk behind the displayed report (user access key necessary).
Display:
Above the listed reports the output selection shows. The current selected output device is on the left side and the alternate devices shows in the brackets.

The listed stored reports contain:
  • Flight leg number of report generation
  • Trigger code, trigger logic, which triggered the report
  • UTC of the report generation
  • Date of the report generation
  • Output status refer to the 'Immediate Output Rule'
  • Report number and
  • Report name.
If no reports are stored the message NO REPORTS shows.
Possible Scratchpad Messages:
+---------------------------------------------------------------------------+
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ?? SCROLL ! - Default message at menu call-up !
! ?? SELECT ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
!------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative --> Print out aborted !
!------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system --> Waiting for !
! ! Print out !
!------------------------!--------------------------------------------------!
! QUEUED TO PRINTER ! - Report is in the printer queue --> Ready to be !
! ! printed !
!------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU not operative --> Downlink aborted !
!------------------------!--------------------------------------------------!
! ACARS BUSY ! - ACARS-MU is busy with other system --> FDIMU !
! ! waits for downlink !
!------------------------!--------------------------------------------------!
! QUEUED TO ACARS ! - Report is in the ACARS queue --> Ready to be !
! ! downlinked !
+---------------------------------------------------------------------------+


(7) Manual Report Request
F AIDS - Manual Report Request ** ON A/C NOT FOR ALL
The Manual Report Request menu allows an immediately report generation and output (Print, Store, Dump or Downlink).
Access:
  • Set AIDS on the MCDU main menu
  • Set MAN REQST REPORTS on the AIDS menu
  • Use the scroll arrows to get access to the next pages.
Report Trigger:
  • Push the right or left arrow key to change the output function. To trigger a report push the line select key adjacent to the asterix or '<' on the left side of the listed report number. If the Manual Report Request Format menu (Report <06>, <07>, <09> or <10> is selected) comes into view,push the line select key adjacent to the asterix of the related engine data.
Display:
The Manual Request Report menu contains 3 pages. Use the scroll arrows to get access to the previous or next page.
Above the listed reports the output selection shows. The current selected output device is on the left side and the alternate devices shows in the brackets.
If an asterix on the left side of the listed report is displayed, this report is triggered after selection. If a '<' character instead of an asterix is displayed the Manual Report Request Format page calls-up after selection.
In the Manual Report Request Format menu the Engine data format must be selected before generation of the report.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ?? SCROLL ! - Default message at menu call-up !
! ?? SELECT ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
! ! - Up, Down, Left, Right Arrow key !
!------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative --> Print out aborted !
!------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system --> Waiting for !
! ! Print out !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful print attempt --> Print out !
! PRTR ! aborted !
!------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU non operative --> Downlink aborted !
!------------------------!--------------------------------------------------!
! ACARS BUSY ! - ACARS-MU is busy with other system --> FDIMU !
! ! waits for downlink !
!------------------------!--------------------------------------------------!
! LINK NOT AVAILABLE ! - Link is currently not available --> Downlink !
! ! aborted !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful downlink attempt --> Downlink !
! ACARS ! aborted !
!------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - Displayed after selection of a report for !
! ! manual request and until report is printed or !
! ! downlinked !
!------------------------!--------------------------------------------------!
! REPORT NOT READY ! - Selected report can not be currently generated,!
! ! because generation of this report is in !
! ! progress due to an automatic trigger !
!------------------------!--------------------------------------------------!
! SELECT REPORT CONTENT ! - Default message at menu call-up !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful dump attempt --> Dump aborted !
! MDDU ! !
!------------------------!--------------------------------------------------!
! DISK SPACE: XXXX KBYTE ! - Remaining Disk space after successful report !
! ! dump !
-----------------------------------------------------------------------------


(8) Manual Report Request
F AIDS - Manual Report Request ** ON A/C NOT FOR ALL
The FDIMU provides through the MCDU a report selection menu to enable manual selection of reports for immediate generation and output to one of the following destinations:
+------------------------------------+
!Output device ! Output rule !
!--------------!---------------------!
! - Printer ! Print Immediately !
! - ACARS ! Downlink Immediately!
! - MDDU ! (no rule defined !
+------------------------------------+


Access:
  • Set AIDS on the MCDU main menu
  • Set MAN REQST REPORTS on the AIDS menu
  • Use the scroll arrows to get access to the next pages.
Report Trigger:
  • Push the right or left arrow key to change the output function. To trigger a report push the line select key adjacent to the asterisk or '<' on the left side of the listed report number.
Display:
The Manual Request Report menu contains 3 pages. Use the scroll arrows to get access to the previous or next page.
Above the listed reports the output selection shows. The current selected output device is on the left side and the alternate devices shows in the brackets.
An asterisk is displayed at this position if only a single data set or format was defined for the related report.
If multiple formats or data sets are defined for a report the "<" character is displayed instead of the asterisk at this position.
In the Manual Report Request Format menu the Engine data format must be selected before generation of the report.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ?? SCROLL ! - Default message at menu call-up !
! ?? SELECT ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
! ! - Up, Down, Left, Right Arrow key !
!------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - Displayed after selection of a report manual !
! ! request and until report is printed or down !
! ! linked !
!------------------------!--------------------------------------------------!
! REPORT NOT READY ! - Selected report can't be currently generated !
! ! because, generation of this report is in !
! ! progress due to an automatic trigger. !
!------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative --> Print out aborted !
!------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system --> FDIMU waits !
! ! for print out !
!------------------------!--------------------------------------------------!
! QUEUED TO PRINTER ! - Report is in printer queue --> Ready to print !
! ! out !
!------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU not operative --> Downlink aborted !
!------------------------!--------------------------------------------------!
! QUEUED TO ACARS ! - Report is in the ACARS queue --> Downlink to be!
! ! down linked !
+---------------------------------------------------------------------------+


(9) List of Stored SAR Data
F AIDS - List of Stored SAR Data ** ON A/C NOT FOR ALL
The list of stored SAR data shows the available SAR channels. After selection of the requested SAR channel the list of the SAR files calls-up. In addition this menu allows to initiate a dump of the selected channel and shows the allocated memory size of the SSMM.
Access:
  • Set AIDS on the MCDU main menu
  • Set STORED SAR DATA on the AIDS menu.
Selection:
  • Push the right line select key adjacent to the related SAR channel indication to dump all SAR files of this channel.
  • Push the left line select key adjacent to the related SAR channel indication to call-up the list of the SAR files.
  • To dump SAR files separately in the list of the SAR files push the left line select key adjacent to the related SAR file indication.
Display:
Below the SELECT CHANNEL DUMP indication the available SAR channels are listed.
Each listed SAR channel contains:
  • Title (or message CHANNEL NOT ASSIGNED)
  • SAR channel number and
  • Memory size indication.
If a SAR channel dump is selected, the color of the selected SAR channel indication changes into green and the message SAR x DUMP IN PROGRESS shows on the scratchpad while the dump procedure. If a SAR file menu is called-up the list of all stored SAR files of the selected SAR channel shows.
Each SAR file indication contains:
  • Flight leg
  • Trigger code
  • Date when the SAR file is triggered
  • UTC when the SAR file is triggered and
  • File size of the memory.
If the file is downloaded the DMP indication shows behind the file size indication.
If a SAR file dump is selected, the message FILE DUMP IN PROGRESS shows on the scratchpad while the download procedure.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! ?? SCROLL ! - Default message at menu call-up !
! ?? SELECT ! !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key !
! ! - Left, Right Arrow key !
!------------------------!--------------------------------------------------!
! MDDU/DISK NOT ! - No AIDS Manual Dump Disk inserted or !
! AVAILABLE ! - No PDL connected or !
! ! - PDL/ADL not operative !
! ! --> Dump aborted !
!------------------------!--------------------------------------------------!
! INSUFFICIENT DISK ! - Remaining disk space is not sufficient for !
! SPACE ! selected report --> Dump aborted !
!------------------------!--------------------------------------------------!
! CHANGE DISK TO ! - Remaining disk space is not sufficient for !
! CONTINUE ! next file to be dumped, but at least one file !
! ! of the channel dump has been already dumped !
! ! --> FDIMU is waiting to continue channel dump !
! ! on next disk !
!------------------------!--------------------------------------------------!
! SAR X DUMP IN PROGRESS ! - After dump initialization until completion of !
! ! channel dump 'X' represents the appropriate !
! ! SAR channel number; This message replace the !
! ! message CHANGE DISK TO CONTINUE once the next !
! ! Manual Dump Disk has been inserted !
!------------------------!--------------------------------------------------!
! DISK SPACE: XXXX KBYTE ! - Remaining Disk space after successful SAR !
! ! channel dump !
!------------------------!--------------------------------------------------!
! NOT TRANSMITTED TO ! - Unsuccessful dump attempt --> Dump aborted !
! MDDU ! !
!------------------------!--------------------------------------------------!
! SAR X DUMP ABORTED ! - Not all files of the selected SAR channel have !
! ! been successfully dumped --> Dump aborted !
!------------------------!--------------------------------------------------!
! FILE DUMP IN PROGRESS ! - After dump initialization until completion !
! ! of file dump !
-----------------------------------------------------------------------------


(10) Manual Request of SAR Recording
F AIDS - Manual Request of SAR Recording ** ON A/C NOT FOR ALL
The AIDS Manual SAR-Recording menu allows a manual start/stop control of the SAR recording through the MCDU. The manual start/stop control is independent from the GSE programmed automatic trigger conditions.
Access:
  • Set AIDS on the MCDU main menu
  • Set MAN REQST SAR/RECRDNG on the AIDS menu.
Selection:
  • Push the line select key adjacent to the START indication of the related SAR channel to initiate SAR recording manually.
  • Push the line select key adjacent to STOP indication of the running SAR channel to finish the recording manually.
Display:
Below the menu title line the available SAR channels are listed.
Each listed SAR channel contains:
  • Title (or message CHANNEL NOT ASSIGNED),
  • SAR channel number and
  • Run/Stop status indication.
Adjacent to the left line select keys the START or STOP indication shows to initiate the related SAR recording function.
Behind the SAR channel numbers the current start/stop indications (green) show:
  • STOPPED : The channel is inactive (neither manually nor automatically triggered).
  • RUNNING : The channel is active (neither manually or automatically triggered).

(11) DAR Recording Menu
F AIDS - DAR Recording ** ON A/C NOT FOR ALL
The AIDS Manual Request for DAR Recording menu allows a manual start/stop control of the DAR recording through the MCDU. The manual start/stop control is independent from the GSE programmed automatic trigger conditions.
Access:
  • Set AIDS on the MCDU main menu
  • Set DAR RECRDNG on the AIDS menu.
Selection:
  • Push the line select key adjacent to the MANUAL START indication (1L) to initiate DAR recording manually.
  • Push the line select key adjacent to the MANUAL STOP indication (1L) to finish the recording manually.
  • Push the line select key adjacent to the DISPLAY indication (1R) to get access to the AIDS DAR MONITOR menu.
  • On the DAR monitor menu enter a word number into the scratchpad and push the line select key (1L), (2L), (3L), (4L) or (5L) to display the appropriate data.
Display:
Below the title line the current start/stop status indication (green) shows:
  • STOPPED : The channel is inactive (neither manually nor automatically triggered).
  • RUNNING : The channel is active (neither manually or automatically triggered).
Adjacent to the left line select key (1L) the MANUAL START or MANUAL STOP indication shows to initiate the DAR recording function.
In addition the data of history time, recorder speed and data encoding show.
(12) AIDS Airline Functions Menu
F AIDS - Airline Function ** ON A/C NOT FOR ALL
The AIDS Airline Function menu gives access to the:
  • Password entry menu
  • DMU Programming functions.
(a) Password Entry
The access to the functions are password protected.
Access:
  • Set AIDS on the MCDU main menu
  • Set AIRLINE FUNCTION on the AIDS menu.
Entry:
Enter the eight character security-access user identification into the scratchpad. For each character a star (*) shows on the scratchpad. Push the line select key adjacent to ENTER PASSWORD indication to change the User Access Level.
Display/Result:
After correct password entry the message ANYBODY next to the USER ACCESS indication changes into LINEMTCE or ENGINEER.
Possible Scratchpad Messages:
-----------------------------------------------------------------------------
! Scratchpad Message ! Reason !
!------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK or !
! ! - Invalid MCDU Mode Key or !
! ! - Up, Down, Left, Right - Arrow Key !
!------------------------!--------------------------------------------------!
! INVALID PASSWORD ! - Entered Password is not correct !
-----------------------------------------------------------------------------

