AIDS INPUT INTERFACE - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The parameter set sampled by the DMU contains parameters used for condition monitoring. All other parameters from the connected system busses are also sampled.
The parameter set sampled by the FDIMU (DMU-Part) contains parameters used for condition monitoring. All other parameters from the connected system busses are also sampled.
** ON A/C NOT FOR ALL The parameter set sampled by the DMU contains parameters used for condition monitoring. All other parameters from the connected system busses are also sampled.
The parameter set sampled by the FDIMU (DMU-Part) contains parameters used for condition monitoring. All other parameters from the connected system busses are also sampled.
2. System description
A. Architecture of Inputs
FDIMU (DMU-Part) Source Block Diagram
DMU Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
The FDIMU (DMU-Part) is connected to various source systems to collect the whole parameter set. The block diagram of input sources shows the connection
of the FDIMU (DMU-Part) to the respective sources.
FDIMU (DMU-Part) Source Block Diagram
DMU Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL
FDIMU (DMU-Part) Source Block Diagram (sheet 1/2) ** ON A/C NOT FOR ALL of the FDIMU (DMU-Part) to the respective sources.
(1) Power Supply of Input Sources
All parameter source systems are supplied by their own system power supplies.
All parameter source systems are supplied by their own system power supplies.
B. DMU Input Parameters
All DMU parameters are listed in the parameters list. The DMU uses these parameters to perform the various functions. Also the DMU internal parameters and parameters on Output Bus A+B and listed in the parameters list. For all calculations, logical decisions and parameters to be included in a print report only valid parameters are used. If there is no valid parameter available, the corresponding parameter column is filled with '<'.
If a parameter, which is defined to be included in a print report, is not transmitted on the appropriate 'ARINC' bus, the corresponding data field is filled with '>'. If a parameter, which is used for a logical decision, is invalid or not transmitted during the whole flight phase, (in which it is intended to be used), this causes a class 3 fault. For average calculations valid parameters only are used. The validity of a parameter is detected by monitoring the SSM bits. Also the parity bit of the appropriate ARINC 429 word. If a parameter fail is detected, the alternative system 2 parameter is used if possible. If an alternative parameter is used, this is indicated by an associated to the parameter number, for all the various functional descriptions.
If a parameter which is used for logics is invalid or not transmitted, or an alternative parameter is not available, the previous good value is used for up to three reads. After three consecutive reads this parameter is marked as failed and the logic is not performed.
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", ...).
Means are provided to observe also those busses which are not permanently used for the logics or reports.
All DMU parameters are listed in the parameters list. The DMU uses these parameters to perform the various functions. Also the DMU internal parameters and parameters on Output Bus A+B and listed in the parameters list. For all calculations, logical decisions and parameters to be included in a print report only valid parameters are used. If there is no valid parameter available, the corresponding parameter column is filled with '<'.
If a parameter, which is defined to be included in a print report, is not transmitted on the appropriate 'ARINC' bus, the corresponding data field is filled with '>'. If a parameter, which is used for a logical decision, is invalid or not transmitted during the whole flight phase, (in which it is intended to be used), this causes a class 3 fault. For average calculations valid parameters only are used. The validity of a parameter is detected by monitoring the SSM bits. Also the parity bit of the appropriate ARINC 429 word. If a parameter fail is detected, the alternative system 2 parameter is used if possible. If an alternative parameter is used, this is indicated by an associated to the parameter number, for all the various functional descriptions.
If a parameter which is used for logics is invalid or not transmitted, or an alternative parameter is not available, the previous good value is used for up to three reads. After three consecutive reads this parameter is marked as failed and the logic is not performed.
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", ...).
Means are provided to observe also those busses which are not permanently used for the logics or reports.
C. FDIMU (DMU-part) Input Parameters
All FDIMU (DMU-part) parameters are listed in the parameters list. The FDIMU uses these parameters to do various functions. Also the FDIMU internal parameters and parameters on Output Bus A+B and listed in the parameters list. For all calculations, logical decisions and parameters to be included in a print report only valid parameters are used. If there is no valid parameter available, the related parameter column is filled with '<'.
If a parameter, which is specified to be included in a print report, is not transmitted on the appropriate 'ARINC' bus, the related data field is filled with '>'. If a parameter, which is used for a logical decision, is invalid or not transmitted during the whole flight phase, (in which it is intended to be used), this causes a class 3 fault. For average calculations valid parameters only are used. The validity of a parameter is detected by monitoring the SSM bits. Also the parity bit of the appropriate ARINC 429 word. If a parameter fail is detected, the alternative system 2 parameter is used if possible. If an alternative parameter is used, this is shown by an associated to the parameter number, for all the various functional descriptions.
If a parameter which is used for logics is invalid or not transmitted, or an alternative parameter is not available, the previous good value is used for up to three reads. After three consecutive reads this parameter is marked as failed and the logic is not performed.
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 which shows "not Normal Operation", then t parameter is marked with dashes ("---").
If the length of the parameter is too large (overflow) the display field show Es. The possible length of parameters is between one and six characters (for example: "E", "EE", ...).
Means are provided to observe also those busses which are not permanently used for the logics or reports.
All FDIMU (DMU-part) parameters are listed in the parameters list. The FDIMU uses these parameters to do various functions. Also the FDIMU internal parameters and parameters on Output Bus A+B and listed in the parameters list. For all calculations, logical decisions and parameters to be included in a print report only valid parameters are used. If there is no valid parameter available, the related parameter column is filled with '<'.
If a parameter, which is specified to be included in a print report, is not transmitted on the appropriate 'ARINC' bus, the related data field is filled with '>'. If a parameter, which is used for a logical decision, is invalid or not transmitted during the whole flight phase, (in which it is intended to be used), this causes a class 3 fault. For average calculations valid parameters only are used. The validity of a parameter is detected by monitoring the SSM bits. Also the parity bit of the appropriate ARINC 429 word. If a parameter fail is detected, the alternative system 2 parameter is used if possible. If an alternative parameter is used, this is shown by an associated to the parameter number, for all the various functional descriptions.
If a parameter which is used for logics is invalid or not transmitted, or an alternative parameter is not available, the previous good value is used for up to three reads. After three consecutive reads this parameter is marked as failed and the logic is not performed.
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 which shows "not Normal Operation", then t parameter is marked with dashes ("---").
If the length of the parameter is too large (overflow) the display field show Es. The possible length of parameters is between one and six characters (for example: "E", "EE", ...).
Means are provided to observe also those busses which are not permanently used for the logics or reports.
D. Procedure for the Fuel Flow Parameter
The parameter FF (7C/1/244/01 for eng 1 and 7C/2/244/10 for eng 2) is marked as failed after 10 consecutive reads of no or not valid data.
Up to this moment the previous good value is used for the logics and the reports.
The parameter FF (7C/1/244/01 for eng 1 and 7C/2/244/10 for eng 2) is marked as failed after 10 consecutive reads of no or not valid data.
Up to this moment the previous good value is used for the logics and the reports.
E. Explanations to the Parameter List
The parameter list is organized refered to the connected ARINC 429 data buses.
The connected systems (e.g. FAC, ECU, EEC, etc.) and the related ATA chapter numbers are stated in the header on the left side of each page of the parameter lists.
The columns are described as follows:
The columns are described as follows:
The columns are described as follows:
The columns are described as follows:
The columns are described as follows:
The columns are described as follows:
The parameter list is organized refered to the connected ARINC 429 data buses.
The connected systems (e.g. FAC, ECU, EEC, etc.) and the related ATA chapter numbers are stated in the header on the left side of each page of the parameter lists.
The columns are described as follows:
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 1st ! EQ/SYS/LAB/SDI = Parameter number |
| SYS/LAB/SDI ! |
| ! System number: According to the system which is |
| ! sending out the corresponding parameter: |
| ! 1 for system one |
| ! 2 for system two |
| ! 3 for system three |
| ! Label of the parameter, octal value |
| ! according to ARINC 429. |
| ! SDI states the Source/Destination Identifier |
| ! which is used by the system for the |
| ! corresponding parameter: |
| ! 00 means SDI 00 (0) |
| ! 01 means SDI 01 (1) |
| ! 10 means SDI 10 (2) |
| ! 11 means SDI 11 (3) |
| -------------------!------------------------------------------------ |
| 2nd ! PARAMETER |
| PARAMETER ! Parameter Name |
| -------------------!------------------------------------------------ |
| 3rd ! RANGE |
| RANGE ! |
| ! Three different types of ranges are shown in |
| ! this column: |
| ! The first one, indicated by a 'W' (WORDRANGE), |
| ! is related to the ARINC 429 data bus. This |
| ! shows the maximum value of the parameter that |
| ! can be transferred on the bus. This |
| ! depends on the number of data bits (see |
| ! column DATA BITS) and the resolution ('R') of |
| ! the parameter (see column ACCURACY). |
| ! The second one, with no specific indication, |
| ! shows the normal operational range of the |
| ! parameter. |
| ! The third one is related to the ARINC 429 |
| ! Discrete Data Words. There are two states: |
| ! 'bit status 0' or 'bit status 1'. They |
| ! indicate the true condition of the |
| ! corresponding data word bit position. |
The columns are described as follows:
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 1st ! can contain 'U' or 'D' |
| ! 'U' means: used for AIDS |
| ! 'D' means: used for DAR STANDARD FRAME |
| -------------------------------------------------------------------- |
| 2nd ! EQ/SYS/LAB/SDI = Parameternumber |
| EQ/SYS/LAB/SDI ! |
| ! EQuipment identifier for the connected bus; |
| ! hexadecimal value according to ARINC 429. |
| ! |
| ! SYStem number: According to the system which is |
| ! sending out the corresponding parameter: |
| ! 1 for system one |
| ! 2 for system two |
| ! 3 for system three |
| ! |
| ! LABel of the parameter, octal value |
| ! according to ARINC 429. |
| ! |
| ! SDI states the Source/Destination Identifier |
| ! which is used by the system for the |
| ! corresponding parameter: |
| ! 00 means SDI 00 (0) |
| ! 01 means SDI 01 (1) |
| ! 10 means SDI 10 (2) |
| ! 11 means SDI 11 (3) |
| -------------------!------------------------------------------------ |
| 3rd ! PARAMETER |
| PARAMETER ! Parameter Name |
| -------------------!------------------------------------------------ |
| 4th ! RANGE |
| RANGE ! |
| ! Three different types of ranges are shown in |
| ! this column: |
| ! |
| ! The first one, indicated by a 'W' (WORDRANGE), |
| ! is related to the ARINC 429 data bus. It |
| ! shows the maximum value of the parameter that |
| ! can be transferred on the bus. This |
| ! depends on the number of data bits (see |
| ! column DATA BITS) and the resolution ('R') of |
| ! the parameter (see column ACCURACY). |
| ! |
| ! The second one, with no specific indication, |
| ! shows the normal operational range of the |
| ! parameter. |
| ! |
| ! The third one is related to the ARINC 429 |
| ! Discrete Data Words. There are two states: |
| ! 'bit status 0' or 'bit status 1'. |
| ! They indicate the true condition of the |
| ! corresponding data word bit position. |
The columns are described as follows:
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 1st ! |
| EQ/SYS/LAB/SDI ! EQuipment identifier for the connected bus; |
| ! hexadecimal value according to ARINC 429. |
| ! |
| ! SYStem number: According to the system which is |
| ! sending out the corresponding parameter: |
| ! 1 for system one |
| ! 2 for system two |
| ! 3 for system three |
| ! |
| ! LABel of the parameter, octal value according |
| ! to ARINC 429. |
| ! |
| ! SDI gives the Source/Destination Identifier |
| ! which is used by the system for the |
| ! corresponding parameter: |
| ! 00 means SDI 00 (0) |
| ! 01 means SDI 01 (1) |
| ! 10 means SDI 10 (2) |
| ! 11 means SDI 11 (3) |
| -------------------!------------------------------------------------ |
| 2nd ! CODE |
| CODE ! |
| ! BNR = binary data word |
| ! BCD = binary coded decimal data word |
| ! ISO = data word coded in ISO 5 code |
| ! DIS = discrete data word |
| ! HEX = hexadecimal coded |
| ! OCT = octal coded |
| ! HYB = mixed code: |
| ! e.g. bit 11 to 16 DIS |
| ! bit 17 to 28 BNR |
| -------------------!------------------------------------------------ |
| 3rd ! UPD/msec |
| UPD/msec ! |
| ! This column shows how many times the parameter |
| ! is transmitted by the source system. |
The columns are described as follows:
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 1st ! Alpha Call-Up |
| Alpha Call-Up ! |
| ! This column shows the mnemonic for the |
| ! related parameter. |
| ! If you enter this code in the MCDU, the MCDU |
| ! display shows the current parameter value, one |
| ! value for each system (if there is more than |
| ! one system). |
| -------------------!------------------------------------------------ |
| 2nd ! Source |
| Source ! |
| ! This column shows the source origin of the |
| ! alpha call-up (the related source component |
| ! and the number of the related system, if |
| ! applicable). |
| -------------------!------------------------------------------------ |
| 3rd ! Eq.Sys.Lab.SDI = Parameter number |
| Eq.Sys.Lab.SDI ! |
| ! This column shows the parameter number that |
| ! has the subsequent parts: |
| ! - Equipment identifier of the connected bus |
| ! (hexadecimal value of related ARINC 429 BUS) |
| ! - System number of the system which sends the |
| ! related parameter: |
| ! 1 for system one |
| ! 2 for system two |
| ! 3 for system three |
| ! - Label of the parameter (octal value |
| ! of related ARINC 429 BUS) |
| ! - SDI states the source/destination identifier |
| ! used by the system for the related parameter: |
| ! 00 means SDI 00 (0) |
| ! 01 means SDI 01 (1) |
| ! 10 means SDI 10 (2) |
| ! 11 means SDI 11 (3). |
| -------------------------------------------------------------------- |
The columns are described as follows:
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 1st ! Alpha Call-Up |
| Alpha Call-Up ! |
| ! This column shows the mnemonic for the |
| ! related parameter. |
| ! If you enter this code in the MCDU, the MCDU |
| ! display shows the current parameter value, one |
| ! value for each system (if there is more than |
| ! one system). |
| -------------------!------------------------------------------------ |
| 2nd ! Source |
| Source ! |
| ! This column shows the source origin of the |
| ! alpha call-up (the related source component |
| ! and the number of the related system, if |
| ! applicable). |
| -------------------!------------------------------------------------ |
| 3rd ! Eq/Sys/Lab/SDI = Parameter number |
| Eq/Sys/Lab/SDI ! |
| ! This column shows the parameter number that |
| ! has the subsequent parts: |
| ! - Equipment identifier of the connected bus |
| ! (hexadecimal value of related ARINC 429 BUS) |
| ! - System number of the system which sends the |
| ! related parameter: |
| ! 1 for system one |
| ! 2 for system two |
| ! 3 for system three |
| ! - Label of the parameter (octal value |
| ! of related ARINC 429 BUS) |
| ! - SDI states the source/destination identifier |
| ! used by the system for the related parameter: |
| ! 00 means SDI 00 (0) |
| ! 01 means SDI 01 (1) |
| ! 10 means SDI 10 (2) |
| ! 11 means SDI 11 (3). |
| -------------------------------------------------------------------- |
The columns are described as follows:
| -------------------------------------------------------------------- |
| Column | Description |
| -------------------+------------------------------------------------ |
| 1st | Alpha Call-Up |
| Alpha Call-Up | |
| | This column shows the mnemonic for the |
| | related parameter. |
| | If you enter this code in the MCDU, the MCDU |
| | display shows the current parameter value, one |
| | value for each system (if there is more than |
| | one system). |
| -------------------|------------------------------------------------ |
| 2nd | Source |
| Source | |
| | This column shows the source origin of the |
| | alpha call-up (the related source component |
| | and the number of the related system, if |
| | applicable). |
| -------------------|------------------------------------------------ |
| 3rd | Parameter number = Eq/Sys/Lab/SDI |
| Parameter Number | |
| | This column shows the parameter number that |
| | has the subsequent parts: |
| | - Equipment identifier of the connected bus |
| | (hexadecimal value of related ARINC 429 BUS) |
| | - System number of the system which sends the |
| | related parameter: |
| | 1 for system one |
| | 2 for system two |
| | 3 for system three |
| | - Label of the parameter (octal value |
| | of related ARINC 429 BUS) |
| | - SDI states the source/destination identifier |
| | used by the system for the related parameter: |
| | 00 means SDI 00 (0) |
| | 01 means SDI 01 (1) |
| | 10 means SDI 10 (2) |
| | 11 means SDI 11 (3). |
| -------------------------------------------------------------------- |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 4th ! ACCURACY |
| ACCURACY ! Two different types of values are shown |
| ! in this column: |
| ! The first one, indicated with an 'R' |
| ! (RESOLUTION) is related to the ARINC |
| ! 429 data bus. It also shows the |
| ! resolution of the data word. The second |
| ! one, with no specific indication, shows |
| ! the total accuracy of the parameter. |
| -------------------!------------------------------------------------ |
| 5th ! SIGN BIT |
| SIGN BIT ! |
| ! This column shows whether a sign bit |
| ! is available and in which bit position |
| ! of the data word it is situated. |
| -------------------!------------------------------------------------ |
| 6th ! DATA BITS |
| DATA BITS ! |
| ! Describes the number of data bits not |
| ! including the sign bit. 'A' and a number |
| ! means the discrete bit position in the |
| ! ARINC 429 data word. |
| ! For BCD coded data words the number of |
| ! significant data digits is shown, |
| ! indicated by '(1)'. |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 5th ! ACCURACY |
| ACCURACY ! Two different types of values are shown |
| ! in this column: |
| ! |
| ! The first one, indicated by an 'R' |
| ! (RESOLUTION) is related to the ARINC |
| ! 429 data bus. It shows the resolution |
| ! of the data word. The second |
| ! Attention: for the EUC programming use |
| ! the exact values. |
| ! |
| ! The second one, with no specific indication, |
| ! shows the total accuracy of the parameter. |
| -------------------!------------------------------------------------ |
| 6th ! SIGN BIT |
| SIGN BIT ! |
| ! This column shows whether a sign bit |
| ! is available and in which bit position |
| ! of the data word it is situated. |
| -------------------!------------------------------------------------ |
| 7th ! DATA BITS |
| DATA BITS ! |
| ! Describes the number of data bits not |
| ! including the sign bit. A '#' and a number |
| ! means the discrete bit position in the |
| ! ARINC 429 data word. |
| ! |
| ! For BCD coded data words the number of |
| ! significant data digits is shown, |
| ! visible by the remark'(1)'. |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 4th ! LSB |
| LSB ! |
| ! Last Significant Bit |
| -------------------!------------------------------------------------ |
| 5th ! PARAMETER |
| PARAMETER ! |
| ! Parameter name |
| -------------------!------------------------------------------------ |
| 6th ! ALPHA CODING |
| ALPHA CODING ! |
| ! This column shows the mnemonic for the parameter |
| ! (if available). If you enter this code in the |
| ! MCDU the current parameter-value shows on the |
| ! display. |
| ! The value from both systems (if available) show. |
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 4th ! Unit |
| Unit ! |
| ! This column shows the unit of the parameter. |
| -------------------!------------------------------------------------ |
| 5th ! Parameter |
| Parameter ! |
| ! This column shows the parameter name used by |
| ! the system for the related alpha call-up |
| ! code. |
| -------------------!------------------------------------------------ |
| 6th ! Comment |
| Comment ! |
| ! This column shows the additional data |
| ! of the alpha call-up parameter. |
| -------------------------------------------------------------------- |
| -------------------------------------------------------------------- |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 4th ! Unit |
| Unit ! |
| ! This column shows the unit of the parameter. |
| -------------------!------------------------------------------------ |
| 5th ! Parameter |
| Parameter ! |
| ! This column gives the parameter name used by |