(b) DMU Programming Menu
The DMU programming menu gives access to the:
  • DAR RECORDING functions
  • REPORT PROGRAMMING functions
  • FTL PHASE LOGIC LIMITS functions.
Access:
  • Set AIDS on the MCDU main menu
  • Set AIRLINE FUNCTION on the AIDS menu
  • Set PROGRAMMING MENUS on the AIRLINE FUNCTION menu.
Selection:
  • Push the Line Select Key (LSK) adjacent to the DAR RECORDING indication (2L) to get access to the DAR recording function.
  • Push the LSK adjacent to REPORT PROGRAMMING indication (3L) to get access to the separate report programming function.
  • Push the LSK adjacent to the FLT PHASE LOGIC LIMITS (4L) to get access to the separate flight logic limts.
1 DAR Recording Menu
F AIDS - DAR Recording Function ** ON A/C NOT FOR ALL
The DAR recording menu gives the possibility to start or stop the DAR data recording in separate flight phases.
Access:
  • Set AIDS on the MCDU main menu
  • Set AIRLINE FUNCTION on the AIDS menu
  • Set PROGRAMMING MENUS on the AIRLINE FUNCTION menu
  • Set DAR RECORDING on the DMU PROGRAMMING menu
  • Set DAR PHASE RECORD or set DAR INTERMITTENT RECORDING on the DAR RECORDING menu.
Selection:
  • On the DAR PH RECORD menu push the Line Select Key (LSK) adjacent to the YES indication to start a DAR data record in the related flight phase.
  • On the DAR PH RECORD menu push the LSK adjacent to the NO indication to stop a DAR data record in the related flight phase.
  • On the DAR INTERMIT RECORDING menu push the LSK adjacent to the YES indication to stop a DAR data record in the related flight phase.
  • On the DAR INTERMIT RECORDING menu push the LSK adjacent to the NO indication to allow a DAR data record in the related flight phase.
Display:
  • The DAR stores flight data in a flight phase, if the STATUS indication for the related flight phase shows YES on the DAR PH RECORD menu.
  • The DAR stores flight data in a flight phase, if the STATUS indication for the related flight phase shows NO on the DAR INTERMIT RECORDING menu.
2 Report Programming Function
F AIDS - Report Programming Function ** ON A/C NOT FOR ALL
The report programming function gives the possibility to change the report output rules as a function of flight phases and/or trigger codes.
Access:
  • Set AIDS on the MCDU main menu
  • Set AIRLINE FUNCTION on the AIDS menu
  • Set PROGRAMMING MENUS on the AIRLINE FUNCTION menu
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu.
Selection:
  • Push the Line Select Key (LSK) adjacent to the REMOTE PRINT BUTTON indication to get access to the remote print-button function.
  • Push the LSK adjacent to the REPORT ROUTING indication to get access to the report routing functions.
  • Push the LSK adjacent to the REPORT INHIBIT indication to get access to the report inhibit functions.
  • Push the LSK adjacent to the REPORT CNTR INCREMENT indication to get access to the report-counter increment functions.
  • Push the LSK adjacent to the ECM REPORT indication to get access to the Engine Condition Monitoring (ECM) report functions.
a Remote Print Button Function
F AIDS - Remote Print Button Function ** ON A/C NOT FOR ALL
The remote print button function is used to give the possibility to do or to prevent the print of reports (report 1 thru 19) in a flight phase.
Access:
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu
  • Set REMOTE PRINT BUTTON on the REPORT PROGRAMMING menu.
Selection:
  • Set a report and push the Line Select Key (LSK) adjacent to it.
  • A remote print of the report in a related flight is possible, if you push the LSK adjacent to the YES indication.
  • To prevent the remote print of the report in a related flight phase push the LSK adjacent to the NO indication.
Display:
  • The STATUS indication on the REMOTE PRINT menu shows YES, if a remote print of the report is possible.
  • The STATUS indication on the REMOTE PRINT menu shows NO, if a remote print of the report is not possible.
b Report Routing Function
F AIDS - Report Routing Function ** ON A/C NOT FOR ALL
The report routing function is used to set the output media (printer, MDDU, PCMCIA, ACARS) of a triggered report.
Access:
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu
  • Set REPORT ROUTING on the REPORT PROGRAMMING menu.
Selection:
  • Set a report and push the Line Select Key (LSK) adjacent to it.
  • Scroll through the different menus to get access to the separate output medias and trigger codes.
  • Push the LSK adjacent to the YES indication to set the related output rule.
  • Push the LSK adjacent to the NO indication to prevent the related output rule.
Display:
  • The STATUS indication on the REPORT ROUTE shows YES, if the shown output rule is set.
  • The STATUS indication on the REMOTE PRINT menu shows NO, if the shown output rule is not set.
c Report Inhibit Function
F AIDS - Report Inhibit Function ** ON A/C NOT FOR ALL
The report inhibit function is used to prevent the generation of a report by a separate trigger code. For example, if you set the trigger code 4000 on the REPORT 06 INHIB page to YES, the generation of the report by trigger code 4000 is prevented.
Access:
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu
  • Set REPORT INHIBIT on the REPORT PROGRAMMING menu.
Selection:
  • Scroll through the pages and set the related report (e.g. report 06)
  • Push the Line Select Key (LSK) adjacent to the report name.
  • On the REPORT XX INHIB page use the LSK adjacent to the YES indications to prevent the report generation by the related trigger code.
  • Push the LSK adjacent to the NO indication to let the system do a report generation by a related trigger code.
  • Push the LSK adjacent to the YES indication to prevent the report generation by a related trigger code.
Display:
  • The STATUS indication on the REPORT XX INHIB menu shows NO, if the report generation by a related trigger code is possible.
  • The STATUS indication on the REPORT XX INHIB menu shows YES, if the report is not generated by the related trigger code.
d Report-Counter Increment Function
F AIDS - Report Counter Function ** ON A/C NOT FOR ALL
The report-counter increment function of the AIDS is used to set the report counter of a report (report 01 thru 19) on or off. A trigger code higher than 1000 increments the report counter of a report (report 01 thru 19), if the counter function is set to YES. If the function is set to NO the report counter function is set to off.
Access:
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu
  • Set REPORT CNTR INCREMENTT on the REPORT PROGRAMMING menu.
Selection:
  • Scroll through the pages and set the related report (e.g. report 01)
  • Push the Line Select Key (LSK) adjacent to the YES indication, if you want to have the counter function.
  • Push the LSK adjacent to the NO, if you want to prevent the counter function.
Display:
  • The STATUS indication on the REPORT CNTR INC page shows YES, if the counter function of the related report is on.
  • The STATUS indication on the REPORT CNTR INC page shows NO, if the counter function of the related report is off.
e ECM Reports Function
F AIDS - ECM Reports Function ** ON A/C NOT FOR ALL
The Engine Condition Monitoring (ECM) reports function is used to set the generation of ECM reports (ECM Take Off report, ECM Cruise report) on or off. The function also is used to set the output media (ACARS, printer, MDDU) of ECM reports.
Access:
  • Set REPORT PROGRAMMING on the DMU PROGRAMMING menu
  • Set ECM REPORTS on the REPORT PROGRAMMING menu.
Selection:
  • Push the LSK adjacent to the ECM REPORTS indication to get access to the ECM REPORTS ENABLE/DISABLE function.
  • Push the Line Select Key (LSK) adjacent to the ECM CRUISE REPORT or ECM TAKE OFF REPORT indication to get access to the ECM report route functions.
  • On the ECM REPORT ENABLE/DISABLE menu use the LSK adjacent to the ENABLE or DISABLE indication to set the generation of the shown reports on or off.
  • On the REPORT ROUTE MENU scroll through the pages to get access to the different output medias (ACARS, MDDU, printer). Use the LSK adjacent to the YES indication if you want to set a shown output media for a flight phase. Use the LSK adjacent to the NO indication, if you want to prevent the function.
Display:
  • An ECM Take Off or ECM Cruise report is generated by the AIDS, if the related STATUS indication on the ECM REPORTS page shows ENABLE. No report is generated, if the STATUS indication shows DISABLE.
  • A report is sent to the shown output media (ACARS, printer, MDDU), if the STATUS indication on the REPORT ROUTE MENU shows YES. If the STATUS indication shows NO, the AIDS does not send the report to the shown output media.
3 Flight-Phase Logic Limits Function
F AIDS - Flight-Phase Logic Limits Function ** ON A/C NOT FOR ALL
The flight-phase logic limits function gives the possibility to change the limits of the parameters:
  • ALT1
  • ALT2
  • IVV1
  • IVV2
  • IVV3
  • SLAT1.
Access:
  • Set AIDS on the MCDU main menu
  • Set AIRLINE FUNCTION on the AIDS menu
  • Set PROGRAMMING MENUS on the AIRLINE FUNCTION menu
  • Set FLT PHASE LOGIC LIMITS on the DMU PROGRAMMING menu.
Selection:
  • Choose the parameter you want to change with the left hand adjacent Line Select Key (LSK) (2L-5L).
  • Insert the new limit of the parameter with the scratchpad and push the right hand adjacent LSK (2R-5R) to confirm the new value.
J. MCDU AIDS Access Levels
All FDIMU functions, which can be manually activated by the user through the MCDU are protected by a user access control mechanism based on passwords. Security users identify themselves to the FDIMU by entering a password in the SPECIAL FUNCT/REPROGRAMMING menu. No password entry is necessary to get access to the 'Security User 1' functions (lowest access rights). The 'Security User 1' functions are enabled automatically after power-up of the FDIMU.
No password entry is necessary to branch into the sub-menus, to print MCDU screens and to enter report and SAR/DAR channel numbers for the purpose of menu selection.
Three user access levels are defined as follows:
----------------------------------------------------------------------
! Security Access User Identification !
!--------------------------------------------------------------------!
!No.! Code ! Name: ! Password !
!---!-----------------------------------------------------!----------!
! 1 ! ANYBODY ! Unidentified User ! XXXX !
!---!-----------------------------------------------------!----------!
! 2 ! LINEMTCE ! Line Maintenance ! LINE !
!---------------------------------------------------------!----------!
! 3 ! ENGINEER ! AIDS Engineer ! ENGI !
----------------------------------------------------------------------

The following table defines for each user function of the FDIMU the type of security user, for which these function are enabled.
-----------------------------------------------------------------------------
! Security User MCDU Function !Security !
! !Access User !
!-------------------------------------------------------------!-------------!
! Data Recording ! ANYBODY (1) !
! Run Control ! !
!-------------------------------------------------------------!-------------!
! Label Call-Up ! ANYBODY (1) !
!-------------------------------------------------------------!-------------!
! Alpha Call-Up ! ANYBODY (1) !
!-------------------------------------------------------------!-------------!
! Manual Report Request ! ANYBODY (1) !
! ! !
! Print Report ! !
! Send Report ! !
!-------------------------------------------------------------!-------------!
! List of stored Reports ! ANYBODY (1) !
! Print stored Reports ! !
! Send stored Reports ! !
! Dump stored Reports ! !
!-------------------------------------------------------------!-------------!
! Manual Request of SAR Recording ! ANYBODY (1) !
!-------------------------------------------------------------!-------------!
! Manual Dump of SAR Channels ! ANYBODY (1) !
!-------------------------------------------------------------!-------------!
! Manual Dump of SAR Files ! ANYBODY (1) !
!-------------------------------------------------------------!-------------!
! Enter Password !NO PROTECTION!
!-------------------------------------------------------------!-------------!
! Enter/Modify Statistic Counter Values ! LINEMTCE (2)!
! ! ENGINEER (3)!!
!-------------------------------------------------------------!-------------!
! Report Inhibit ! LINEMTCE (2)!
! ! ENGINEER (3)!
!-------------------------------------------------------------!-------------!
! Report Constants ! !
! Reprogramming ! !
! ! !
! Modify Values of Customer ! ENGINEER (3)!
! Programmable Constants of ! !
! the selected Report ! !
!-------------------------------------------------------------!-------------!
! Report Counter /Logic Reset ! LINEMTCE (2)!
! ! ENGINEER (3)!!
-----------------------------------------------------------------------------

It is possible to redefine the Security-Access User assignment on the GSE by the use of the reconfiguration software.
K. MCDU AIDS Menu Levels
The AIDS main menu gives access to these functions:
* Parameter Call-up:
- Parameter Label Call-Up
- Parameter Alpha Call-Up - Alpha Call Up Help
- Parameter Menus
* FDIMU (DMU-part) Software Load:
- Load Status
* Report Functions:
- List of Previous Reports
- Global List of Stored Reports
- Manual Report Request
* SAR/DAR Functions
- SAR Summary
- List of SAR stored Records (Data Recording, Extended Troubleshooting, Event
Recording
- SAR Manual Request
- DAR PCM
* PRINT BUTTON
- Assignment Remote Print
* Reprogramming
- Programming
* Programming Menus
- Programming Menus (Report Inhibit, Report Limits, Report Internal Counters,
Statistic Counters)

L. User Access Levels
All FDIMU functions, which can be manually activated by the user through the MCDU are protected by a user access control based on a password. Two user access levels are defined as follows:
----------------------------------------------------------------------
! Security Access User Identification !
!--------------------------------------------------------------------!
!No ! Code ! Name: ! Password !
!---!-----------------------------------------------------!----------!
! 1 ! ANYBODY ! Unidentified User ! -------- !
!---!-----------------------------------------------------!----------!
! 2 ! LINEMTCE ! Line Maintenance ! SFIM !
----------------------------------------------------------------------


No password entry is required to enable the access to the 'Security User No 1' (ANYBODY) protected AIDS functions. For the 'Security User No 2' (LINEMTCE) protected AIDS functions, the Security User Code (Password) can have a maximum of 8 digits.
Individual Security Access Control is provided for:
  • Each MCDU Menu
  • Each AIDS Report
  • Each SAR Channel.
    The contents of the Security MCDU Access Matrix represents the AI Standard Setup of the delivered FDIMU software.
    +---------------------------------------------------------------------------+
    ! Security User MCDU Function !Security !
    ! !Access User !
    !-------------------------------------------------------------+-------------!
    ! AIDS Main Menu ! No Access !
    ! - Manual DAR Start/Stop Control ! Restrictions!
    !-------------------------------------------------------------!-------------!
    ! Label Call-Up ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Alpha Call-Up ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Load Status ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Manual Report Request ! ANYBODY (1) !
    ! - List Selected Reports on MCDU screen ! !
    ! - Print Selected Report ! !
    ! - Send Selected Report (through ACARS) ! !
    !-------------------------------------------------------------!-------------!
    ! List of Stored Reports ! ANYBODY (1) !
    ! - List Selected Reports on MCDU screen ! !
    ! - Print Selected Report ! !
    ! - Send Selected Report (through ACARS) ! !
    !-------------------------------------------------------------!-------------!
    ! List of Previous Reports ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! SAR/DAR ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! SAR Summary ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! List of SAR Stored Record ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! SAR Manual Request ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! DAR PCM ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Assignment of Print Button ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Programming ! ANYBODY (1) !
    !-------------------------------------------------------------!-------------!
    ! Report Inhibit ! LINEMTCE (2)!
    !-------------------------------------------------------------!-------------!
    ! Report Limits ! LINEMTCE (2)!
    ! - Report Oil Table ! !
    !-------------------------------------------------------------!-------------!
    ! Report Int Counter ! LINEMTCE (2)!
    !-------------------------------------------------------------!-------------!
    ! Statistic Counters ! LINEMTCE (2)!
    -----------------------------------------------------------------------------


    It is possible to redefine the Security Access User assignment on the GSE by the use of the reconfiguration software. If a user has insufficient access privileges for a menu, he is able to call-up the menu but not to initiate any functions or to modify any data.
    All generated reports and SAR files are displayed in the respective menus. If a user has insufficient access privileges for specific reports or SAR files only the asterisks for initiation of report output is removed.
(1) Parameter Call Up Menu
The parameter call-up functions are a part of the FDIMU (DMU-part) operational software. The operation of the alpha call-up function depends on the availability of an alpha call-up table and an associated EUC table.
(a) Parameter Label Call-up
F Parameter Label Call-Up ** ON A/C NOT FOR ALL
Each parameter transmitted on one of the up to 64 ARINC 429 connected data buses are selectable for display on the MCDU screen. The selection are made using EQ, source system, label and SDI. Additionally the number of data bits to be used for decimal representation are selectable. The parts of the parameter number are isolated with a slash '/'.
The number of the data bits can be omitted. The default value is 18. The displayed parameters are updated once per second. Up to 2 parameters are displayed on one page. 8 pages can be selected via slew up/slew down button, which leads to a maximum number of 16 parameters to be monitored simultaneously.
Example : Parameter Call-Up with EQ and System Number
EQ/SYS/LAB/SDI = 1A/2/156/01

1 The procedure to select the Parameter Label Call-Up Menu is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'PARAM LABEL CALL-UP' on the AIDS Param Call-Up Menu.
  • Enter the parameter (e.g. 1C/1/344/01/12) on the scratchpad
  • Set the 1L key

2 Menu Definitions:
_____________________________________________________________________________
! EQ ! ARINC 429 equipment identification: !
! ! two-digit hexadecimal character e.g. 1B (for SFCC) !
!-----------!---------------------------------------------------------------!
! SYS ! System Number: !
! ! one character (only 1 to 4) !
!-----------!---------------------------------------------------------------!
! LAB ! ARINC 429 Label: !
! ! three-digit octal character (valid entries 000 - 377) !
!-----------!---------------------------------------------------------------!
! SDI ! Source Destination Identifier: !
! ! valid entries 00, 01, 10, 11 and XX (XX represents a case in !
! ! which the DMU samples the parameter without looking at the !
! ! SDI field) !
!-----------!---------------------------------------------------------------!
! DATABITS ! Identifies which ARINC 429 bits to extract from the label !
! ! call-up parameter and show as decimal value (valid entries !
! ! 1 to 20) !
!-----------!---------------------------------------------------------------!
! VALIDITY ! Validity of the requested parameter: !
! ! '>' parameter has not been transmitted/updated. !
! ! 'Blank' parameter has been updated. !
!-----------!---------------------------------------------------------------!
! SSM ! Sign Status Matrix: !
! ! is taken from bits 31 to 29 of the parameter and shows in !
! ! binary form. !
!-----------!---------------------------------------------------------------!
! DECIMAL ! Decimal value of the parameter calculated using the 'DATABITS'!
! VALUE ! entry to specify the number of bits to use as data. The !
! ! decimal value is calculated assuming the extracted data bits !
! ! as a whole represent a 2's complement value. For example !
! ! 'DATABITS' of 12 results in the decimal display of ARINC 429 !
! ! bits 28 to 17 . A 'DATABITS' entry of 20 results in a decimal !
! ! display of ARINC 429 bits 28 to 09. If bit 29=0, then the !
! ! decimal equivalent of the two complement of the 'DATABIT' !
! ! value will be preceded with a negative sign. !
!-----------!---------------------------------------------------------------!
! BINARY ! Binary Data (bits 28 to 11) of the parameter are shown on the !
! DATA ! on the line below the label 'DATABITS 28-11'. !
-----------------------------------------------------------------------------

3 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Equipment Identification (EQ) is not a !
! ! valid 2 character hex number !
! ! or - System Number (SYS) not within 1, 2 !
! ! or - Label (LAB) is not a valid 3 character octal!
! ! number within 000 to 377 !
! ! or - SDI code is not within '00', '01', '10', !
! ! '11', 'XX' !
! ! or - Number of databits is not a valid 2 digit !
! ! decimal number within 01 to 20 !
! ! or - At least one of the mandatory parameter !
! ! number parts EQ, SYS, LAB, SDI is missing !
! ! and has not been entered previously !
! ! or - Invalid delimeter character ('/') !
! ! or - Any further undefined characters !
!-------------------------!--------------------------------------------------!
! UNKNOWN EQ/SYS IDENT ! - ARINC-429 Equipment Identification (EQ) is !
! ! not defined in the DMU Setup Database !
! ! or - Entered System Number (SYS) is not defined !
! ! in the Setup Database for related Equipment !
! ! Identification (EQ). !
------------------------------------------------------------------------------

(b) Parameter Alpha Call-up
F Parameter Alpha Call-Up ** ON A/C NOT FOR ALL
For all the parameters, which are listed in the alpha call-up table. The selection is possible by their alpha codes. If parameters from two systems are available, both parameters are displayed on the MCDU upon a single alpha call-up code entry. The displayed parameter values are refreshed once per second.
All numeric type alpha call-up parameters are displayed on the MCDU in engineering units. The display format is a floating point representation of max. 6 characters including the decimal point and the '-' sign if applicable. In case of positive numbers without decimal point all 6 characters are available for digits. Display of loading zeros are suppressed. The applicable units are shown below the alpha call-up code on the MCDU screen.
Alpha call-up parameters, which consist of a combination of several discrete bits or packed discretes are displayed in hexadecimal representation. In this case the indication of the applicable units of the parameter are 'HEX'.

1 The procedure to select the Parameter Alpha Call-Up Menu is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'PARAM ALPHA CALL-UP' on the AIDS Parameter Call-Up Menu.
  • Enter the Alpha Call-Up Code on the adjacent LSK
  • Set the adjacent line key

  • Set 'CLEAR ALL'
  • all entries are deleted

2 Display indications:
-----------------------------------------------------------------------------
! ALPHA ! Alphanumeric name for specific aircraft parameter !
!-----------------!---------------------------------------------------------!
! SOURCE ! Name and system number of the source computer of !
! ! subsystem !
!-----------------!---------------------------------------------------------!
! POSITION ! Position identifier referenced to the aircraft !
!-----------------!---------------------------------------------------------!
! VALIDITY ! Validity of Alpha Call-up parameter: !
! ! - ':' (white) parameter has been updated and contains !
! ! valid SSM !
! ! - '>' (green) parameter has not been updated !
! ! - '<' (green) parameter contains invalid SSM !
!-----------------!---------------------------------------------------------!
! VALUE ! Value of parameter in engineering units. !
!-----------------!---------------------------------------------------------!
! UNITS ! Units associated with parameter !
-----------------------------------------------------------------------------


3 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! UNKNOWN ALPHA CODE ! - No valid Alpha Call-Up ASCII code or up to !
! ! 5 characters. !
! ! or - Any further undefined characters !
! ! - Alpha Call-Up code is not defined within !
! ! the DMU Database Software !
------------------------------------------------------------------------------

(c) AIDS Parameter Menu
F Parameter Menu ** ON A/C NOT FOR ALL

1 The procedure to set the Parameter Menus is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'MENUS' on the AIDS Parameter Call-Up Menu.
  • The display shows this sub menu:
    <FLIMOD
    <REPORT1
    <DIVERGENCE
    <RETURN
    PRINT*

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
------------------------------------------------------------------------------

(d) AIDS DMU Programming Menu

F AIDS FDIMU Programming ** ON A/C NOT FOR ALL
The AIDS DMU PROGRAMMING menu shows the A/C Type, the hardware part number, the operational software part number, the database version and revision level and date. Before you set the '<PROGRAMMING MENUS' the security access code have to be entered. The security access code has 8 characters. For each entered password character an asterisk '*' is placed into the scratchpad.
The submenus 'REPORT INHIBIT', 'REPORT LIMITS', 'REPORT COUNTERS' and 'STATISTIC COUNTERS' are selectable from the 'AIDS DMU PROGRAMMING' menu.

1 The procedure to get access to the PROGRAMMING menu is as follows:
  • Set 'AIDS' on the MCDU Menu
  • Set 'PROGRAMMING' on the AIDS Main Menu
  • Enter the password
  • Set the 'PROGRAMMING MENUS'.
  • The display shows these selections:
    <REPORT INHIBIT
    <REPORT LIMITS
    <REPORT COUNTERS
    <STATISTIC COUNTERS.

a REPORT INHIBIT Submenu

F AIDS FDIMU Programming ** ON A/C NOT FOR ALL
In this screen it is possible to inhibit the generation, printing and linking of all reports via the MCDU as follows:
  • the asterisk (next to the YES or NO indication) shows that you can select the option. If no asterisk is present, you can not select the option.
  • YES PRINT NO* shows that printing is permitted. The reports get printed if the reports were defined for print in the database.
  • *YES PRINT NO shows that printing is inhibited.
  • YES LINK NO* shows that the ACARS transmission is permitted.
  • *YES LINK NO shows that the ACARS transmission is inhibited.
NOTE: The selection of PRINT or LINK inhibit functions is valid during the current flight or until next DMU power off.
If more Free Programmable Reports are created by the GSE, the list of reports in the Report Inhibit submenu are extended subsequently. Password access is programmable for this function.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK !
! ! or - Invalid MCDU Mode Key !
!-------------------------!--------------------------------------------------!
! ACCESS DENIED ! !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Negative number !
! (Report Limits only) ! or - LSK 1L Number > 9999 !
! ! or - LSK 2L Number > 99 !
! ! or - LSK 2R Number > 9999999999 !
!-------------------------!--------------------------------------------------!
! VALIDATE OK ! - SET COUNTERS Function activated !
! (Report 1, 4, 9 and 10) ! !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Negative number !
! (Statistic Count. only) ! or - Number > 99999 !
------------------------------------------------------------------------------

(e) SAR Recording Menu
F SAR Recording ** ON A/C NOT FOR ALL
The SAR stores data in a Solid State Mass Memory (SSMM). The data is compressed in the storage and organized in one SAR File. Three different modes are provided:
- DATA Recording
* Storage of up four user predefined datasets (each up to 128 samples per
second) between a start event and stop event
* 25 start/stop events are provided
* The data is collected for each trigger event with up to 5 minutes of
history data.
- Extended Troubleshooting
* Storage of up to four user predefined datasets with pre event data when a
start event is met
* 25 events are provided
* The data are collected for each trigger event for up to 5 minutes of
history data.
- Event Recording
* Storage, when an event is detected, of a user predefined dataset (15
selectable parameters) specific for each event
* Up to 50 different events are provided


1 The procedure to set the SAR menus is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'SAR' on the AIDS Main Menu.
  • The following previous menus are shown:
    <SAR SUMMARY
    <List of SAR RECORDS
    <MAN request SAR
    <SAR PCM

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - data set greater than the maximum of data !
! ! sets available !
!-------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - displayed when: !
! ! * manual start is effective !
! ! * during the whole recording if no message !
! ! has to be displayed !
------------------------------------------------------------------------------

(f) Remote Print Assignment Menu
F Remote Print Assignment ** ON A/C NOT FOR ALL
The 'Remote Print' page shows the Report Number, Engine Number, DMU-part Internal PH and incrementation of report counter (Y=incremented N=not incremented).