| ! the system for the related alpha call-up code. |
| -------------------!------------------------------------------------ |
| 6th ! Comment |
| Comment ! |
| ! This column shows the additional data |
| ! of the alpha call-up parameter. |
| -------------------------------------------------------------------- |
| -------------------------------------------------------------------- |
| Column | Description |
| -------------------+------------------------------------------------ |
| 4th | Unit |
| Unit | |
| | This column shows the unit of the parameter. |
| -------------------|------------------------------------------------ |
| 5th | Parameter |
| Parameter | |
| | This column shows the parameter name used by |
| | the system for the related alpha call-up |
| | code. |
| -------------------|------------------------------------------------ |
| 6th | Comment |
| Comment | |
| | This column shows the additional data |
| | of the alpha call-up parameter. |
| -------------------------------------------------------------------- |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 7th ! UPD/s |
| UPD/s ! |
| ! This column shows how many times the |
| ! parameter will be transmitted by the source |
| ! system. |
| -------------------!------------------------------------------------ |
| 8th ! CODE |
| CODE ! |
| ! BNR = binary data word |
| ! BCD = binary coded decimal data word |
| ! ISO = data word coded in ISO 5 Code |
| ! DIS = discrete data word |
| ! HEX = hexadecimal coded |
| ! OCT = octal coded |
| ! HYB = mixed code; |
| ! e.g. : bit 11 to 16 DIS |
| ! bit 17 to 28 BNR |
| -------------------!------------------------------------------------ |
| 9th ! ALPHA CODING |
| ALPHA CODING ! |
| ! This column shows the mnemonic for the |
| ! parameter (if available). By entering |
| ! this code via the MCDU, the current |
| ! parameter-value will be shown on the |
| ! display. The value from both systems |
| ! (if available) will be shown. |
| -------------------!------------------------------------------------ |
| 10th ! This column shows the source origin, its |
| Source ! bus number, ATA Ref., and its label. |
| EQPT ! |
| BUS NR ! |
| ATA. REF ! |
| CONV ! |
| -------------------!------------------------------------------------ |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 8th ! UPD/sec |
| UPD/sec ! |
| ! This column shows how many times the |
| ! parameter will be transmitted by the source |
| ! system. |
| -------------------!------------------------------------------------ |
| 9th ! CODE |
| CODE ! |
| ! BNR = binary data word |
| ! BCD = binary coded decimal data word |
| ! ISO = data word coded in ISO 5 Code |
| ! DIS = discrete data word |
| ! HEX = hexadecimal coded |
| ! OCT = octal coded |
| ! HYB = mixed code; |
| ! e.g. : bit 11 to 16 DIS |
| ! bit 17 to 28 BNR |
| -------------------!------------------------------------------------ |
| 10th ! ALPHA CODING |
| ALPHA CODING ! |
| ! This column shows the mnemonic for the |
| ! parameter (if available). By entering |
| ! this code via the MCDU, the current |
| ! parameter-value will be shown on the |
| ! display. The value from both systems |
| ! (if available) will be shown. |
| -------------------!------------------------------------------------ |
| -------------------!------------------------------------------------ |
| Column ! Description |
| -------------------!------------------------------------------------ |
| 7th ! used |
| used ! |
| ! Used by DMU-function to process ACU, |
| ! trigger condition, report and recording. |
| -------------------!------------------------------------------------ |
| 8th ! DATA BITS |
| DATA BITS ! |
| ! Describes the number of data bits does not |
| ! include the sign bit. |
| ! A '#' and a number means the discrete bit |
| ! position in the ARINC 429 data word. |
| ! |
| ! For BCD coded data words the number of |
| ! significant data digits is shown, visible |
| ! with the remark '(1)'. |
| ! |
| ! The second one, with no specific indication, |
| ! shows the total accuracy of the parameter. |
| -------------------!------------------------------------------------ |
| 9th ! RANGE |
| RANGE ! |
| ! Three different types of ranges are shown |
| ! in this column: |
| ! |
| ! The first one, indicated by a 'W' (WORDRANGE), |
| ! is related to the ARINC 429 data bus and shows |
| ! the maximum value of the parameter that can be |
| ! transferred on the bus depending on the number |
| ! of data bits (see column DATA BITS) and the |
| ! resolution ('R') of the parameter (see column |
| ! ACCURANCY). |
| ! |
| ! The second one, with no specific indication, |
| ! shows the normal operational range of the |
| ! parameter. |
| ! |
| ! The third one is related to the ARINC 429 |
| ! Discrete Data Words. |
| ! There are two states: |
| ! 'bit status 0' or 'bit status 1'. |
| ! They indicate the true condition of the |
| ! corresponding data-word-bit position. |
| -------------------!------------------------------------------------ |
| 10th ! ACCURACY |
| ACCURACY ! |
| ! Two different types of values are shown in |
| ! this column: |
| ! |
| ! The first one, indicated by an 'R' (RESOLUTION) |
| ! is related to the ARINC 429 data bus and shows |
| ! the (rounded) resolution of the data word. |
| ! Attention: For the EUC programming the exact |
| ! values must be used. |
| ! |
| ! The second one, with no specific indication, shows |
| ! the total accuracy of the parameter. |
| -------------------!------------------------------------------------ |
| 11th ! Units |
| Units ! |
| ! This column shows the unit of the |
| ! parameter. |
| -------------------!------------------------------------------------ |
F. Parameter List
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! CHAPTER |
| ----!-------------------------------------!-------------- |
| 00A ! FAC 1 & 2 ! 22-69-00 |
| 07C § ECU 1 & 2 § 73-25-00 |
| 01B ! SFCC 1 & 2 ! 27-51-00 |
| 023 ! GPWS ! 34-48-00 |
| 026 ! FWC 1 & 2 ! 31-52-00 |
| 06E ! BSCU (optional) ! 32-42-00 |
| 07A ! ECB APU ! 49-61-00 |
| 06C ! FCDC 1 & 2 ! 27-95-00 |
| 004 ! ADIRU (IRS PART) 1 & 2 & 3 ! 34-14-00 |
| 006 ! ADIRU (ADC PART) 1 & 2 & 3 ! 34-13-00 |
| 001 ! FMGC (FGC PART) 1 & 2 ! 22-86-00 |
| 002 ! FMGC OWN C/CB1/CB2 (FMC PART) 1 & 2! 22-86-00 |
| 05D ! ZONE CONTROLLER ! 21-63-00 |
| 08E ! PACK CONTROLLER LH/RH ! 21-61-00 |
| 05C ! PRESSURE CONTROLLER 1 & 2 ! 21-30-00 |
| 06F ! BMC 1 & 2 ! 36-11-00 |
| 025 ! DMC 1 & 2 ! 31-62-00 |
| 05A ! FQIS ! 28-42-00 |
| 06D ! LGCIU 1 & 2 ! 32-61-00 |
| 029 ! SDAC 1 & 2 ! 31-54-00 |
| 03D ! EVM ! 77-30-00 |
| 0A1 ! FCU ! 22-81-00 |
| 07E ! CFDIU ! 31-32-00 |
| 017 ! FDIU ! 31-33-00 |
| 039 ! MCDU ! 22-82-00 |
| 040 ! PRINTER ! 31-35-00 |
| --------------------------------------------------------- |
| OD ! DMU ! 31-37-00 |
| --------------------------------------------------------- |
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! CHAPTER |
| ----!------------------------------------!--------------- |
| 00A ! FAC 1 & 2 ! 22-69-00 |
| 07C ! ECU CFMI 1 & 2 ! 73-25-00 |
| 07C ! EEC IAE 1 & 2 ! 73-25-00 |
| 01B ! SFCC 1 & 2 ! 27-51-00 |
| 023 ! GPWS ! 34-48-00 |
| 026 ! FWC 1 & 2 ! 31-52-00 |
| 06E ! BSCU ! 32-42-00 |
| 07A ! ECB APU ! 49-61-00 |
| 06C ! FCDU 1 & 2 ! 27-95-00 |
| 004 ! ADIRU (IRS PART) 1 & 2 ! 34-14-00 |
| 006 ! ADIRU (ADC PART) 1 & 2 ! 34-13-00 |
| 001 ! FMGC (FGC PART) 1 & 2 ! 22-86-00 |
| 002 ! FMGC (FMC PART) 1 & 2 ! 22-86-00 |
| 05D ! ZONE CONTROLLER ! 21-63-00 |
| 08E ! PACK CONTROLLER LH/RH ! 21-61-00 |
| 05C ! PRESSURE CONTROLLER 1 & 2 ! 21-30-00 |
| 06F ! BMC 1 & 2 ! 36-11-00 |
| 025 ! DMC 1 & 2 ! 31-62-00 |
| 05A ! FQIS ! 28-42-00 |
| 06D ! LGCIU 1 & 2 ! 32-61-00 |
| 029 ! SDAC 1 & 2 ! 31-54-00 |
| 03D ! EVM ! 77-30-00 |
| 0A1 ! FCU ! 22-81-00 |
| 07E ! CFDIU ! 31-32-00 |
| 017 ! FDIU ! 31-33-00 |
| 039 ! MCDU ! 22-82-00 |
| 040 ! PRINTER ! 31-35-00 |
| --------------------------------------------------------- |
| OD ! DMU ! 31-37-00 |
| --------------------------------------------------------- |
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! ENGINES ! CHAPTER |
| -----!-------------------------!-----------!------------- |
| 001 ! FMGC - FGC ! CFMI, IAE ! 22-86-00 |
| 002 ! FMGC OWN C/CB1/CB2- FMC! CFMI, IAE ! 22-86-00 |
| 004 ! ADIRU - IRS ! CFMI, IAE ! 34-14-00 |
| 006 ! ADIRU - ADC ! CFMI, IAE ! 34-13-00 |
| 00A ! FAC ! CFMI, IAE ! 22-66-00 |
| 017 ! FDIU ! CFMI, IAE ! 31-33-00 |
| 01B ! SFCC ! CFMI, IAE ! 27-51-00 |
| 023 ! GPWS ! CFMI, IAE ! 34-48-00 |
| 025 ! DMC ! CFMI, IAE ! 31-62-00 |
| 026 ! FWC ! CFMI, IAE ! 31-52-00 |
| 029 ! SDAC ! CFMI, IAE ! 31-54-00 |
| 037 ! WBS (not connected) ! CFMI, IAE ! 31-44-00 |
| 03D ! EVM (old MOD) ! CFMI, IAE ! 77-30-00 |
| 03D ! EVM (Standard) ! CFMI, IAE ! 77-30-00 |
| 03D ! EVM (Advanced) ! CFMI, IAE ! 77-30-00 |
| 05A ! FQIS ! CFMI, IAE ! 28-42-00 |
| 05A ! FQIS (Mod J0247) ! CFMI, IAE ! 28-42-00 |
| 05C ! PRECON ! CFMI, IAE ! 21-31-00 |
| 05D ! ZONE ! CFMI, IAE ! 21-63-00 |
| 06C ! FCDC ! CFMI, IAE ! 27-95-00 |
| 06D ! LGCIU ! CFMI, IAE ! 32-61-00 |
| 06E ! BSCU ! CFMI, IAE ! 32-42-00 |
| 06F ! BMC ! CFMI, IAE ! 36-11-00 |
| 07A ! APU - ECB ! CFMI, IAE ! 49-61-00 |
| 07C ! ECU/EEC ! CFMI, IAE ! 73-25-00 |
| 07E ! CFDIU ! CFMI, IAE ! 31-32-00 |
| 08E ! PACK ! CFMI, IAE ! 21-61-00 |
| 0A1 ! FCU ! CFMI, IAE ! 22-81-00 |
| 039 ! MCDU ! CFMI, IAE ! 22-82-00 |
| 040 ! PRINTER ! CFMI, IAE ! 31-35-00 |
| ---------------------------------------------------------- |
| OD ! DMU ! ! 31-37-00 |
| ---------------------------------------------------------- |
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! CHAPTER |
| ----!-------------------------------------!-------------- |
| 00A ! FAC 1 & 2 ! 22-69-00 |
| 01B ! SFCC 1 & 2 ! 27-51-00 |
| 025 ! DMC ! 31-62-00 |
| 026 ! FWC 1 & 2 ! 31-52-00 |
| 06E ! BSCU (optional) ! 32-42-00 |
| 07A ! ECB APU ! 49-61-00 |
| 07B ! EIU 1 & 2 ! 73-25-00 |
| 06C ! FCDC 1 & 2 ! 27-95-00 |
| 004 ! ADIRU (IRS PART) 1 & 2 & 3 ! 34-14-00 |
| 006 ! ADIRU (ADC PART) 1 & 2 & 3 ! 34-13-00 |
| 001 ! FMGC (FGC PART) 1 & 2 ! 22-86-00 |
| 002 ! FMGC OWN C/CB1/CB2 (FMC PART) 1 & 2! 22-86-00 |
| 05D ! ZONE CONTROLLER ! 21-63-00 |
| 08E ! PACK CONTROLLER LH/RH ! 21-61-00 |
| 05C ! PRESSURE CONTROLLER 1 & 2 ! 21-30-00 |
| 06F ! BMC 1 & 2 ! 36-11-00 |
| 025 ! DMC 1 & 2 ! 31-62-00 |
| 05A ! FQIC ! 28-42-00 |
| 06D ! LGCIU 1 & 2 ! 32-61-00 |
| 029 ! SDAC 1 & 2 ! 31-54-00 |
| 017 ! FDIU ! 31-33-00 |
| --------------------------------------------------------- |
| OD ! DMU ! 31-37-00 |
| --------------------------------------------------------- |
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! CHAPTER |
| ----!-------------------------------------!-------------- |
| 00A ! FAC 1 & 2 ! 22-69-00 |
| 07C ! EEC 1 & 2 ! 73-25-00 |
| 026 ! FWC 1 & 2 ! 31-52-00 |
| 06E ! BSCU (optional) ! 32-42-00 |
| 07A ! ECB APU ! 49-61-00 |
| 06C ! FCDC 1 & 2 ! 27-95-00 |
| 004 ! ADIRU (IRS PART) 1 & 2 & 3 ! 34-14-00 |
| 006 ! ADIRU (ADC PART) 1 & 2 & 3 ! 34-13-00 |
| 002 ! FMGC OWN C/CB1/CB2 (FMC PART) 1 & 2! 22-86-00 |
| 05D ! ZONE CONTROLLER ! 21-63-00 |
| 08E ! PACK CONTROLLER LH/RH ! 21-61-00 |
| 05C ! PRESSURE CONTROLLER 1 & 2 ! 21-30-00 |
| 06F ! BMC 1 & 2 ! 36-11-00 |
| 025 ! DMC 1 & 2 ! 31-62-00 |
| 05A ! FQIC ! 28-42-00 |
| 029 ! SDAC 1 & 2 ! 31-54-00 |
| --------------------------------------------------------- |
NOTE: Each set of parameters is in the applicable chapter.