1 The procedure to get access to the Remote Print page is as follows:
  • Set 'AIDS' on the MCDU menu.
  • Set 'REMOTE PRINT' on the AIDS main menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!

(g) Software Loading Menu
F AIDS Software Loading ** ON A/C NOT FOR ALL
The 'SOFTWARE LOADING' page shows the actual status of the software loading process (TRANSFER IN PROGRESS or NO TRANSFER IN PROGRESS).
If the AIDS is available, the 'LOAD STATUS' is automatically displayed on the MCDU screen.

1 The procedure to get access to the LOAD STATUS page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LOAD STATUS' on the AIDS Main Menu.
  • The MCDU screen shows the actual status.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
! ! or - Any ASCII Key !
!-------------------------!--------------------------------------------------!
! Bad A/C tail ! - The A/C tail read on FDIU bus is not among !
! ! the one of the diskettes (File ACQUIT.MEM) !
!-------------------------!--------------------------------------------------!
! Bad S/W Num ! - The software reference number written on !
! ! diskette (File ACQUIT.MEM) is not available !
! ! with the resident software or the loading !
! ! software. !
!-------------------------!--------------------------------------------------!
! Bad retrieval date ! - The retrieval date of the diskette !
! ! (File ACQUIT.MEM) has expired. Build a new !
! ! disk for data retrieval on GSE. !
!-------------------------!--------------------------------------------------!
! Not on ground ! - This operation is not allowed when aircraft !
! ! is flying. !
!-------------------------!--------------------------------------------------!
! Missing file name ! - During the OBPM loading, the software has !
! ! not found the file name on this diskette. !
!-------------------------!--------------------------------------------------!
! Timeout file name ! - During OBPM loading, an error has occurred !
! ! on processor 2 or 3 when file name has been !
! ! opened. !
!-------------------------!--------------------------------------------------!
! Disk error ! - During the transfer, a disk error has !
! ! occurred. !
!----------------------------------------------------------------------------!

(h) Database Loading Menu
F AIDS Database Loading ** ON A/C NOT FOR ALL
During the OBPM loading, the MCDU shows automatically the OBPM loading menu, if AIDS is set. It is impossible to select the return key to get access to another menu.
At the end of the loading process the message 'LOAD COMPLETED' is displayed. If any error shows during the load process the message 'LOAD FAILED' is shown.

1 The procedure to get access to the LOAD STATUS page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LOAD STATUS' on the AIDS main menu.
  • The MCDU screen shows the actual status.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(i) AIDS Previous Reports Menu
F AIDS Previous Reports ** ON A/C NOT FOR ALL
The 'PREVIOUS REPORT' page shows the Report Number, Trigger Code, Date, UTC and the Flight Leg (00=current flight leg XX=previous leg).

1 The procedure to get access to the AIDS PREVIOUS REPORTS is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LIST OF PREV REP' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(j) Stored Reports Menu
F AIDS Stored Reports ** ON A/C NOT FOR ALL
The 'STORED REPORTS' page shows a list of all AI reports, which are generated and stored in the FDIMU report buffer. To show each report push the adjacent line select key. To print them push the print line select key.
All stored reports are deleted as soon as a new A/C ident (A/C tailnumber) is recognized by the FDIMU.

1 The procedure to get access to the AIDS STORED REPORTS is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'STORED REPORTS' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(k) Manual Request Reports Menu
F Manual Request Reports ** ON A/C NOT FOR ALL
The 'MAN REQST REPRT' page shows a list of all AI reports, which is generated, if you push the adjacent line key. The 1L key is used to roll options 'PRINT, SEND (ACARS) or STORE'.
An asterisk '*' is displayed at the beginning of each report, if only a single data set or format is defined for the related report.
If multiple formats or data sets are defined for a report, the '<' character is displayed instead of the asterisk.
If the report storage is full and a generated report is stored in the report buffer, the oldest free declared report is deleted to enable the storage on an actual report. In case that the report storage is full with no free declared reports the oldest report is printed and deleted if stored capacity is required.
When a report is set and complete generated it is printed or sent via ACARS.

1 The procedure to get access to the MANUEL REQUEST REPORT is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'MAN REQST REPORTS' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - Display after selection of a report for !
! ! manual request and until report is printed !
! ! or downlinked via ACARS !
!-------------------------!--------------------------------------------------!
! REPORT NOT READY ! - Selected report can not be currently !
! ! generated because, generation of this report!
! ! is in progress due to an automatic trigger !
!-------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative !
! ! --> Print Out aborted !
!-------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system !
! ! --> DMU waits for print out !
!-------------------------!--------------------------------------------------!
! QUEUED TO PRINTER ! - Report is in the printer queue !
! ! --> Ready to print out !
!-------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU not operative !
! ! --> Downlink aborted !
!-------------------------!--------------------------------------------------!
! ACARS BUSY ! - ACARS-MU is busy with other systems !
! ! --> DMU waits for downlink !
!-------------------------!--------------------------------------------------!
! QUEUED TO ACARS ! - Report is in the ACARS queue !
! ! --> Ready to be downlinked !
!-------------------------!--------------------------------------------------!

(l) AIDS Disk Menu
The 'AIDS DISK MENU' shows the submenus DISK IDENT for the PCMCIA media status, DISK DIRECTORY for submenus to the PCMCIA directory and DAR RECORD for submenus to the DAR emulated record status.

1 The procedure to get access to the AIDS DISK MENU is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

3 AIDS Disk Ident Page
F AIDS Disk Ident Page ** ON A/C NOT FOR ALL
The 'AIDS DISK IDENT' page shows the status of the PCMCIA disk. The hardware information consist of a part number, a serial number and disk maintenance word. The additional disk space information shows the free and total space in Kbytes.

4 The procedure to get access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DISK IDENT' on the AIDS DISK Menu

5 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

6 AIDS Disk Directory Menu
F AIDS Disk Directory Page ** ON A/C NOT FOR ALL
The 'DISK DIRECTORY' page has the function to open the next PCMCIA disk directory level. If one of the files is set by the key the next directory is shown. The path is shown on the top. The function key UP* decreases the directory offset and DOWN* increases the directory offset. The key adjacent to *HEX (TEXT) switches the display mode from hexadecimal to text.

7 The procedure to get access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DISK DIRECTORY' on the AIDS DISK menu.

8 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

9 AIDS Disk DAR Record Page
F AIDS Disk DAR Record Page ** ON A/C NOT FOR ALL
The 'AIDS DISK DAR RECORD' page shows the emulated status of the DAR function by the PCMCIA disk. Record status, record file name, record length and free/total disk space in Kbytes are displayed.

10 The procedure to access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DAR RECORD' on the AIDS Disk menu.

11 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(2) AIDS Parameter Menu
(a) Parameter Menus
F AIDS - Parameter Menu ** ON A/C NOT FOR ALL

1 The procedure to set the Parameter Menus is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PARAM' on the AIDS Main Menu.
  • Set 'MENUS' on the AIDS Parameter Call-Up Menu.
  • The display shows this sub menu:
    <FLIMOD
    <REPORT1
    <DIVERGENCE
    <RETURN
    PRINT*

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
------------------------------------------------------------------------------

(b) AIDS DMU Programming Menu

F AIDS FDIMU Programming ** ON A/C NOT FOR ALL
The AIDS DMU PROGRAMMING menu shows the A/C Type, the hardware part number, the operational software part number, the database version and revision level and date. Before you set the '<PROGRAMMING MENUS' the security access code have to be entered. The security access code has 8 characters. For each entered password character an asterisk '*' is placed into the scratchpad.
The submenus 'REPORT INHIBIT', 'REPORT LIMITS', 'REPORT COUNTERS' and 'STATISTIC COUNTERS' are selectable from the 'AIDS DMU PROGRAMMING' menu.

1 The procedure to get access to the PROGRAMMING menu is as follows:
  • Set 'AIDS' on the MCDU Menu
  • Set 'PROGRAMMING' on the AIDS Main Menu
  • Enter the password
  • Set the 'PROGRAMMING MENUS'.
  • The display shows these selections:
    <REPORT INHIBIT
    <REPORT LIMITS
    <REPORT COUNTERS
    <STATISTIC COUNTERS.

a REPORT INHIBIT Submenu

F AIDS - Report Inhibit ** ON A/C NOT FOR ALL
In this screen it is possible to inhibit the generation, printing and linking of all reports through the MCDU as follows:
  • the asterisk (next to the YES or NO indication) shows that you can select the option. If no asterisk is present, you can not select the option.
  • YES PRINT NO* shows that printing is permitted. The reports get printed if the reports were defined for print in the database.
  • *YES PRINT NO shows that printing is inhibited.
  • YES LINK NO* shows that the ACARS transmission is permitted.
  • *YES LINK NO shows that the ACARS transmission is inhibited.
NOTE: The selection of PRINT or LINK inhibit functions is valid during the current flight or until next DMU power off.
If more Free Programmable Reports are created by the GSE, the list of reports in the Report Inhibit submenu are extended subsequently. Password access is programmable for this function.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Undefined LSK !
! ! or - Invalid MCDU Mode Key !
!-------------------------!--------------------------------------------------!
! ACCESS DENIED ! !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Negative number !
! (Report Limits only) ! or - LSK 1L Number > 9999 !
! ! or - LSK 2L Number > 99 !
! ! or - LSK 2R Number > 9999999999 !
!-------------------------!--------------------------------------------------!
! VALIDATE OK ! - SET COUNTERS Function activated !
! (Report 1, 4, 9 and 10) ! !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - Negative number !
! (Statistic Count. only) ! or - Number > 99999 !
------------------------------------------------------------------------------

(c) SAR Recording Menu
The SAR stores data in a Solid State Mass Memory (SSMM). The data is compressed in the storage and organized in one SAR File. Three different modes are provided:
- DATA Recording
* Storage of up four user predefined datasets (each up to 128 samples per
second) between a start event and stop event
* 25 start/stop events are provided
* The data is collected for each trigger event with up to 5 minutes of
history data.
- Extended Troubleshooting
* Storage of up to four user predefined datasets with pre event data when a
start event is met
* 25 events are provided
* The data are collected for each trigger event for up to 5 minutes of
history data.
- Event Recording
* Storage, when an event is detected, of a user predefined dataset (15
selectable parameters) specific for each event
* Up to 50 different events are provided


1 The procedure to set the SAR menus is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'SAR' on the AIDS Main Menu.
  • The following previous menus are shown:
    <SAR SUMMARY
    <List of SAR RECORDS
    <MAN request SAR
    <SAR PCM

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! INVALID ENTRY ! - data set greater than the maximum of data !
! ! sets available !
!-------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - displayed when: !
! ! * manual start is effective !
! ! * during the whole recording if no message !
! ! has to be displayed !
------------------------------------------------------------------------------

(d) Remote Print Assignment Menu
F Remote Print Assignment ** ON A/C NOT FOR ALL
The 'Remote Print' page shows the Report Number, Engine Number, DMU-part Internal PH and incrementation of report counter (Y=incremented N=not incremented).

1 The procedure to get access to the Remote Print page is as follows:
  • Set 'AIDS' on the MCDU menu.
  • Set 'REMOTE PRINT' on the AIDS main menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!

(e) Software Load Status Menu
F Software Load Status ** ON A/C NOT FOR ALL
F AIDS Software Loading ** ON A/C NOT FOR ALL
The 'SOFTWARE LOAD STATUS' page shows the actual status of the software loading process (TRANSFER IN PROGRESS or NO TRANSFER IN PROGRESS).
If the AIDS is available, the 'LOAD STATUS' is automatically displayed on the MCDU screen.

1 The procedure to get access to the LOAD STATUS page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LOAD STATUS' on the AIDS Main Menu.
  • The MCDU screen shows the actual status.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
! ! or - Any ASCII Key !
!-------------------------!--------------------------------------------------!
! Bad A/C tail ! - The A/C tail read on FDIU bus is not among !
! ! the one of the diskettes (File ACQUIT.MEM) !
!-------------------------!--------------------------------------------------!
! Bad S/W Num ! - The software reference number written on !
! ! diskette (File ACQUIT.MEM) is not available !
! ! with the resident software or the loading !
! ! software. !
!-------------------------!--------------------------------------------------!
! Bad retrieval date ! - The retrieval date of the diskette !
! ! (File ACQUIT.MEM) has expired. Build a new !
! ! disk for data retrieval on GSE. !
!-------------------------!--------------------------------------------------!
! Not on ground ! - This operation is not permitted when !
! ! aircraft is flying. !
!-------------------------!--------------------------------------------------!
! Missing file name ! - During the OBPM loading, the software has !
! ! not found the file name on this diskette. !
!-------------------------!--------------------------------------------------!
! Timeout file name ! - During OBPM loading, an error has occurred !
! ! on processor 2 or 3 when file name was !
! ! opened. !
!-------------------------!--------------------------------------------------!
! Disk error ! - During the transfer, a disk error has !
! ! occurred. !
!-------------------------!--------------------------------------------------!
! Invalid disk ! - PCMCIA card not valid for loading. !
! configuration ! !
+----------------------------------------------------------------------------+

(f) Database Loading Menu
F AIDS Database Loading ** ON A/C NOT FOR ALL
During the OBPM loading, the MCDU shows automatically the OBPM loading menu, if AIDS is set. It is impossible to select the return key to get access to another menu.
At the end of the loading process the message 'LOAD COMPLETED' is displayed. If any error shows during the load process the message 'LOAD FAILED' is shown.

1 The procedure to get access to the LOAD STATUS page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LOAD STATUS' on the AIDS main menu.
  • The MCDU screen shows the actual status.

2 Possible Scratchpad Messages:
+----------------------------------------------------------------------------+
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Any ASCII Key !
+----------------------------------------------------------------------------+

(g) AIDS Previous Reports Menu
The 'PREVIOUS REPORT' page shows the Report Number, Trigger Code, Date, UTC and the Flight Leg (00=current flight leg XX=previous leg).

1 The procedure to get access to the AIDS PREVIOUS REPORTS is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'LIST OF PREV REP' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(h) Stored Reports Menu
F AIDS - List of Stored Reports ** ON A/C NOT FOR ALL
The 'STORED REPORTS' page shows a list of all AI reports, which are generated and stored in the FDIMU report buffer. To show each report push the adjacent line select key. To print them push the print line select key.
All stored reports are deleted as soon as a new A/C ident (A/C tailnumber) is recognized by the FDIMU.

1 The procedure to get access to the AIDS STORED REPORTS is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'STORED REPORTS' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

(i) Manual Request Reports Menu
F AIDS - Manual Report Request ** ON A/C NOT FOR ALL
The 'MAN REQST REPRT' page shows a list of all AI reports, which is generated, if you push the adjacent line key. The 1L key is used to roll options 'PRINT, SEND (ACARS) or STORE'.
An asterisk '*' is displayed at the beginning of each report, if only a single data set or format is defined for the related report.
If multiple formats or data sets are defined for a report, the '<' character is displayed instead of the asterisk.
If the report storage is full and a generated report is stored in the report buffer, the oldest free declared report is deleted to enable the storage on an actual report. In case that the report storage is full with no free declared reports the oldest report is printed and deleted if stored capacity is required.
When a report is set and complete generated it is printed or sent through ACARS.

1 The procedure to get access to the MANUEL REQUEST REPORT is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'MAN REQST REPORTS' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!-------------------------!--------------------------------------------------!
! GENERATION IN PROGRESS ! - Display after selection of a report for !
! ! manual request and until report is printed !
! ! or downlinked through ACARS !
!-------------------------!--------------------------------------------------!
! REPORT NOT READY ! - Selected report can not be currently !
! ! generated because, generation of this report!
! ! is in progress due to an automatic trigger !
!-------------------------!--------------------------------------------------!
! PRINTER NOT AVAILABLE ! - Printer not operative !
! ! --> Print Out aborted !
!-------------------------!--------------------------------------------------!
! PRINTER BUSY ! - Printer used by other system !
! ! --> DMU waits for print out !
!-------------------------!--------------------------------------------------!
! QUEUED TO PRINTER ! - Report is in the printer queue !
! ! --> Ready to print out !
!-------------------------!--------------------------------------------------!
! ACARS NOT AVAILABLE ! - ACARS-MU not operative !
! ! --> Downlink aborted !
!-------------------------!--------------------------------------------------!
! ACARS BUSY ! - ACARS-MU is busy with other systems !
! ! --> DMU waits for downlink !
!-------------------------!--------------------------------------------------!
! QUEUED TO ACARS ! - Report is in the ACARS queue !
! ! --> Ready to be downlinked !
!-------------------------!--------------------------------------------------!

(j) AIDS Disk Menu
F AIDS Disk Ident Page ** ON A/C NOT FOR ALL
The 'AIDS DISK MENU' shows the following submenus:
  • < DISK IDENT for the PCMCIA media status,
  • < DISK DIRECTORY for submenus to the PCMCIA directory
  • < DAR RECORD for submenus to the DAR emulated record status and
  • < WEFA.

1 The procedure to get access to the AIDS DISK MENU is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.

2 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

3 AIDS Disk Ident Page
F AIDS Disk Ident Page ** ON A/C NOT FOR ALL
The 'AIDS DISK IDENT' page shows the status of the PCMCIA disk. The hardware information consist of a part number, a serial number and disk maintenance word. The additional disk space information shows the free and total space in Kbytes.

4 The procedure to get access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DISK IDENT' on the AIDS DISK Menu

5 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

6 AIDS Disk Directory Menu
F AIDS Disk Directory Page ** ON A/C NOT FOR ALL
The 'DISK DIRECTORY' page has the function to open the next PCMCIA disk directory level. If one of the files is set by the key the next directory is shown. The path is shown on the top. The function key UP* decreases the directory offset and DOWN* increases the directory offset. The key adjacent to *HEX (TEXT) switches the display mode from hexadecimal to text.

7 The procedure to get access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DISK DIRECTORY' on the AIDS DISK menu.

8 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

9 AIDS Disk DAR Record Page
F AIDS Disk DAR Record Page ** ON A/C NOT FOR ALL
The 'AIDS DISK DAR RECORD' page shows the emulated status of the DAR function by the PCMCIA disk. Record status, record file name, record length and free/total disk space in Kbytes are displayed.

10 The procedure to access to the AIDS DISK IDENT page is as follows:
  • Set 'AIDS' on the MCDU Menu.
  • Set 'PCMCIA' on the AIDS Main Menu.
  • Set 'DAR RECORD' on the AIDS Disk menu.

11 Possible Scratchpad Messages:
------------------------------------------------------------------------------
! Message ! Explanations !
!-------------------------!--------------------------------------------------!
! NOT ALLOWED ! - Invalid LSK !
! ! or - Invalid MCDU Mode Key !
! ! or - Up, Down - Arrow Key !
!----------------------------------------------------------------------------!

** ON A/C NOT FOR ALL
8. Test BITE
A. General
The FDIMU contains Built-In Test Equipments (BITE) related to ARINC 604 regulations. One is for the DFDRS part and a second is for the AIDS part. The BITE's are able to detect at least 95% of the possible failures in the FDIMU. The found failures are divided in system internal faults (FDIMU, DAR) and external faults (connected systems). If a failure is found, the BITE stores the failure messages in the FDIMU BITE memory and sends these continuously to the CFDS through the ARINC 429 output bus. The failures can be called up through the CFDS on the MCDU display.
B. Test
(1) POR BITE
After each Power-On-Reset (POR) the FDIMU does a POR Built-In Test (BITE). For a POR the electrical power must be interrupt greater than 200 msec. In case of the FDIMU does not operate in the correct mode you can do a manual Power-up initialization through open the circuit breaker 5TV for 5 seconds. The POR BITE will be done after each POR independent of ON-GROUND or IN-FLIGHT configuration. The POR BITE is completed within 2 seconds and before the AIDS application software is started.
The POR BITE covers the functions as follows:
  • Power Supply / Battery Test
  • Microprocessor Function / Test of Microprocessor Control Circuitry (e.g. Timer, Watchdog, interrupt control)
  • System Bus / Interprocessor Communication Test
  • External Interface Test (Wrap-Around Tests)
  • E(E) PROM Memory Test
  • Local SRAM Memory Test
(2) FDIMU Test through the MCDU
  • The CFDS provides two test functions for the AIDS:
  • FDIMU Power-up Test (AIDS part)
  • FDIMU Battery Test
The tests are initiated through the MCDU in the AIDS test menu. The message TEST OK comes into view when the test result is positive. If a failure is found, the AIDS Test Result menu comes on.
The AIDS Test Result menu shows:
  • LRU(s) name
  • FIN number
  • associated ATA reference
  • failure class
  • failure message text.

(a) The FDIMU Power-up Test
The Power-up test initiates the complete BITE procedure (POR BITE) which will be done after a power-on of the FDIMU. Additional the test reports the external failures.

(b) The FDIMU Battery Test
The battery test checks the condition of the batteries. If both batteries are still sufficient charged the message BATTERIES OK comes into view. If the charge of at least one of the batteries is insufficient or at least one of the batteries is dead, the AIDS Test Result menu comes on.

(3) FDIMU Test through the Test Connector
In the repair shop the FDIMU test with a test-set and a Personal Computer is possible through the test connector (refer manufacturer manuals).
C. AIDS Failure Messages
+-----------------------------------------------------------------------------+
! Message ! Failure Message Text ! Source ! Chapter ! Failure Class !
! No ! ! ! ! !
!---------!------------------------------!----------!---------!---------------!
! 1.00 ! Power Supply Interrupt ! FDIMU ! 240000 ! Extern I !
! 1.01 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern II !
! 1.04 ! DAR (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.05 ! DAR MEDIA LOW (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.06 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.07 ! FDIMU Battery (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.08 ! FDIMU PCMCIA MEDIA (10TV) ! FDIMU ! 313634 ! Intern II !
! 2.00 ! ATSU1 (1TX1) / FDIMU (10TV) ! ATSU ! 462134 ! Extern III !
! 3.00 ! CFDIU (1TW1) / FDIMU (10TV) ! CFDIU ! 451334 ! Extern III !
! 4.01 ! MCDU 1 (3CA1) / FDIMU (10TV) ! MCDU 1 ! 228212 ! Extern III !
! 4.02 ! MCDU 2 (3CA2) / FDIMU (10TV) ! MCDU 2 ! 228212 ! Extern III !
! 6.00 ! PRINTER (4TW) / FDIMU (10TV) ! Printer ! 313522 ! Extern III !
! 7.01 ! ADIRU 1 (1EP1) / FDIMU (10TV)! ADIRU 1 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.02 ! ADIRU 2 (1EP2) / FDIMU (10TV)! ADIRU 2 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.03 ! ADIRU 3 (1EP3) / FDIMU (10TV)! ADIRU 3 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 8.01 ! BMC 1 (1HA1) / FDIMU (10TV) ! BMC 1 ! 361134 ! Extern III !
! 8.02 ! BMC 2 (1HA2) / FDIMU (10TV) ! BMC 2 ! 361134 ! Extern III !
! 9.00 ! FQU (3QT) / FDIMU (10TV) ! FQU ! 284234 ! Extern III !
! 10.01 ! CPC 1 (11HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 1 ! ! !
! 10.02 ! CPC 2 (12HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 2 ! ! !
! 11.01 ! DMC 1 (1WT1) / FDIMU (10TV) ! DMC 1 ! 316334 ! Extern III !
! 11.02 ! DMC 2 (1WT2) / FDIMU (10TV) ! DMC 2 ! 316334 ! Extern III !
! 12.00 ! ECB (59KD) / FDIMU (10TV) ! APU ECB ! 496134 ! Extern III !
! 13.00 ! EVMU (2EV) / FDIMU (10TV) ! EVMU ! 773234 ! Extern III !
! 14.01 ! FCDC 1 (3CE1) / FDIMU (10TV) ! FCDC 1 ! 279534 ! Extern III !
! 14.02 ! FCDC 2 (3CE2) / FDIMU (10TV) ! FCDC 2 ! 279534 ! Extern III !
! 15.01 ! FAC 1 (1CC1) / FDIMU (10TV) ! FAC 1 ! 226634 ! Extern III !
! 15.02 ! FAC 2 (1CC2) / FDIMU (10TV) ! FAC 2 ! 226634 ! Extern III !
! 16.00 ! FCU (2CA) / FDIMU (10TV) ! FCU A, B ! 228112 ! Extern III !
! 17.00 ! FDIU (10TV) / FDIMU (10TV) ! FDIMU ! 313634 ! Extern III !
! 18.01 ! FMGC 1 (1CA1) / FDIMU (10TV) ! FMGC 1 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 18.02 ! FMGC 2 (1CA2) / FDIMU (10TV) ! FMGC 2 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 19.01 ! FWC 1 (1WW1) / FDIMU (10TV) ! FWC 1 ! 315334 ! Extern III !
! 19.02 ! FWC 2 (1WW2) / FDIMU (10TV) ! FWC 2 ! 315334 ! Extern III !
! 20.00 ! GPWC (1WZ) / FDIMU (10TV) ! GPWC ! 344834 ! Extern III !
! 21.01 ! LGCIU 1 (5GA1) / FDIMU (10TV)! LGCIU 1 ! 323171 ! Extern III !
! 21.02 ! LGCIU 2 (5GA2) / FDIMU (10TV)! LGCIU 2 ! 323171 ! Extern III !
! 22.01 ! SDAC 1 (1WV1) / FDIMU (10TV) ! SDAC 1 ! 315534 ! Extern III !
! 22.02 ! SDAC 2 (1WV2) / FDIMU (10TV) ! SDAC 2 ! 315534 ! Extern III !
! 23.01 ! SFCC 1 (21CV) / FDIMU (10TV) ! SFCC 1 ! 275134 ! Extern III !
! 23.02 ! SFCC 2 (22CV) / FDIMU (10TV) ! SFCC 2 ! 275134 ! Extern III !
! 24.01 ! BSCU 1 (10GG) / FDIMU (10TV) ! BSCU 1 ! 324234 ! Extern III !
! 24.02 ! BSCU 2 (10GG) / FDIMU (10TV) ! BSCU 2 ! 324234 ! Extern III !
! 26.01 ! ACSC1 (47HH) / FDIMU (10TV) ! ACSC1 ! 216134 ! Extern III !
! ! ! ZONE CNTR! ! !
! ! ! PACK CNTR! ! !
! 26.02 ! ACSC2 (57HH) / FDIMU (10TV) ! ACSC2 ! 216134 ! Extern III !
! ! ! ZONE CNTR! ! !
! ! ! PACK CNTR! ! !
! 27.01(1)! ECU 1 (4000KS) / FDIMU (10TV)! ECU ENG1 ! 732160 ! Extern III !
! (2)! EEC 1 (4000KS) / FDIMU (10TV)! EEC ENG1 ! 732234 ! Extern III !
! 27.02(1)! ECU 2 (4000KS) / FDIMU (10TV)! ECU ENG2 ! 732160 ! Extern III !
! (2)! EEC 2 (4000KS) / FDIMU (10TV)! EEC ENG2 ! 732234 ! Extern III !
+-----------------------------------------------------------------------------+
(1) For CFM-egines, (2) for IAE-engines