| --------------------------------------------------------- |
| EQ ! SYSTEM ! CHAPTER |
| ----!-------------------------------------!-------------- |
| 00A ! FAC 1 & 2 ! 22-69-00 |
| 07C ! EEC 1 & 2 ! 73-25-00 |
| 07C ! ECU 1 & 2 ! 73-21-60 |
| 01B ! SFCC 1 & 2 ! 27-51-00 |
| 026 ! FWC 1 & 2 ! 31-52-00 |
| 06E ! BSCU (optional) ! 32-42-00 |
| 07A ! ECB APU ! 49-61-00 |
| 06C ! FCDC 1 & 2 ! 27-95-00 |
| 004 ! ADIRU (IRS PART) 1 & 2 & 3 ! 34-14-00 |
| 006 ! ADIRU (ADC PART) 1 & 2 & 3 ! 34-13-00 |
| 001 ! FMGC (FGC PART) 1 & 2 ! 22-86-00 |
| 002 ! FMGC OWN C/CB1/CB2 (FMC PART) 1 & 2! 22-86-00 |
| 05D ! ZONE CONTROLLER ! 21-63-00 |
| 08E ! PACK CONTROLLER LH/RH ! 21-61-00 |
| 05C ! PRESSURE CONTROLLER 1 & 2 ! 21-30-00 |
| 06F ! BMC 1 & 2 ! 36-11-00 |
| 025 ! DMC 1 & 2 ! 31-62-00 |
| 05A ! FQIC ! 28-42-00 |
| 06D ! LGCIU 1 & 2 ! 32-61-00 |
| 029 ! SDAC 1 & 2 ! 31-54-00 |
| 017 ! FDIU ! 31-33-00 |
| --------------------------------------------------------- |
| OD ! DMU ! 31-37-00 |
| --------------------------------------------------------- |
G. Parameter List
*1 = Only DMU output bus A
*2 = Only DMU output bus C
*3 = Only DMU output bus B
(1)= Significant Data Digits
*1 = Only DMU output bus A
*2 = Only DMU output bus C
*3 = Only DMU output bus B
(1)= Significant Data Digits
| +-----------------------------------------------------------------------------+ |
| ! PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) ! |
| !-----------------------------------------------------------------------------! |
| !EQ/SYS/LAB/SDI! PARAMETER ! RANGE !SIGN!DATA!UPD/!CODE!ALPHA! |
| ! ! DEFINITION ! ACCURACY !BIT !BITS!SEC ! !CODE ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/172/-- ! System Address ! ! ! ! ! ! ! |
| ! ! Label (SAL) ! ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/220/- ! MCDU 1 DATA ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/221/- ! MCDU 2 DATA ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/222/- ! MCDU 3 DATA ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/223/- ! Printer Label ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/226/- ! MDDU Data ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! *2! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/304/- ! ACARS Data ! File Data ! ! 23 ! 1 ! ISO! ! |
| ! ! *3! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/350/00 ! Maintenance ! ! ! 4 ! 2 ! DIS!MDMU ! |
| ! ! Word # 1 *1! ! ! ! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DMU FAIL ! bit status 1 ! ! #11! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR FAIL ! bit status 1 ! ! #12! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR Tape Low ! bit status 1 ! ! #13! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR Manual On ! bit status 1 ! ! #14! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR On ! bit status 1 ! ! #15! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! PCMCIA FAIL ! bit status 1 ! ! #16! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #17! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #18! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #19! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #20! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #21! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #22! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #23! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #24! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #25! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #26! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #27! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #28! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #29! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| ! 0D/1/356/00 ! Maintenance ! ! ! ! ! ! ! |
| ! ! Message *1! ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| ! 0D/1/377/00 ! Equipment *1! bits: ! !2(1)! 2 ! HEX! ! |
| ! ! Identification ! 11-14 low part ! ! ! ! ! ! |
| ! ! ! 15-18 high part ! ! ! ! ! ! |
| ! ! ! 19-29 logic '0' ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
*1 = Only DMU output bus A
*2 = Only DMU output bus C
*3 = Only DMU output bus B
(1)= Significant Data Digits
| +-----------------------------------------------------------------------------+ |
| ! PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) ! |
| !-----------------------------------------------------------------------------! |
| !EQ/SYS/LAB/SDI! PARAMETER ! RANGE !SIGN!DATA!UPD/!CODE!ALPHA! |
| ! ! DEFINITION ! ACCURACY !BIT !BITS!SEC ! !CODE ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/172/DD ! System Address ! ! ! ! ! ! ! |
| ! ! Label (SAL) ! ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/220/DD ! MCDU 1 DATA ! File Data ! ! 21 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/221/DD ! MCDU 2 DATA ! File Data ! ! 21 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/222/DD ! MCDU 3 DATA ! File Data ! ! 21 ! 1 ! ISO! ! |
| ! ! Label *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/223/DD ! Printer Label ! File Data ! ! 21 ! 1 ! ISO! ! |
| ! ! *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/226/DD ! MDDU Data ! File Data ! ! 21 ! 0 ! ISO! ! |
| ! ! *2! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/304/DD ! ACARS Data ! File Data ! ! 21 ! 0 ! ISO! ! |
| ! ! *3! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| !0D/1/350/00 ! Maintenance ! ! ! 4 ! 2 ! DIS!MDMU ! |
| ! ! Word # 1 *1! ! ! ! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DMU FAIL ! bit status 1 ! ! #11! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR FAIL ! bit status 1 ! ! #12! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR Tape Low ! bit status 1 ! ! #13! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR Manual On ! bit status 1 ! ! #14! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! DAR On ! bit status 1 ! ! #15! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! PCMCIA FAIL ! bit status 1 ! ! #16! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #17! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #18! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #19! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #20! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #21! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #22! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! FDIMU INSTALLED ! bit status 1 ! ! #23! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #24! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #25! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #26! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #27! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #28! ! ! ! |
| ! !-----------------!------------------!----!----!----!----!-----! |
| ! ! SPARE ! ! ! #29! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| ! 0D/1/354/DD ! LRU Ident ! File Data ! ! 21 ! 1 ! ISO! ! |
| ! ! *1! Transfer ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| ! 0D/1/356/DD ! Maintenance ! ! ! ! ! ! ! |
| ! ! Message *1! ! ! ! 4 ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
| ! 0D/1/377/00 ! Equipment *1! bits: ! !2(1)! 2 ! HEX! ! |
| ! ! Identification ! 11-14 low part ! ! ! ! ! ! |
| ! ! ! 15-18 high part ! ! ! ! ! ! |
| ! ! ! 19-29 logic '0' ! ! ! ! ! ! |
| !--------------!-----------------!------------------!----!----!----!----!-----! |
*1 = Only DMU output bus A
*2 = Only DMU output bus C
*3 = Only DMU output bus B
(1)= Significant Data Digits
H. Alpha Call-Up List
NOTE: This Alpha Call-Up list is for CFMI engines only.