+-----------------------------------------------------------------------------+
! Message ! Failure Message Text ! Source ! Chapter ! Failure Class !
! No ! ! ! ! !
!---------!------------------------------!----------!---------!---------------!
! 1.00 ! Power Supply Interrupt ! FDIMU ! 240000 ! Extern I !
! 1.01 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern II !
! 1.04 ! DAR (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.05 ! DAR MEDIA LOW (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.06 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.07 ! FDIMU Battery (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.08 ! FDIMU PCMCIA MEDIA (10TV) ! FDIMU ! 313634 ! Intern II !
! 2.00 ! ATSU1 (1TX1) / FDIMU (10TV) ! ATSU ! 462134 ! Extern III !
! 3.00 ! CFDIU (1TW1) / FDIMU (10TV) ! CFDIU ! 451334 ! Extern III !
! 4.01 ! MCDU 1 (3CA1) / FDIMU (10TV) ! MCDU 1 ! 228212 ! Extern III !
! 4.02 ! MCDU 2 (3CA2) / FDIMU (10TV) ! MCDU 2 ! 228212 ! Extern III !
! 6.00 ! PRINTER (4TW) / FDIMU (10TV) ! Printer ! 313522 ! Extern III !
! 7.01 ! ADIRU 1 (1EP1) / FDIMU (10TV)! ADIRU 1 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.02 ! ADIRU 2 (1EP2) / FDIMU (10TV)! ADIRU 2 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.03 ! ADIRU 3 (1EP3) / FDIMU (10TV)! ADIRU 3 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 8.01 ! BMC 1 (1HA1) / FDIMU (10TV) ! BMC 1 ! 361134 ! Extern III !
! 8.02 ! BMC 2 (1HA2) / FDIMU (10TV) ! BMC 2 ! 361134 ! Extern III !
! 9.00 ! FQIC (3QT) / FDIMU (10TV) ! FQIC ! 284234 ! Extern III !
! 10.01 ! CPC 1 (11HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 1 ! ! !
! 10.02 ! CPC 2 (12HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 2 ! ! !
! 11.01 ! DMC 1 (1WT1) / FDIMU (10TV) ! DMC 1 ! 316334 ! Extern III !
! 11.02 ! DMC 2 (1WT2) / FDIMU (10TV) ! DMC 2 ! 316334 ! Extern III !
! 12.00 ! ECB (59KD) / FDIMU (10TV) ! APU ECB ! 496134 ! Extern III !
! 13.00 ! EVMU (2EV) / FDIMU (10TV) ! EVMU ! 773234 ! Extern III !
! 14.01 ! FCDC 1 (3CE1) / FDIMU (10TV) ! FCDC 1 ! 279534 ! Extern III !
! 14.02 ! FCDC 2 (3CE2) / FDIMU (10TV) ! FCDC 2 ! 279534 ! Extern III !
! 15.01 ! FAC 1 (1CC1) / FDIMU (10TV) ! FAC 1 ! 226634 ! Extern III !
! 15.02 ! FAC 2 (1CC2) / FDIMU (10TV) ! FAC 2 ! 226634 ! Extern III !
! 16.00 ! FCU (2CA) / FDIMU (10TV) ! FCU A, B ! 228112 ! Extern III !
! 17.00 ! FDIU (10TV) / FDIMU (10TV) ! FDIMU ! 313634 ! Extern III !
! 18.01 ! FMGC 1 (1CA1) / FDIMU (10TV) ! FMGC 1 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 18.02 ! FMGC 2 (1CA2) / FDIMU (10TV) ! FMGC 2 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 19.01 ! FWC 1 (1WW1) / FDIMU (10TV) ! FWC 1 ! 315334 ! Extern III !
! 19.02 ! FWC 2 (1WW2) / FDIMU (10TV) ! FWC 2 ! 315334 ! Extern III !
! 20.00 ! GPWC (1WZ) / FDIMU (10TV) ! GPWC ! 344834 ! Extern III !
! 21.01 ! LGCIU 1 (5GA1) / FDIMU (10TV)! LGCIU 1 ! 323171 ! Extern III !
! 21.02 ! LGCIU 2 (5GA2) / FDIMU (10TV)! LGCIU 2 ! 323171 ! Extern III !
! 22.01 ! SDAC 1 (1WV1) / FDIMU (10TV) ! SDAC 1 ! 315534 ! Extern III !
! 22.02 ! SDAC 2 (1WV2) / FDIMU (10TV) ! SDAC 2 ! 315534 ! Extern III !
! 23.01 ! SFCC 1 (21CV) / FDIMU (10TV) ! SFCC 1 ! 275134 ! Extern III !
! 23.02 ! SFCC 2 (22CV) / FDIMU (10TV) ! SFCC 2 ! 275134 ! Extern III !
! 24.01 ! BSCU 1 (10GG) / FDIMU (10TV) ! BSCU 1 ! 324234 ! Extern III !
! 24.02 ! BSCU 2 (10GG) / FDIMU (10TV) ! BSCU 2 ! 324234 ! Extern III !
! 25.00(A)! ZC (8HK) / FDIMU (10TV) ! Zone CNTR! 216334 ! Extern III !
! 26.01(A)! Pack (7HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 1 ! ! !
! 26.02(A)! Pack (27HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 2 ! ! !
! 26.01(B)! ACSC 1 (47HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 26.02(B)! ACSC 2 (57HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 27.01(1)! ECU 1 (4000) / FDIMU (10TV) ! ECU ENG1 ! 732160 ! Extern III !
! (2)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732234 ! Extern III !
! (3)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 27.02(1)! ECU 2 (4000) / FDIMU (10TV) ! ECU ENG2 ! 732160 ! Extern III !
! (2)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG2 ! 732234 ! Extern III !
! (3)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 29.00 ! ANSU DISK FULL ! ANSU ! 461100 ! Extern III !
! 30.00 ! ANSU (3TL) / FDIMU (10TV) ! ANSU ! 461135 ! Extern III !
! 31.01 ! HUDC 1 (11FH1) / FDIMU (10TV)! HUDC1 ! 343534 ! Extern III !
! 31.02 ! HUDC 2 (11FH2) / FDIMU (10TV)! HUDC2 ! 343534 ! Extern III !
!-----------------------------------------------------------------------------!
! (1) For CFM-engines, (2) for IAE-engines, (3) P&W-engines. !
! (A) Zone- and Pack Controller Configuration. !
! (B) ACSC Configuration. !
+-----------------------------------------------------------------------------+

+-----------------------------------------------------------------------------+
! Message ! Failure Message Text ! Source ! Chapter ! Failure Class !
! No ! ! ! ! !
!---------!------------------------------!----------!---------!---------------!
! 1.00 ! Power Supply Interrupt ! FDIMU ! 240000 ! Extern I !
! 1.01 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern II !
! 1.04 ! DAR (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.05 ! DAR MEDIA LOW (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.06 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.07 ! FDIMU Battery (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.08 ! FDIMU PCMCIA MEDIA (10TV) ! FDIMU ! 313634 ! Intern II !
! 2.00 ! ATSU1 (1TX1) / FDIMU (10TV) ! ATSU ! 462134 ! Extern III !
! 3.00 ! CFDIU (1TW1) / FDIMU (10TV) ! CFDIU ! 451334 ! Extern III !
! 4.01 ! MCDU 1 (3CA1) / FDIMU (10TV) ! MCDU 1 ! 228212 ! Extern III !
! 4.02 ! MCDU 2 (3CA2) / FDIMU (10TV) ! MCDU 2 ! 228212 ! Extern III !
! 5.00 ! MDDU (1TD) / FDIMU (10TV) ! MDDU ! 452334 ! Extern III !
! 6.00 ! PRINTER (4TW) / FDIMU (10TV) ! Printer ! 313522 ! Extern III !
! 7.01 ! ADIRU 1 (1EP1) / FDIMU (10TV)! ADIRU 1 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.02 ! ADIRU 2 (1EP2) / FDIMU (10TV)! ADIRU 2 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.03 ! ADIRU 3 (1EP3) / FDIMU (10TV)! ADIRU 3 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 8.01 ! BMC 1 (1HA1) / FDIMU (10TV) ! BMC 1 ! 361134 ! Extern III !
! 8.02 ! BMC 2 (1HA2) / FDIMU (10TV) ! BMC 2 ! 361134 ! Extern III !
! 9.00 ! FQIC (3QT) / FDIMU (10TV) ! FQIC ! 284234 ! Extern III !
! 10.01 ! CPC 1 (11HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 1 ! ! !
! 10.02 ! CPC 2 (12HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 2 ! ! !
! 11.01 ! DMC 1 (1WT1) / FDIMU (10TV) ! DMC 1 ! 316334 ! Extern III !
! 11.02 ! DMC 2 (1WT2) / FDIMU (10TV) ! DMC 2 ! 316334 ! Extern III !
! 12.00 ! ECB (59KD) / FDIMU (10TV) ! APU ECB ! 496134 ! Extern III !
! 13.00 ! EVMU (2EV) / FDIMU (10TV) ! EVMU ! 773234 ! Extern III !
! 14.01 ! FCDC 1 (3CE1) / FDIMU (10TV) ! FCDC 1 ! 279534 ! Extern III !
! 14.02 ! FCDC 2 (3CE2) / FDIMU (10TV) ! FCDC 2 ! 279534 ! Extern III !
! 15.01 ! FAC 1 (1CC1) / FDIMU (10TV) ! FAC 1 ! 226634 ! Extern III !
! 15.02 ! FAC 2 (1CC2) / FDIMU (10TV) ! FAC 2 ! 226634 ! Extern III !
! 16.00 ! FCU (2CA) / FDIMU (10TV) ! FCU A, B ! 228112 ! Extern III !
! 17.00 ! FDIU (10TV) / FDIMU (10TV) ! FDIMU ! 313634 ! Extern III !
! 18.01 ! FMGC 1 (1CA1) / FDIMU (10TV) ! FMGC 1 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 18.02 ! FMGC 2 (1CA2) / FDIMU (10TV) ! FMGC 2 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 19.01 ! FWC 1 (1WW1) / FDIMU (10TV) ! FWC 1 ! 315334 ! Extern III !
! 19.02 ! FWC 2 (1WW2) / FDIMU (10TV) ! FWC 2 ! 315334 ! Extern III !
! 20.00 ! GPWC (1WZ) / FDIMU (10TV) ! GPWC ! 344834 ! Extern III !
! 21.01 ! LGCIU 1 (5GA1) / FDIMU (10TV)! LGCIU 1 ! 323171 ! Extern III !
! 21.02 ! LGCIU 2 (5GA2) / FDIMU (10TV)! LGCIU 2 ! 323171 ! Extern III !
! 22.01 ! SDAC 1 (1WV1) / FDIMU (10TV) ! SDAC 1 ! 315534 ! Extern III !
! 22.02 ! SDAC 2 (1WV2) / FDIMU (10TV) ! SDAC 2 ! 315534 ! Extern III !
! 23.01 ! SFCC 1 (21CV) / FDIMU (10TV) ! SFCC 1 ! 275134 ! Extern III !
! 23.02 ! SFCC 2 (22CV) / FDIMU (10TV) ! SFCC 2 ! 275134 ! Extern III !
! 24.01 ! BSCU 1 (10GG) / FDIMU (10TV) ! BSCU 1 ! 324234 ! Extern III !
! 24.02 ! BSCU 2 (10GG) / FDIMU (10TV) ! BSCU 2 ! 324234 ! Extern III !
! 25.00(A)! ZC (8HK) / FDIMU (10TV) ! Zone CNTR! 216334 ! Extern III !
! 26.01(A)! Pack (7HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 1 ! ! !
! 26.02(A)! Pack (27HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 2 ! ! !
! 26.01(B)! ACSC 1 (47HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 26.02(B)! ACSC 2 (57HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 27.01(1)! ECU 1 (4000) / FDIMU (10TV) ! ECU ENG1 ! 732160 ! Extern III !
! (2)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732234 ! Extern III !
! (3)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 27.02(1)! ECU 2 (4000) / FDIMU (10TV) ! ECU ENG2 ! 732160 ! Extern III !
! (2)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG2 ! 732234 ! Extern III !
! (3)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 29.00 ! ANSU DISK FULL ! ANSU ! 461100 ! Extern III !
! 30.00 ! ANSU (3TL) / FDIMU (10TV) ! ANSU ! 461135 ! Extern III !
! 31.01 ! HUDC 1 (11FH1) / FDIMU (10TV)! HUDC1 ! 343534 ! Extern III !
! 31.02 ! HUDC 2 (11FH2) / FDIMU (10TV)! HUDC2 ! 343534 ! Extern III !
!-----------------------------------------------------------------------------!
! (1) For CFM-engines, (2) for IAE-engines, (3) P&W-engines. !
! (A) Zone- and Pack Controller Configuration. !
! (B) ACSC Configuration. !
+-----------------------------------------------------------------------------+

+-----------------------------------------------------------------------------+
! Message ! Failure Message Text ! Source ! Chapter ! Failure Class !
! No ! ! ! ! !
!---------!------------------------------!----------!---------!---------------!
! 1.00 ! Power Supply Interrupt ! FDIMU ! 240000 ! Extern I !
! 1.01 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern II !
! 1.04 ! DAR (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.05 ! DAR MEDIA LOW (2TV) ! FDIMU ! 313652 ! Intern II !
! 1.06 ! FDIMU (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.07 ! FDIMU Battery (10TV) ! FDIMU ! 313634 ! Intern III !
! 1.08 ! FDIMU PCMCIA MEDIA (10TV) ! FDIMU ! 313634 ! Intern II !
! 2.00 ! ATSU1 (1TX1) / FDIMU (10TV) ! ATSU ! 462134 ! Extern III !
! 3.00 ! CFDIU (1TW1) / FDIMU (10TV) ! CFDIU ! 451334 ! Extern III !
! 4.01 ! MCDU 1 (3CA1) / FDIMU (10TV) ! MCDU 1 ! 228212 ! Extern III !
! 4.02 ! MCDU 2 (3CA2) / FDIMU (10TV) ! MCDU 2 ! 228212 ! Extern III !
! 5.00 ! MDDU (1TD) / FDIMU (10TV) ! MDDU ! 452334 ! Extern III !
! 6.00 ! PRINTER (4TW) / FDIMU (10TV) ! Printer ! 313522 ! Extern III !
! 7.01 ! ADIRU 1 (1EP1) / FDIMU (10TV)! ADIRU 1 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.02 ! ADIRU 2 (1EP2) / FDIMU (10TV)! ADIRU 2 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 7.03 ! ADIRU 3 (1EP3) / FDIMU (10TV)! ADIRU 3 ! 341234 ! Extern III !
! ! ! - ADC ! ! !
! ! ! - IRS ! ! !
! 8.01 ! BMC 1 (1HA1) / FDIMU (10TV) ! BMC 1 ! 361134 ! Extern III !
! 8.02 ! BMC 2 (1HA2) / FDIMU (10TV) ! BMC 2 ! 361134 ! Extern III !
! 9.00 ! FQIC (3QT) / FDIMU (10TV) ! FQIC ! 284234 ! Extern III !
! 10.01 ! CPC 1 (11HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 1 ! ! !
! 10.02 ! CPC 2 (12HL) / FDIMU (10TV) ! Pressure ! 213134 ! Extern III !
! ! ! Cntr 2 ! ! !
! 11.01 ! DMC 1 (1WT1) / FDIMU (10TV) ! DMC 1 ! 316334 ! Extern III !
! 11.02 ! DMC 2 (1WT2) / FDIMU (10TV) ! DMC 2 ! 316334 ! Extern III !
! 12.00 ! ECB (59KD) / FDIMU (10TV) ! APU ECB ! 496134 ! Extern III !
! 13.00 ! EVMU (2EV) / FDIMU (10TV) ! EVMU ! 773234 ! Extern III !
! 14.01 ! FCDC 1 (3CE1) / FDIMU (10TV) ! FCDC 1 ! 279534 ! Extern III !
! 14.02 ! FCDC 2 (3CE2) / FDIMU (10TV) ! FCDC 2 ! 279534 ! Extern III !
! 15.01 ! FAC 1 (1CC1) / FDIMU (10TV) ! FAC 1 ! 226634 ! Extern III !
! 15.02 ! FAC 2 (1CC2) / FDIMU (10TV) ! FAC 2 ! 226634 ! Extern III !
! 16.00 ! FCU (2CA) / FDIMU (10TV) ! FCU A, B ! 228112 ! Extern III !
! 17.00 ! FDIU (10TV) / FDIMU (10TV) ! FDIMU ! 313634 ! Extern III !
! 18.01 ! FMGC 1 (1CA1) / FDIMU (10TV) ! FMGC 1 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 18.02 ! FMGC 2 (1CA2) / FDIMU (10TV) ! FMGC 2 ! 228334 ! Extern III !
! ! ! - FMC ! ! !
! ! ! - FGC ! ! !
! 19.01 ! FWC 1 (1WW1) / FDIMU (10TV) ! FWC 1 ! 315334 ! Extern III !
! 19.02 ! FWC 2 (1WW2) / FDIMU (10TV) ! FWC 2 ! 315334 ! Extern III !
! 20.00 ! GPWC (1WZ) / FDIMU (10TV) ! GPWC ! 344834 ! Extern III !
! 21.01 ! LGCIU 1 (5GA1) / FDIMU (10TV)! LGCIU 1 ! 323171 ! Extern III !
! 21.02 ! LGCIU 2 (5GA2) / FDIMU (10TV)! LGCIU 2 ! 323171 ! Extern III !
! 22.01 ! SDAC 1 (1WV1) / FDIMU (10TV) ! SDAC 1 ! 315534 ! Extern III !
! 22.02 ! SDAC 2 (1WV2) / FDIMU (10TV) ! SDAC 2 ! 315534 ! Extern III !
! 23.01 ! SFCC 1 (21CV) / FDIMU (10TV) ! SFCC 1 ! 275134 ! Extern III !
! 23.02 ! SFCC 2 (22CV) / FDIMU (10TV) ! SFCC 2 ! 275134 ! Extern III !
! 24.01 ! BSCU 1 (10GG) / FDIMU (10TV) ! BSCU 1 ! 324234 ! Extern III !
! 24.02 ! BSCU 2 (10GG) / FDIMU (10TV) ! BSCU 2 ! 324234 ! Extern III !
! 25.00(A)! ZC (8HK) / FDIMU (10TV) ! Zone CNTR! 216334 ! Extern III !
! 26.01(A)! Pack (7HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 1 ! ! !
! 26.02(A)! Pack (27HH) / FDIMU (10TV) ! Pack CNTR! 216134 ! Extern III !
! ! ! LH 2 ! ! !
! 26.01(B)! ACSC 1 (47HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 26.02(B)! ACSC 2 (57HH) / FDIMU (10TV) !-ZONE CNTR! 216134 ! Extern III !
! ! !-PACK CNTR! ! !
! 27.01(1)! ECU 1 (4000) / FDIMU (10TV) ! ECU ENG1 ! 732160 ! Extern III !
! (2)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732234 ! Extern III !
! (3)! EEC 1 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 27.02(1)! ECU 2 (4000) / FDIMU (10TV) ! ECU ENG2 ! 732160 ! Extern III !
! (2)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG2 ! 732234 ! Extern III !
! (3)! EEC 2 (4000) / FDIMU (10TV) ! EEC ENG1 ! 732134 ! Extern III !
! 29.00 ! ANSU DISK FULL ! ANSU ! 461100 ! Extern III !
! 30.00 ! ANSU (3TL) / FDIMU (10TV) ! ANSU ! 461135 ! Extern III !
! 31.01 ! HUDC 1 (11FH1) / FDIMU (10TV)! HUDC1 ! 343534 ! Extern III !
! 31.02 ! HUDC 2 (11FH2) / FDIMU (10TV)! HUDC2 ! 343534 ! Extern III !
!-----------------------------------------------------------------------------!
! (1) For CFM-engines, (2) for IAE-engines, (3) P&W-engines. !
! (A) Zone- and Pack Controller Configuration. !
! (B) ACSC Configuration. !
+-----------------------------------------------------------------------------+

D. CFDS Menu Function
You can use the MCDU to show the failures that occurred during the last flight. The data comes from the CFDS (Ref. AMM D/O 31-32-00-00). You can also start system tests from the MCDU. To show the AIDS control data on the MCDU or to start a system test:
  • Push the line select key adjacent to 'CFDS' on MCDU Menu
  • Push the line select key adjacent to 'SYSTEM REPORT/TEST' CFDS Main Menu
  • Push the line select key adjacent to 'INST' on System Report/Test Menu
  • Push the line select key adjacent to '<DMU' to access to the AIDS Menu.
From the AIDS Menu, you can set:
  • <LAST LEG REPORT
  • <PREVIOUS LEGS REPORTS
  • <LRU IDENT
  • <GND SCANNING
  • <TROUBLE SHOOT DATA
  • <CLASS 3 FAULTS
  • <TEST
  • <GROUND REPORT
  • <SOFTWARE LOAD STATUS.
(1) <LAST LEG REPORT
F Last Leg Report ** ON A/C NOT FOR ALL
F CFDS - Last Leg Report ** ON A/C NOT FOR ALL
If you push the '<LAST LEG REPORT' LSK, the screen shows each class 1 and 2 failure found during the last flight leg with:
  • The time when the failure occurred
  • The ATA number of the component
  • The FIN of the component
  • The class of the failure.
The screen shows a maximum of two failures at a time. If there are more failures, push the next page key on the MCDU keyboard. If there are no failures, the display shows the 'NO FAULT DETECTED' message.
If you push the LSK adjacent to the failure class the screen shows the trouble shooting data for that failure.

(2) <PREVIOUS LEGS REPORT
F Previous Legs Reports ** ON A/C NOT FOR ALL
F CFDS - Previous Leg Report ** ON A/C NOT FOR ALL
If you push the '<PREVIOUS LEGS REPORT' LSK, the display shows each failure, that has not been corrected from previous reports with:
  • The aircraft tail number
  • The flight leg
  • The date of the applicable flight leg
  • The time the failure occurred
  • The ATA reference of the failure
  • The class of the failure
  • The FIN of the component.
The display shows a maximum of two failures at a time. If there are more failures, push the next page key on the MCDU keyboard. If there are no failures, the display shows the message NO FAULT DETECTED.
In case of an aircraft tailnumber change (e.g. the FDIMU was moved to a different aircraft - internal fault messages are not cleared) the fault messages with different tail number are displayed on the next pages.
If you push the LSK adjacent to the failure class the display shows the trouble shooting data for the failure.