| ------------------------------------------------------------------------------- |
| Alpha Parameter Unit Comment |
| ------------------------------------------------------------------------------- |
| ACTYP A/C Type (DMU computed) |
| ACW1 APU control word #1 (DMU computed) |
| ACW2 APU control word #2 (DMU computed) |
| ACW3 APU control word #3 (DMU computed) |
| ACW4 APU control word #4 (DMU computed) |
| ACYC APU cycles (DMU computed) |
| ACYI 7A 1 133 01 CYCLES APU start cycles |
| ADW1 7A 1 037 01 APU:Discrete status word #1 |
| AHRI 7A 1 132 01 H APU operating hours |
| AHRS APU hours (DMU computed) |
| AIL 6C 1 310 01 DEG Aileron position left |
| 6C 1 330 01 DEG Aileron position right |
| AILL 6C 1 310 01 DEG Aileron position left |
| 6C 2 310 10 DEG Aileron position left |
| AILR 6C 1 330 01 DEG Aileron position right |
| 6C 2 330 10 DEG Aileron position right |
| ALT 06 1 203 01 FEET Altitude (1013.25mb) (switched parameter) |
| 06 2 203 10 FEET Altitude (1013.25mb) (switched parameter) |
| ALT3 26 1 203 11 FEET altitude 3 (1013.25 ha) |
| ALTR 01 1 365 00 FT/MIN Altitude rate (VZBI) |
| 01 2 365 00 FT/MIN Altitude rate (VZBI) |
| AMW1 7A 1 353 01 APU:Maintenance word #l |
| AMW2 7A 1 351 01 APU:Maintenance word #2 |
| AMW3 7A 1 352 01 APU:Maintenance word #3 |
| AOA 06 1 241 01 DEG Corrected angle of attack system #l |
| 06 2 241 10 DEG Corrected angle of attack system #2 |
| A0A3 26 1 241 11 DEG Corrected angle of attack 3 |
| AP Auto pilot status (AP) left |
| Auto pilot status (AP) right |
| APLAT A/P lateral mode left |
| A/P lateral mode right |
| APLON A/P longitudinal mode left |
| A/P longitudinal mode right |
| ASN 7A 1 050 01 APU serial number |
| BP1 6E 1 300 01 BAR brake 1 pressure |
| 6E 2 300 10 BAR brake 1 pressure |
| BP2 6E 1 301 01 BAR brake 2 pressure |
| 6E 2 301 10 BAR brake 2 pressure |
| BP3 6E 1 302 01 BAR brake 3 pressure |
| 6E 2 302 10 BAR brake 3 pressure |
| BP4 6E 1 303 01 BAR brake 4 pressure |
| 6E 2 303 10 BAR brake 4 pressure |
| BT1 6E 1 114 01 DEGC Brake 1 temperature |
| 6E 2 114 10 DEGC Brake 1 temperature |
| BT2 6E 1 115 01 DEGC Brake 2 temperature |
| 6E 2 115 10 DEGC Brake 2 temperature |
| BT3 6E 1 116 01 DEGC Brake 3 temperature |
| 6E 2 116 10 DEGC Brake 3 temperature |
| BT4 6E 1 117 01 DEGC Brake 4 temperature |
| 6E 2 117 10 DEGC Brake 4 temperature |
| BVP 26 1 031 01 Scavenge valve open engine #1 |
| 26 1 031 10 Scavenge valve open engine #2 |
| CAS 06 1 206 01 KTS Computed air speed (switched parameter) |
| 06 2 206 10 KTS Computed air speed (switched parameter) |
| CAS3 26 1 206 11 KTS Computed air speed 3 |
| CFPG Calculated flight path acceleration system #1 |
| CG 02 1 077 00 %MAC Calculated flight path acceleration system #2 |
| 02 2 077 00 %MAC Long center of gravity (switched parameter) |
| CIVV Calculated inertial vertical speed system #1 |
| Calculated inertial vertical speed system #2 |
| CNT report count |
| COT 8E 1 123 11 DEGC Pack compr. outlet temperature LH |
| 8E 2 123 00 DEGC Pack compr. outlet temperature RH |
| CSV1 6E 1 310 01 MA current SVN1 |
| 6E 2 310 10 MA current SVN1 |
| CSV2 6E 1 311 01 MA current SVN2 |
| 6E 2 311 10 MA current SVN2 |
| CSV3 6E 1 312 01 MA current SVN3 |
| 6E 2 312 10 MA current SVN3 |
| CSV4 6E 1 313 01 MA current SVN4 |
| 6E 2 313 10 MA current SVN4 |
| DA 04 1 321 01 DEG Drift angle |
| 04 2 321 10 DEG Drift angle |
| DATE 17 1 260 00 GMT date |
| DMEF 25 1 035 01 MHz DME 1 frequency |
| 25 1 035 10 MHz DME 2 frequency |
| DSW1 6E 1 270 01 BSCU discrete status word 1 |
| 6E 2 270 10 BSCU discrete status word 1 |
| DSW2 6E 1 026 01 BSCU discrete status word 2 |
| 6E 2 026 10 BSCU discrete status word 2 |
| DSW3 6E 1 027 01 BSCU discrete status word 3 |
| 6E 2 027 10 BSCU discrete status word 3 |
| ECW1 Engine #1 control word #1 |
| Engine #2 control word #1 |
| ECW2 Engine #1 control word #2 |
| Engine #2 control word #2 |
| ECW3 Engine #1 control word #3 |
| Engine #2 control word #3 |
| ECW4 Engine #1 control word #4 |
| Engine #2 control word #4 |
| ECW5 Engine #1 control word #5 |
| Engine #2 control word #5 |
| ECYC Engine # 1 cycles (DMU computed) |
| Engine # 2 cycles (DMU computed) |
| EGT 7C 1 345 01 DEGC EGT LPT exit temp engine #1 |
| 7C 2 345 10 DEGC EGT LPT exit temp engine #2 |
| EGTA 7A 1 175 01 DEGC APU EGT |
| EGTF DEGC EGT LPT exit temp engine #1:Filtered parameter |
| DEGC EGT LPT exit temp engine #2:Filtered parameter |
| EGTK EGT corrected left (DMU computed) |
| EGT corrected right (DMU computed) |
| EGTP DEGC APU EGT PEAK during APU start |
| EGTR DEG delta EGT reference value in climb |
| delta EGT reference value in cruise |
| EHRS Engine #1 hours (DMU computed) |
| Engine #2 hours (DMU computed) |
| ELEV 6C 1 314 01 DEG Elevator position left |
| 6C 1 334 01 DEG Elevator position right |
| ENGFA 17 1 304 00 A/C type engine |
| ENTYP Engine type (DMU computed) |
| ERT 7C 1 050 01 H Engine #1 running time |
| 7C 2 050 10 H Engine #2 running time |
| ESN Engine #1 serial number (DMU computed) |
| Engine #2 serial number (DMU computed) |
| ESN1 7C 1 047 01 Engine serial number (First half) engine #1 |
| 7C 1 046 01 Engine serial number (Last half) engine #1 |
| ESN2 7C 2 047 10 Engine serial number (First half) engine #2 |
| 7C 2 046 10 Engine serial number (Last half) engine #2 |
| EVM 3D 1 035 01 EVM discrete word #1 engine #1 |
| 3D 1 035 10 EVM discrete word #1 engine #2 |
| F319 1B 1 137 01 FLAP actual position left for A319 |
| 1B 2 137 10 FLAP actual position right for A319 |
| F320 1B 1 137 01 FLAP actual position left for A320 |
| 1B 2 137 10 FLAP actual position right for A320 |
| F321 1B 1 137 01 DEG FLAP actual position left for A321 |
| 1B 2 137 10 DEG FLAP actual position right for A321 |
| FD Fuel density left wing tank (DMU computed) |
| Fuel density right, wing tank (DMU computed) |
| FDC Fuel density center wing tank (DMU computed) |
| FDL Fuel density left wing tank (DMU computed) |
| FDR Fuel density right wing tank (DMU computed) |
| FDRAW 5A 2 272 10 Fuel density |
| FF 7C 1 244 01 PPH/KG Fuel mass flow rate engine #1 |
| 7C 2 244 10 PPH/KG Fuel mass flow rate engine #2 |
| FFK Fuel flow corrected engine #1 |
| Fuel flow corrected engine #2 |
| FLAP DEG FLAP actual position left |
| DEG FLAP actual position right |
| FLAPW DEG FLAP actual position switched |
| FLCNT Flight counter |
| FLNUM Flight number (DMU computed) |
| FLT Flight number (DMU computed) |
| FM Flight phase to display (DMU computed) |
| FMB Flight phase broadcasted to ACARS(DMU computed) |
| FMF 26 1 126 01 FWC Flight phases |
| 26 2 126 01 FWC Flight phases |
| FMGD1 01 1 274 00 FMGC discrete status word #1 |
| 01 2 274 00 FMGC discrete status word #1 |
| FMGD2 01 1 275 00 FMGC discrete status word #2 |
| 01 2 275 00 FMGC discrete status word #2 |
| FMGD4 01 1 146 00 FMGC discrete status word #4 |
| 01 2 146 00 FMGC discrete status word #4 |
| FMI Internal flight phase (DMU computed) |
| FMV 7C 1 347 01 % Selected FMV position engine #1 |
| 7C 2 347 10 % Selected FMV position engine #2 |
| FPA 04 1 322 01 DEG Flight path angle |
| 04 2 322 10 DEG Flight path angle |
| FPAC 04 1 323 01 G Flight path acceleration |
| 04 2 323 10 G Flight path acceleration |
| FPPU 1B 1 137 01 DEG FLAP actual position (FPPU angle value) |
| 1B 2 137 10 DEG FLAP actual position (FPPU angle value) |
| FROM Departure (DMU computed) |
| FRTO ORIGIN Departure (DMU computed) |
| Destination (DMU COMPUTED) |
| FT 5A 2 177 10 DEGC Fuel temperature engine #1 |
| 5A 2 201 10 DEGC Fuel temperature engine #2 |
| GLA 29 1 100 00 % APU Generator load |
| 29 2 100 00 % APU Generator load |
| GLE 29 1 077 01 % Generator load engine #1 |
| 29 1 077 10 % Generator load engine #2 |
| GLS 25 1 174 01 DDM ILS1 glideslope deviation |
| 25 1 174 10 DDM ILS2 glideslope deviation |
| GS 04 1 312 01 KTS Ground speed |