(3) <LRU IDENT
F CFDS - LRU Identification ** ON A/C NOT FOR ALL
F CFDS - LRU Identification ** ON A/C NOT FOR ALL
If you push the '<LRU IDENT' LSK, the display shows the applicable LRU identification with:
  • The name of the LRU (FDIMU)
  • The LRU hardware part number
  • The LRU serial number
  • The software part number.

(4) <GND SCANNING
F Ground Scanning ** ON A/C NOT FOR ALL
F CFDS - Ground Scanning Report ** ON A/C NOT FOR ALL
If you push the '<GND SCANNING' LSK, the display shows the GND SCAN IN PROGRESS legend. If there are failures in the system the screen shows:
  • The time when the failure occurred
  • The ATA reference of the failure
  • The class of the failure
  • The FIN of the component.
The display shows a maximum of two failures at a time. If there are more failures, push the next page key on the MCDU keyboard. If there are no failures, the display shows the message NO FAULT DETECTED.
If you set the <RETURN function key the system deletes all the recorded failures.
If you push the failure class LSK the screen shows the trouble shooting data for the failure.

(5) <TROUBLE SHOOT DATA
F CFDS - Trouble Shooting Data Menu ** ON A/C NOT FOR ALL
F CFDS - Trouble Shooting Data Menu ** ON A/C NOT FOR ALL
If you push the '<TROUBLE SHOOT DATA' LSK, the screen shows:
  • The date when the failure occurred
  • The time when the failure occurred
  • The failure type
  • The failure class
  • The count of failure occurrence
  • The failure message
  • The port number
  • The bus name
  • The equipment code
  • The system number.
If there are no trouble shooting data, the display shows 'NO TROUBLESHOOTING DATA AVAILABLE'

(6) <CLASS 3 FAULTS
F CFDS - Last Leg Class 3 Faults ** ON A/C NOT FOR ALL
F CFDS - Last Leg Class 3 Faults ** ON A/C NOT FOR ALL
If you push the '<CLASS 3 FAULTS' LSK, the display shows each class 3 failure found during the last flight leg with:
  • The time when the failure occurred
  • The ATA reference of the failure
  • The FIN of the component
  • The failure message.
If you push the LSK adjacent to the failure the display shows the trouble shooting data for the failure.
The display shows a maximum of two failures at a time. If there more failures, push the next page key on the MCDU keyboard. If there are no failures, the display shows the message NO FAULT DETECTED.

(7) <TEST
F Test Menu ** ON A/C NOT FOR ALL
F CFDS - Test Menus ** ON A/C NOT FOR ALL
If you push the '<TEST' LSK the display shows:
  • <AIDS TEST
  • <FDIMU BATTERY TEST.
(a) <AIDS TEST
If you push the '<AIDS TEST' LSK the FDIMU initiates a complete BITE procedure.
If the test is longer than 1 second, the display shows TEST IN PROGRSS xxS (x= approximate maximum waiting time in seconds).
If the system has no failures the display shows TEST OK.
If faults are found, the test result menu shows the faulty LRU with:
  • The ATA reference of the failure
  • The FIN of the component
  • The class of the failure
  • The failure message.
If you push the LSK adjacent to the failure class the display shows the trouble shooting data for the failure.

(b) <FDIMU BATTERY TEST
If you push the '<FDIMU DMU BATTERY TEST' LSK the FDIMU initiate a battery test which does not interfere with the normal FDIMU operation.
If the test is longer than 1 second, the screen shows the TEST IN PROGRSS xS (x= approximate maximum waiting time in seconds).
If the system has no failures the display shows BATTERIES OK.
If faults are found, the test result menu shows the faulty LRU with:
  • The ATA reference of the failure
  • The FIN of the component
  • The class of the failure
  • The failure message.
If you push the LSK adjacent to the failure class the display shows the trouble shooting data for the failure.

(8) <GROUND REPORT
F CFDS - Ground Report ** ON A/C NOT FOR ALL
If you push the '<GROUND REPORT' LSK, the display shows each internal failure during the last flight leg with:
  • The time when the failure occurred
  • The ATA reference of the failure
  • The FIN of the component
  • The class of the failure.
The display shows a maximum of two failures at a time. If there are more failures, push the next page key on the MCDU keyboard. If there are no failures, the display shows the message NO FAULT DETECTED.
If you push the LSK adjacent to the failure class, the display shows the trouble shooting data for the failure.

(9) <SOFTWARE LOAD STATUS
F Software Load Status ** ON A/C NOT FOR ALL
F CFDS - Software Load Status ** ON A/C NOT FOR ALL
If you push the '<SOFTWARE LOAD STATUS' LSK, the display shows:
  • The system software part number
  • The date when the system software was loaded
  • The combined setup database/customer version part number
  • The date when the combined setup database/customer software was loaded.
If the software loading was unsuccessful the screen shows SOFTWARE LOAD ERROR.
E. Wireless Function
(1) General Description
The wireless function for the AIDS system supplies an end to end solution for the maintenance data wireless transfer.
Data generated by the AIDS and stored on the PCMCIA memory card are transmitted.
These types of data are as follow:
  • Report-data
  • DAR-data
  • SAR-data
  • QAR-data
(2) Hardware
The name of this PCMCIA card is SPC (Smart PCMCIA Card).
The wireless communication uses the Cellular Technology.
(3) Software
The Ground Server Application (GSA), used for the configuration of the SPC, makes it possible to configure the transmission function.
You can configure these different functions:
(a) Types of data to transmit:
  • Report-data
  • DAR-data
  • SAR-data
  • QAR-data.
(b) Connection data.
(4) SPC - Functionality
The wireless communication uses the Cellular Technology and supply these protocols:
  • HSDPA (3G+)
  • UMTS (3G)
  • GPRS (2.5G)
  • GSM (2G).
F. FDIMU Wireless Extention for AIDS (WEFA) Ready
(1) General
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
The Wireless Extension For AIDS is a system made of 4 main elements:
  • a WEFA ready unit,
  • a Smart PCMCIA Card (called SPC) plugged in the PCMCIA interface.

    The WEFA ready unit is fully compatible with FDIMU ED48A200.

    All the requirements applicable for FDIMU ED48A100/ED48A200 are also applicable for the WEFA ready unit.

    The WEFA ready unit permits a wireless connection to the SPC through the PCMCIA connector.
    The WEFA ready unit hosts the SPC in the PCMCIA slot.
    If there is no SPC inserted, the WEFA ready unit will operate the same as ED48A200.
    If there is a standard PCMCIA storage card (solid state flash card) inserted to the PCMCIA slot, the WEFA ready unit operates correctly.
    When the transmission of data by the WEFA function is not enabled, the storage function of the standard PCMCIA interface is available, regardless if a SPC or a standard PCMCIA storage card is inserted into the WEFA ready unit.
(2) Mechanical characteristics for the WEFA ready unit
F Flight Data Interface and Management Unit (FDIMU) ** ON A/C NOT FOR ALL
The front panel of the WEFA ready unit keeps the optic conductors of the ED48A200 which shows the ED48 Monitoring LEDs.

The front panel and the cover allows the presence of an SPC in a WEFA ready unit without disrespecting the ARINC600 standard.
The cover of the WEFA ready unit front-panel for the SPC is transparent in order to see the LEDs on the SPC.
The WEFA ready unit uses the following listed discrete for the interlock mechanism of wireless data transmission through SPC.
+--------------------------------------------+
! Discrete input ! Discrete type ! ACU !
!----------------!-----------------!---------!
! MP 14E ! ARINC 717 shunt ! WEFA1 !
!----------------!-----------------!---------!
! TP 14H ! ARINC 717 shunt ! WEFA2 !
!----------------!-----------------!---------!
! MP 14G ! ARINC 717 shunt ! WEFA3 !
+--------------------------------------------+

NOTE: WEFA1 is connected to the Engine signal.
WEFA2 is connected to the Engine Master Lever 2 signal.
WEFA3 is connected to the Doors signal.
G. Smart PCMCIA Card (SPC)
(1) Mechanical characteristics for the SPC
F Smart PCMCIA Card (SPC) ** ON A/C NOT FOR ALL
  • The SPC is mechanically compatible with a PCMCIA slot type III.
  • The SPC is hosted in the PCMCIA slot of the FDIMU.
  • The SPC is fully compatible with the AIDS PCMCIA connector.
  • The PCMCIA connector is the only connection between the SPC and the FDIMU.
  • The antenna for wireless transmission is part of the SPC.
(2) Functional characteristics for the SPC
F Smart PCMCIA Card (SPC) ** ON A/C NOT FOR ALL
The SPC puts together two functions:
  • The storage function (solid state flash card)
  • The wireless transmission of data.
The SPC gives a minimum storage capacity of 2 GByte for AIDS data storage.
The FDIMU access to the memory of the SPC is also possible when the interlock mechanism operates.
The SPC automatically transmits only data, which was not already transmitted before.
In case the solid state memory of the SPC is 100% occupied, there is a 'wrap-around' for the data.
All interchange (information, power) between FDIMU and SPC (for WEFA and NON-WEFA functions) are done through the PCMCIA connector only.
H. AIDS WEFA Menu
(1) WEFA Maintenance Menu
F AIDS - WEFA Maintenance Menu ** ON A/C NOT FOR ALL
(a) ENABLED>
If the status of the WEFA is enabled or disabled, each time the <MAINTENANCE LSK is pushed, the submenu AIDS WEFA MAINTENANCE (ENABLED) or AIDS WEFA MAINTENANCE (DISABLED) comes into view.
1 <*MANUAL TRIGGER
Each time the <*MANUAL TRIGGER LSK is pushed, a WEFA Report is generated. The report code is related to a manual request.
The '*' is removed during the report generation.
This key becomes available only when the WEFA status is 'ENABLED'.
NOTE: Only the storage of the report with the code 1000 is possible, but no printing.
(b) ENABLED*>
Each time the ENABLED*> LSK is pushed, the status of the WEFA function changes (Enabled or Disabled).
This status is stored in NVRAM (by default, after a first installation or a new installation of the AIDS SW, the WEFA function is ENABLED). This WEFA activation is memorized in the AIDS non volatile memory. The SPC card removal or new installation has no effect on this activation, but without the SPC card, the display status is 'DISABLED'.
A password controls the access to this key.
The possible types of wireless status are:
  • <SIM: OK / CARD MISSING / CARD LOCKED
  • <NETWORK: NOT CONNECTED / CONNECTED(2G) / CONNECTED(3G)
  • <TRANSFER: INACTIVE / IN PROGRESS / SW ERROR / HW ERROR.
    If the WEFA interlock does not enable the WEFA transmission, the status for SIM, NETWORK and TRANSFER will be displayed with '-' (dash).
(c) DISABLED*>
Each time the DISABLED*> LSK is pushed, the status of the WEFA function changes (Enabled or Disabled). This status is stored in NVRAM (by default, after a first installation or a new installation of the AIDS SW, the WEFA function is ENABLED). This WEFA activation is memorized in the AIDS non volatile memory. The SPC card removal or new installation has no effect on this activation, but without the SPC card, the display status is 'DISABLED'.
A password controls the access to this key.
(2) WEFA Status Menu
F AIDS - WEFA Status Menu ** ON A/C NOT FOR ALL
(a) AIDS WEFA STATUS page 1/2

<WEFA1, <WEFA2, <WEFA3 give the position of the aircraft inhibition discretes. The status ON/OFF means: ON = active, OFF = Grounded.
<ENABLE1 and <ENABLE2: the redundant enable outputs of the ED48 mezzanine board. Possible states are ON/OFF: ON = enabled.
<MEZZ STATE: the ED48 mezzanine computed XXX: the ENABLE output are coherent with the WEFA discrete inputs. In addition, if the fail safe fuse of the SPC is burned, this status will be also set (the mezzanine is supposed to be the reason of the fuse burn). States OK/FAIL.

(b) AIDS WEFA STATUS page 2/2

<WEFA1, <WEFA2, <WEFA3 give the position of the aircraft inhibition discretes The status ON/OFF means: ON = active, OFF = Grounded.
<RF PWR Input shows the presence of the SPC input POWER for wireless function.
<SAFE PWR OUT: shows the state of the fail safe circuit, including the protection fuse.
<RF POWER OUT: power applied to wireless module.
<SPC STATE: shows failure of the SPC, including the wireless interlock.
(3) WEFA SPC STATUS
F AIDS - WEFA SPC Status ** ON A/C NOT FOR ALL
<SPC STATUS gives access to some detailed characteristics about the SPC.
RES SW PN: Resident version implemented on the SPC.
APP SW PN: Software version implemented on the SPC.
BYTE0, BYTE1, BYTE2:
GSM RSSI LEVEL: Level of network reception.
GSM MOD TEMP: Temperature of the GSM module.
[Rev.10 from 2021] 2026.04.01 00:35:18 UTC
"Aviabrain" 2025