| 04 2 312 10 KTS Ground speed |
| GW 02 1 075 00 10Kg Actual Gross Weight |
| 02 2 075 00 10Kg Actual Gross Weight |
| GWFK 0A 1 074 00 KG gross weight FAC (kg) |
| 0A 2 074 00 KG gross weight FAC (kg) |
| GWFL 0A 1 074 00 LBS gross weight FAC (lbs) |
| 0A 2 074 00 LBS gross weight FAC (lbs) |
| HPT 7C 1 306 01 % Selected HPTC position engine #1 |
| 7C 2 306 10 % Selected HPTC position engine #2 |
| HPTC 7C 1 063 01 % HPTC demand #1 |
| 7C 2 063 10 % HPTC demand #2 |
| IALT 04 1 361 FEET Inertial altitude |
| 04 2 361 FEET Inertial altitude |
| IGV 7A 1 130 01 DEG APU IGV position |
| ILS 25 1 033 01 MHz ILS 1 frequency |
| 25 1 033 10 MHz ILS 2 frequency |
| IVV 04 1 365 01 FT/MIN Initial vertical speed |
| 04 2 365 10 FT/MIN Initial vertical speed |
| K K value for divergence (EGT or TN) computing |
| LATA 29 1 332 01 G Lateral acceleration |
| 29 2 332 01 G Lateral acceleration |
| LATG 04 1 332 01 G body lateral acceleration |
| 04 2 332 10 G body lateral acceleration |
| LATP 04 1 310 Present position latitude system 1 |
| 04 2 310 Present position latitude system 2 |
| LCDT 7A 1 074 01 DEGC APU Bleed air temperature |
| LCIT 7A 1 110 01 DEGC APU Load compressor inlet temperature |
| LGDW 6D 1 021 01 LGCIU discrete word #2 |
| 6D 2 021 10 LGCIU discrete word #2 |
| LOC 25 1 173 01 DDM ILS1 localizer deviation |
| 25 1 173 10 DDM ILS2 localizer deviation |
| LONA 29 1 331 01 G Longitudinal acceleration |
| 29 2 331 01 G Longitudinal acceleration |
| LONG 04 1 331 01 G body longitudinal acceleration |
| 04 2 331 10 G body longitudinal acceleration |
| LONP 04 1 311 DEG Present position longitude System 1 |
| 04 2 311 DEG Present position longitude system 2 |
| LOPP 6E 1 331 01 DEG Left brake pedal angle |
| 6E 2 330 10 DEG Left brake pedal angle |
| LPT 7C 1 307 01 % Selected LPTC position engine #1 |
| 7C 2 307 10 % Selected LPTC position engine #2 |
| MFDI 17 1 350 00 FDIU maintenance word |
| MH 04 1 320 01 DEG Magnetic heading |
| 04 2 320 10 DEG Magnetic heading |
| MN 06 1 205 01 MACH Mach (switched parameter) |
| 06 2 205 10 MACH Mach (switched Parameter) |
| MN3 26 1 205 11 MACH Mach 3 |
| MW1 7C 1 350 01 ECU Maintenance data word #1 engine #1 |
| 7C 2 350 10 ECU Maintenance data word #1 engine #2 |
| MW2 7C 1 351 01 ECU Maintenance data word #2 engine #1 |
| 7C 2 351 10 ECU Maintenance data word #2 engine #2 |
| MW3 7C 1 352 01 ECU Maintenance data word #3 engine #1 |
| 7C 2 352 10 ECU Maintenance data word #3 engine #2 |
| MW4 7C 1 353 01 ECU Maintenance data word #4 engine #1 |
| 7C 2 353 10 ECU Maintenance data word #4 engine #2 |
| MW5 7C 1 354 01 ECU Maintenance data word #5 engine #1 |
| 7C 2 354 10 ECU Maintenance data word #5 engine #2 |
| N1 7C 1 346 01 %RPM Actual (low rotor speed) engine #1 |
| 7C 2 346 10 %RPM Actual (low rotor speed) engine #2 |
| N1C 7C 1 341 01 %RPM N1 command engine #1 |
| 7C 2 341 10 %RPM N1 command engine #2 |
| N1F %RPM N1 Actual (low rotor speed) engine |
| #1:Filtered Parameter |
| %RPM N1 Actual (low rotor speed) engine |
| #2:Filtered Parameter |
| N1K N1K N1 corrected left (DMU computed) |
| N1 corrected right (DMU computed) |
| N1L 7C 1 337 01 %RPM N1 limit engine #1 |
| 7C 2 337 10 %RPM N1 limit engine #2 |
| N1MX 7C 1 342 01 %RPM N1 maximum engine #1 |
| 7C 2 342 10 %RPM N1 maximum engine #2 |
| N1R %RPM N1 left rate |
| %RPM N1 right rate |
| N2 7C 1 344 01 %RPM N2 Actual (high rotor speed) engine #1 |
| 7C 2 344 10 %RPM N2 Actual (high rotor speed) engine #2 |
| N2F %RPM N2 Actual (high rotor speed) engine #1:Filtered |
| %RPM N2 Actual (high rotor speed) engine #2:Filtered |
| N2K N2 corrected left (DMU computed) |
| N2 corrected right (DMU computed) |
| NA 7A 1 176 01 %RPM APU RPM |
| NAI 50 2 061 10 Nacelle anti-ice engine #1 open |
| 50 2 061 10 Nacelle anti-ice engine #2 open |
| NPA %RPM APU RPM at APU EGT peak during APU start |
| NRA 6E 1 336 01 DEG NWS reference angle |
| 6E 2 336 10 DEG NWS reference angle |
| NSVC 6E 1 335 01 MA current servo valve NWS |
| 6E 2 335 10 MA current servo valve NWS |
| NWSA 6E 1 334 01 DEG NWS angle |
| 6E 2 334 10 DEG NWS angle |
| OIP 26 1 317 01 PSI OIL pressure engine #1 |
| 26 1 317 10 PSI OIL pressure engine #2 |
| OIQ 26 1 073 01 QUART OIL quantity engine #1 |
| 26 1 073 10 QUART OIL quantity engine #2 |
| OIQH QTS/H OIL consumption from the previous flight Eng.#1 |
| QTS/H OIL consumption from the previous flight Eng.#2 |
| OIT 26 1 316 01 DEGC OIL temperature engine #1 |
| 26 1 316 10 DEGC OIL temperature engine #2 |
| OTA 7A 1 247 01 DEGC APU OIL sum temperature |
| OVP 5C 1 153 01 % Outflow valve position |
| 5C 2 153 10 % Outflow valve position |
| PO 7C 1 114 01 PSIA Selected PO (Ambient pressure) engine #1 |
| 7C 2 114 10 PSIA Selected PO (Ambient pressure) engine #2 |
| P2 7C 1 131 01 PSIA PT2 (FAN inlet pressure) engine #1 |
| 7C 2 131 10 PSIA PT2 (FAN inlet pressure) engine #2 |
| P25 7C 1 262 01 PSIA P2.5 (Low Pressure Compressor exit pressure) #1 |
| 7C 2 262 10 PSIA P2.5 (Low Pressure Compressor exit pressure) #2 |
| P2A 7A 1 112 01 BAR APU inlet pressure |
| P3 7C 1 264 01 PSIA Pb burner pressure engine #1 |
| 7C 2 264 10 PSIA Pb burner pressure engine #2 |
| PB 7C 1 264 01 PSIA Pb burner pressure engine #1 |
| 7C 2 264 10 PSIA Pb burner pressure engine #2 |
| PBV 8E 1 112 11 % Pack bypass valve position system #1 |
| 8E 2 112 00 % Pack bypass valve position system #2 |
| PCSW 5C 1 057 01 Press control bus:Status + Fault info |
| 5C 2 057 10 Press control bus:Status + Fault info |
| PD 6F 1 143 01 PSI Precooler inlet pressure engine #1 |
| 6F 1 142 01 PSI Precooler inlet pressure engine #2 |
| PDC 5C 1 144 01 PSI Cabin differential pressure |
| 5C 2 144 10 PSI Cabin differential pressure |
| PF 8E 1 126 11 KG/S Pack flow system #1 |
| 8E 2 126 00 KG/S Pack flow system #2 |
| PFAD 7A 1 004 01 APU:Performance adjustments |
| PH Flight phase to display (DMU computed) |
| PHA 3D 1 226 01 DEG N1 phase unbalance brg1 engine #1 |
| 3D 1 226 10 DEG N1 phase unbalance brg1 engine #2 |
| PHT 3D 1 226 11 DEG N1 phase unbalance TRF engine #1 |
| 3D 1 226 00 DEG N1 phase unbalance TRF engine #2 |
| PS13 7C 1 127 01 PSIA PS13 (FAN exit pressure) engine #1 |
| 7C 2 127 10 PSIA PS13 (FAN exit pressure) engine #2 |
| PSB 26 1 320 01 PSIA No4 bearing pressure engine #1 |
| 26 1 320 10 PSIA No4 bearing pressure engine #2 |
| PSEL Status of different FADEC sensor engine #1 |
| Status of different FADEC sensor engine #2 |
| PSW1 8E 1 062 11 Discrete data word (Label 062) of pack |
| control bus system #1 |
| 8E 2 062 00 Discrete data word (Label 062) of pack |
| control bus system #2 |
| PT 7A 1 166 01 BAR Bleed air pressure |
| PT2 7C 1 131 01 PSIA PT2 (FAN inlet pressure) engine #1 |
| 7C 2 131 10 PSIA PT2 (FAN inlet pressure) engine #2 |
| PTCH 04 1 324 01 DEG Pitch angle |
| 04 2 324 10 DEG Pitch angle |
| PTCR 04 1 326 01 DEG/S Body axis pitch rate |
| 04 2 326 10 DEG/S Body axis pitch rate |
| RAC 7C 1 055 01 % Rotor active clearance control position Eng. #1 |
| 7C 2 055 10 % Rotor active clearance control position Eng. #2 |
| RALT 25 1 164 01 FEET Radio height (R/A1) |
| 25 1 164 10 FEET Radio height (R/A2) |
| RI 8E 1 130 11 % Pack ram inlet position LH |
| 8E 2 130 00 % Pack ram inlet position RH |
| RO 8E 1 124 11 % Pack ram outlet position LH |
| 8E 2 124 00 % Pack ram outlet position RH |
| ROLL 04 1 325 01 DEG ROLL angle |
| 04 2 325 10 DEG ROLL angle |
| ROLR 04 1 327 01 DEG/S Body axis roll rate |
| 04 2 327 10 DEG/S Body axis roll rate |
| ROPP 6E 1 330 01 DEG Right brake pedal angle |
| 6E 2 330 10 DEG Right brake pedal angle |
| RSCC 6E 1 332 01 KTS reference speed command channel |
| 6E 2 332 10 KTS reference speed command channel |
| RSP2 6C 1 362 01 DEG LH spoiler #2 position |
| 6C 1 372 01 DEG RH spoiler #2 position |
| RSP3 6C 1 363 01 DEG LH spoiler #3 position |
| 6C 1 373 01 DEG RH spoiler #3 position |
| RSP4 6C 1 364 01 DEG LH spoiler #4 position |
| 6C 1 374 01 DEG RH spoiler #4 position |
| RSP5 6C 1 365 01 DEG LH spoiler #5 position |
| 6C 1 375 01 DEG RH spoiler #5 position |
| RUDD 29 1 312 00 DEG Rudder position |
| 29 2 312 00 DEG Rudder position |
| RUDT 0A 1 313 00 DEG Rudder trim |
| 0A 2 313 00 DEG Rudder trim |
| SAT 06 1 213 01 DEGC Static air temperature (BNR) |
| 06 2 213 10 DEGC Static air temperature (BNR) |
| SC1 29 1 242 01 DEGC/F Selected ckpt compt temp |
| SC1 29 2 242 01 DEGC/F Selected ckpt compt temp |
| SC2 29 1 244 01 DEGC/F Sel fwd cab compt temp |
| SC2 29 2 244 01 DEGC/F Sel fwd cab compt temp |
| SC3 29 1 244 01 DEGC/F Sel aft cab compt temp |
| SC3 29 2 244 01 DEGC/F Sel aft cab compt temp |
| SCC 6E 1 340 01 DEG steering command captain |
| 6E 2 340 10 DEG steering command captain |
| SCFD 6E 1 341 01 DEG steering command F/0 |
| 6E 2 341 10 DE steering command F/0 |
| SDS1 29 1 001 01 SDAC discrete word #1 |
| 29 2 001 01 SDAC discrete word #1 |
| SDS2 29 1 001 10 SDAC discrete word #2 |
| 29 2 001 10 SDAC discrete word #2 |
| SLAT 1B 1 127 01 DEG SLAT actual position system #1 |
| 1B 2 127 10 DEG SLAT actual position system #2 |
| SLP 0A 1 226 00 DEG Estimd sideslip (side slip angle) system #1 |
| 0A 2 226 00 DEG Estimd sideslip (side slip angle) system #2 |
| SM 7C 1 273 01 Autostart sequence in progress engine #1 |
| 7C 2 273 10 Autostart sequence in progress engine #2 |
| SSEL1 Status of different FADEC sensor: part 1 |
| SSEL2 Status of different FADEC sensor: part 2 |
| SSEL3 Status of different FADEC sensor: part 3 |
| SSEL4 Status of different FADEC sensor: part 4 |
| STA SEC APU start time |
| STA01 Stability status for report 01 monitoring |
| STA02 Stability status for report 02 monitoring |
| STAB 6C 1 315 01 DEG Stabilizer position #1 |
| STVC 26 1 032 01 Scavenge valve stuck closed engine #1 |
| 26 1 032 10 Scavenge valve stuck closed engine #2 |
| STVO 26 1 032 01 Scavenge valve stuck open engine #1 |
| 26 1 032 10 Scavenge valve stuck open engine #2 |
| SV 7C 1 270 01 Starter air valve open (local switch) engine #1 |
| 7C 2 270 10 Starter air valve open (local switch) engine #2 |
| SW1 7C 1 270 01 ECU Discrete status word #1 engine #1 |
| 7C 2 270 10 ECU Discrete status word #1 engine #2 |
| SW2 7C 1 272 01 ECU Discrete status word #2 engine #1 |
| 7C 2 272 10 ECU Discrete status word #2 engine #2 |
| SW3 7C 1 273 01 ECU Discrete status word #3 engine #1 |
| 7C 2 273 10 ECU Discrete status word #3 engine #2 |
| SW4 7C 1 274 01 ECU Discrete status word #4 engine #1 |
| 7C 2 274 10 ECU Discrete status word #4 engine #2 |
| SW5 7C 1 275 01 ECU Discrete status word #5 engine #1 |
| 7C 2 275 10 ECU Discrete status word #5 engine #2 |
| T12 7C 1 130 01 DEGC T12 (Fan inlet temperature) engine #1 |
| 7C 2 130 10 DEGC T12 (Fan inlet temperature) engine #2 |
| T25 7C 1 263 01 DEGC T2.5 (Low Pressure Compressor exit |
| temperature) engine #1 |
| 7C 2 263 10 DEGC T2.5 (Low Pressure Compressure exit |
| temperature) engine #2 |
| T3 7C 1 265 01 DEGC T3 (High Pressure Compressor exit |
| temperature) engine #1 |
| 7C 2 265 10 DEGC T3 (High Pressure Compressor exit |
| temperature) engine #2 |
| T5 7C 1 260 01 DEGC T5 (Low pressure turbine-exit |
| temperature) engine #1 |
| 7C 2 260 10 DEGC T5 (Low pressure turbine-exit |
| temperature) engine #2 |
| TAIL1 A/C ident word #1 (DMU computed) |
| TAIL2 A/C ident word #2 (DMU computed) |
| TAT 06 1 211 01 DEGC Total air temperature (BNR) (switched param.) |
| 06 2 211 10 DEGC Total air temperature (BNR) (switched param.) |
| THDG 04 1 044 01 DEG TRUE HEADING system #1 |
| 04 2 044 10 DEG TRUE HEADING system #2 |
| TLA 7C 1 133 01 DEG Selected TLA (Throttle resolver angle) Eng.#1 |
| 7C 2 133 10 DEG Selected TLA (Throttle resolver angle) Eng.#2 |
| TN 26 1 322 01 DEGC Nacelle temperature engine #1 |
| 26 1 322 10 DEGC Nacelle temperature engine #2 |
| TNR DEG delta TN reference value in climb |
| DEG delta TN reference value in cruise |
| TO Destination (DMU COMPUTED) |
| TP 8E 1 121 11 DEGC Pack outlet temperature LH |
| 8E 2 121 00 DEGC Pack outlet temperature RH |
| TPO 6F 1 141 01 DEGC Precooler eng #1 outlet temperature |
| 6F 1 140 01 DEGC Precooler eng #2 outlet temperature |
| TR 7C 1 273 01 4 T/R Doors (stowed and locked+deployed) Eng.1 |
| 7C 2 273 10 4 T/R Doors (stowed and locked+deployed) Eng.2 |
| TW 8E 1 111 11 DGEC Pack water extr. temperature LH |
| 8E 2 111 00 DGEC Pack water extr. temperature RH |
| UTC 17 1 150 00 UTC UTC (Universal time coordinated BNR) |
| V3 0A 1 263 00 KTS V3 (min speed flaps retracted ) |
| 0A 2 263 00 KTS V3 (min speed flaps retracted ) |
| V4 0A 1 264 00 KTS V4 (min speed slats retracted ) |
| 0A 2 264 00 KTS V4 (min speed slats retracted ) |
| VA 5D 2 220 10 % CAB temp reg vlv pos group 3 |
| VACC 04 1 364 01 G Vertical acceleration |
| 04 2 364 10 G Vertical acceleration |
| VB1 3D 1 135 01 UNITS N1 vibration eng #1 |
| 3D 1 135 10 UNITS N1 vibration eng #2 |
| VB2 3D 1 136 01 UNITS N2 vibration eng #1 |
| 3D 1 136 10 UNITS N2 vibration eng #2 |
| VBV 7C 1 071 01 DEG Selected VBV position (Variable bleed valve) #1 |
| 7C 2 071 10 DEG Selected VBV position (Variable bleed valve) #2 |
| VC 3D 1 230 01 IPS Displace unbalance TRF (LPT) eng1 |
| 3D 1 230 10 IPS Displace unbalance TRF (LPT) eng2 |
| VF 5D 2 206 10 % CAB temp reg vlv pos group 1 |
| VH 3D 1 230 11 IPS N2 veloc unbalance BRG1 (HPC)engine #1 |
| 3D 1 230 00 IPS N2 veloc unbalance BRG1 (HPC) engine #2 |
| VL 3D 1 227 11 MILS TRF pick up N1 track vibration engine 1 |
| 3D 1 227 00 MILS TRF pick up N1 track vibration engine 2 |
| VLS 0A 1 245 00 KTS VLS (Min. airspeed) |
| 0A 2 245 00 KTS VLS (Min. airspeed) |
| VMAN 0A 1 265 00 KTS Vman (maneuvering speed ) |
| 0A 2 265 00 KTS Vman (maneuvering speed ) |
| VMAX 0A 1 207 00 KTS V Max (Max. allowable airspeed) |
| 0A 2 207 00 KTS V Max (Max. allowable airspeed) |
| VN 3D 1 227 01 MILS Displace unbalance BRG1 or TRF engine 1 |
| 3D 1 227 10 MILS Displace unbalance BRG1 or TRF engine 2 |
| VORF 25 1 034 01 MHz VOR 1 frequency |
| 25 1 034 10 MHz VOR 2 frequency |
| VRTA 29 1 333 01 G Normal acceleration |
| 29 2 333 01 G Normal acceleration |
| VRTG 04 1 333 01 G body normal acceleration |
| 04 2 333 10 G body normal acceleration |
| VSCB 5C 1 150 01 FT/MIN Cabin v/s |
| 5C 2 150 10 FT/MIN Cabin v/s |
| VSV 7C 1 072 01 DEG Selected VSV position (Variable stator |
| vanes) engine #1 |
| 7C 2 072 10 DEG Selected VSV position (Variable stator |
| vanes) engine #2 |
| VW 5D 2 207 10 % CAB temp reg viv pos group 2 |
| WAI 29 1 001 11 WAI LH wing anti ice valve closed system #1 |
| 29 1 001 00 WAI RH wing anti ice valve closed system #2 |
| WARN 26 1 126 00 FWC Discrete status word (Label=1 26 SDI=00) |
| WB 7A 1 123 01 KG/S APU bleed air flow |
| WD 04 1 316 01 DEG WIND DIRECTION true system #1 |
| 04 2 316 10 DEG WIND DIRECTION true system #2 |
| WFQ 5A 2 257 10 KG/LBS Fuel quantity LH inner cell system #1 |
| 5A 2 261 10 KG/LBS Fuel quantity LH inner cell system #2 |
| WS 04 1 315 01 KTS WIND SPEED system #1 |
| 04 2 315 10 KTS WIND SPEED system #2 |
| WS1 6E 1 320 01 M/S wheel 1 speed |
| 6E 2 320 10 M/S wheel 1 speed |
| WS2 6E 1 321 01 M/S wheel 2 speed |
| 6E 2 321 10 M/S wheel 2 speed |
| WS3 6E 1 322 01 M/S wheel 3 speed |
| 6E 2 322 10 M/S wheel 3 speed |
| WS4 6E 1 323 01 M/S wheel 4 speed |
| 6E 2 323 10 M/S wheel 4 speed |
| YAW 04 1 330 01 DEG/S Body axis YAW rate |
| 04 2 330 10 DEG/S Body axis YAW rate |
| ZCB 5C 1 151 01 FEET Cabin altitude |
| 5C 2 151 10 FEET Cabin altitude |
| ZDW1 50 2 060 10 Discrete data word(Label 060) Zone |
| Controller bus2 |
| ZLD 5C 1 163 01 FEET Landing elevation |
| 5C 2 163 10 FEET Landing elevation |
NOTE: This Alpha Call-Up list is for CFMI engines only.
| ------------------------------------------------------------------------------- |
| Alpha Parameter Unit Comment |
| ------------------------------------------------------------------------------- |
| ACID11 17 1 301 00 A/C TAIL NUMBER CHARS.1 |
| ACID21 17 1 301 00 A/C TAIL NUMBER CHARS.2 |
| ACID31 17 1 301 00 A/C TAIL NUMBER CHARS.3 |
| ACID41 17 1 302 00 A/C TAIL NUMBER CHARS.4 |
| ACID51 17 1 302 00 A/C TAIL NUMBER CHARS.5 |
| ACID61 17 1 302 00 A/C TAIL NUMBER CHARS.6 |
| ACID71 17 1 303 00 A/C TAIL NUMBER CHARS.7 |
| ACIDB111 17 1 304 00 A/C TYPE CODE BITS 11-16 SYS. |
| ACIDB181 17 1 304 00 FLEET IDENT BITS 18-21 SYS. |
| ACYI 7A 1 133 01 CYCLES START CYCLES |
| ADW1ALL1 7A 1 37 01 APU SW 1 |
| ADW1B111 7A 1 37 01 APU BLEED VALVE OPEN |
| ADW1B121 7A 1 37 01 APU BLEED VALVE CLOSED |
| ADW1B131 7A 1 37 01 APU FUEL LOW PRESSURE |
| ADW1B171 7A 1 37 01 AUTOMATIC SHUT DOWN |
| ADW1B181 7A 1 37 01 EMERGENCY (EXTERNAL) S/D |
| ADW1B201 7A 1 37 01 LOW OIL LEVEL |
| ADW1B211 7A 1 37 01 MAIN ENG START MODE |
| ADW1B221 7A 1 37 01 APU START IN PROGRESS |
| AHRI 7A 1 132 01 HOURS OPERATING HOURS |
| AILL 6C 1 310 01 DEG AILERON POSITION LEFT SYS. |
| 6C 2 310 10 AILERON POSITION LEFT SYS. |
| AILR 6C 1 330 01 DEG AILERON POSITION RIGHT SYS. |
| 6C 2 330 10 AILERON POSITION RIGHT SYS. |
| ALT 06 1 203 01 FT ALTITUDE (1013.25MB) |
| 06 2 203 10 ALTITUDE (1013.25MB) |
| ALT01 06 1 203 01 ALTITUDE (1013.25MB) SYS. |
| ALT02 06 2 203 10 ALTITUDE (1013.25MB) SYS. |
| ALTBARFN 25 1 222 01 ALT BARO SET CAPT FINE |
| 25 2 222 10 ALT BARO SET CAPT FINE |
| ALTBARFO 25 1 223 01 ALT BARO SET F/O FINE |
| 25 2 223 10 ALT BARO SET F/O FINE |
| AMW1B111 7A 1 353 01 NO FLAME |
| AMW1B121 7A 1 353 01 REVERSE FLOW |
| AMW1B131 7A 1 353 01 LOSS OF DC POWER |
| AMW1B141 7A 1 353 01 HIGH OIL TEMPERATURE |
| AMW1B171 7A 1 353 01 INLET DOOR FAILURE |
| AMW1B181 7A 1 353 01 HIGH GEN. OIL TEMPERATURE |
| AMW1B201 7A 1 353 01 OVERTEMPERATURE |
| AMW1B211 7A 1 353 01 SENSOR FAILURE (EGT OR LOP) |
| AMW1B221 7A 1 353 01 NO ACCELERATION |
| AMW1B231 7A 1 353 01 SLOW START |
| AMW1B241 7A 1 353 01 OVERSPEED |
| AMW1B251 7A 1 353 01 ECB FAILURE |
| AMW1B261 7A 1 353 01 LOW OIL PRESSURE |
| AMW1B271 7A 1 353 01 LOSS OF OVERSPEED PROTECTION |
| AMW1B281 7A 1 353 01 INLET GUIDE VANES |
| AMW2ALL1 7A 1 351 01 APU CONTROL WORD |
| AMW2B111 7A 1 351 01 PT SENSOR |
| AMW2B121 7A 1 351 01 DELTA P SENSOR |
| AMW2B131 7A 1 351 01 SPEED SENSOR NO. 1 |
| AMW2B141 7A 1 351 01 SPEED SENSOR NO. 2 |
| AMW2B151 7A 1 351 01 HIGH OIL TEMP SWITCH |
| AMW2B161 7A 1 351 01 OIL TEMP SENSOR |
| AMW2B171 7A 1 351 01 FUEL CONTROL TORQUE MOTOR |
| AMW2B181 7A 1 351 01 SURGE VALVE TORQUE MOTOR |
| AMW2B191 7A 1 351 01 EGT RAKE NO. 1 |
| AMW2B201 7A 1 351 01 EGT RAKE NO. 2 |
| AMW2B211 7A 1 351 01 IGV ACTUATOR |
| AMW2B221 7A 1 351 01 IGNITION UNIT |
| AMW2B231 7A 1 351 01 DEOIL SOLENOID |
| AMW2B241 7A 1 351 01 GEN. OIL TEMP SENSOR |
| AMW2B251 7A 1 351 01 ECS DEMAND SIGNAL |
| AMW2B261 7A 1 351 01 APU STARTER |
| AMW2B271 7A 1 351 01 OIL PRESSURE SWITCH |
| AMW2B281 7A 1 351 01 P2 SENSOR |
| AMW2B291 7A 1 351 01 ECB |
| AMW3ALL1 7A 1 352 01 DISCRETE STATUS WORD |
| AMW3B121 7A 1 352 01 LOAD VALVE SOLENOID |
| AMW3B131 7A 1 352 01 LCDT SENSOR |
| AMW3B141 7A 1 352 01 LCIT SENSOR |
| AMW3B151 7A 1 352 01 FUEL SOLENOID |
| AMW3B161 7A 1 352 01 START CONTACTOR |
| AMW3B171 7A 1 352 01 BACK UP START CONTACTOR |
| AMW3B181 7A 1 352 01 APU S/N ENCODER |
| AMW3B201 7A 1 352 01 AIR INTAKE ACTUATOR |
| AMW3B221 7A 1 351 01 IGNITION UNIT |
| AOA1 06 1 241 01 DEG CORRECTED ANGLE OF ATTACK SYS. 1 |
| AOA2 06 2 241 10 DEG CORRECTED ANGLE OF ATTACK SYS. 2 |
| AP1146 01 1 146 00 SYS 1 AP LAND TRACK |
| AP1274 01 1 274 00 AP SYS 1 LABEL 274 (ALL BITS) |
| AP127411 01 1 274 00 AP SYS 1 LABEL 274 BIT 11 |
| AP127412 01 1 274 00 AP SYS 1 LABEL 274 BIT 12 |
| AP127413 01 1 274 00 AP SYS 1 LABEL 274 BIT 13 |
| AP127414 01 1 274 00 AP SYS 1 LABEL 274 BIT 14 |
| AP127415 01 1 274 00 AP SYS 1 LABEL 274 BIT 15 |
| AP127416 01 1 274 00 AP SYS 1 LABEL 274 BIT 16 |
| AP127417 01 1 274 00 AP SYS 1 LABEL 274 BIT 17 |
| AP127418 01 1 274 00 AP SYS 1 LABEL 274 BIT 18 |
| AP127419 01 1 274 00 AP SYS 1 LABEL 274 BIT 19 |
| AP127420 01 1 274 00 AP SYS 1 LABEL 274 BIT 20 |
| AP127421 01 1 274 00 AP SYS 1 LABEL 274 BIT 21 |
| AP127422 01 1 274 00 AP SYS 1 LABEL 274 BIT 22 |
| AP127423 01 1 274 00 AP SYS 1 LABEL 274 BIT 23 |
| AP127424 01 1 274 00 AP SYS 1 LABEL 274 BIT 24 |
| AP1275 01 1 275 00 AP SYS 1 LABEL 275 (ALL BITS) |
| AP127511 01 1 275 00 AP SYS 1 LABEL 275 RUNWAY MODE |
| AP127512 01 1 275 00 AP SYS 1 LABEL 275 NAV MODE |
| AP127513 01 1 275 00 AP SYS 1 LABEL 275 LOC CAPTURE MODE |
| AP127514 01 1 275 00 AP SYS 1 LABEL 275 LOC TRACK MODE |
| AP127515 01 1 275 00 AP SYS 1 LABEL 275 ROLL GO AROUND MODE |
| AP127516 01 1 275 00 AP SYS 1 LABEL 275 HEADING MODE |
| AP127517 01 1 275 00 AP SYS 1 LABEL 275 TRACK MODE |
| AP2146 01 2 146 00 SYS 2 AP LAND TRACK |
| AP2274 01 2 274 00 AP SYS 2 LABEL 274 (ALL BITS) |
| AP227411 01 2 274 00 AP SYS 2 LABEL 274 BIT 11 |
| AP227412 01 2 274 00 AP SYS 2 LABEL 274 BIT 12 |
| AP227413 01 2 274 00 AP SYS 2 LABEL 274 BIT 13 |
| AP227414 01 2 274 00 AP SYS 2 LABEL 274 BIT 14 |
| AP227415 01 2 274 00 AP SYS 2 LABEL 274 BIT 15 |
| AP227416 01 2 274 00 AP SYS 2 LABEL 274 BIT 16 |
| AP227417 01 2 274 00 AP SYS 2 LABEL 274 BIT 17 |
| AP227418 01 2 274 00 AP SYS 2 LABEL 274 BIT 18 |
| AP227419 01 2 274 00 AP SYS 2 LABEL 274 BIT 19 |
| AP227420 01 2 274 00 AP SYS 2 LABEL 274 BIT 20 |
| AP227421 01 2 274 00 AP SYS 2 LABEL 274 BIT 21 |
| AP227422 01 2 274 00 AP SYS 2 LABEL 274 BIT 22 |
| AP227423 01 2 274 00 AP SYS 2 LABEL 274 BIT 23 |
| AP227424 01 2 274 00 AP SYS 2 LABEL 274 BIT 24 |
| AP2275 01 2 275 00 AP SYS 2 LABEL 275 (ALL BITS) |
| AP227511 01 2 275 00 AP SYS 2 LABEL 275 RUNWAY MODE BIT 11 |
| AP227512 01 2 275 00 AP SYS 2 LABEL 275 NAV MODE BIT 12 |
| AP227513 01 2 275 00 AP SYS 2 LABEL 275 LOC CAPTURE BIT 13 |
| AP227514 01 2 275 00 AP SYS 2 LABEL 275 LOC TRACK BIT 14 |
| AP227515 01 2 275 00 AP SYS 2 LABEL 275 ROLL GO AROUND BIT 15 |
| AP227516 01 2 275 00 AP SYS 2 LABEL 275 HEADING BIT 16 |
| AP227517 01 2 275 00 AP SYS 2 LABEL 275 TRACK BIT 17 |
| ASN 7A 1 50 01 APU SERIAL NUMBER SYS. 1 |
| AUTBRKFF 6E 1 26 01 AUTO BRAKE OFF |
| 6E 2 26 10 AUTO BRAKE OFF |
| AUTBRKFT 6E 1 26 01 AUTO BRAKE FAULT |
| 6E 2 26 10 AUTO BRAKE FAULT |
| BMCW4152 6F 1 66 01 BMC DISCRETE WORD # 4 |
| 6F 2 66 10 BMC DISCRETE WORD # 4 |
| BMCW4172 6F 1 66 01 BMC DISCRETE WORD # 4 |
| 6F 2 66 10 BMC DISCRETE WORD # 4 |
| BMCW5151 6F 1 67 01 BMC DISCRETE WORD # 5 |
| 6F 2 67 10 BMC DISCRETE WORD # 5 |
| BMCW5172 6F 1 67 01 BMC DISCRETE WORD # 5 |
| 6F 2 67 10 BMC DISCRETE WORD # 5 |
| BSCU281 6E 1 27 01 BSCU SYSTEM 1 ENGAGED |
| BSCU282 6E 2 27 10 BSCU SYSTEM 2 ENGAGED |
| BVP1B211 26 1 31 01 ENG1 MODE SELECT SYS.1 |
| BVP1B212 26 2 31 01 ENG1 MODE SELECT SYS.2 |
| BVP1B261 26 1 31 01 ENG1 SCAVENGE VLV OPEN SYS.1 |
| 26 2 31 01 ENG1 SCAVENGE VLV OPEN SYS.1 |
| BVP2B261 26 1 31 10 ENG2 SCAVENGE VLV OPEN SYS.1 |
| 26 2 31 10 ENG2 SCAVENGE VLV OPEN SYS.1 |
| CAS 06 1 206 01 KTS COMPUTED AIRSPEED |
| 06 2 206 10 COMPUTED AIRSPEED |
| CAS1 06 1 206 01 COMPUTED AIRSPEED SYS.1 |
| CAS2 06 2 206 10 % MAC COMPUTED AIRSPEED SYS.2 |
| CG 02 1 77 00 LONG CENTER OF GRAVITY |
| 02 2 77 00 LONG CENTER OF GRAVITY |
| CG1 02 1 77 00 LONG CENTER OF GRAVITY SYS.1 |
| CG2 02 2 77 00 LONG CENTER OF GRAVITY SYS.2 |
| CONSALT1 25 1 163 01 CONSTRAINED ALTITUDE |
| 25 2 163 10 CONSTRAINED ALTITUDE |
| COT1 8E 1 123 11 DEG. C PACK COMPR. OUTLET TEMPERATURE SYS.1 |
| COT2 8E 2 123 00 DEG. C PACK COMPR. OUTLET TEMPERATURE SYS.2 |
| CTYPR40A 01 1 40 NA CITY PAIR LABEL 040 FOR DAR |
| CTYPR41A 01 1 41 NA CITY PAIR LABEL 041 FOR DAR |
| CTYPR42A 01 1 42 NA CITY PAIR LABEL 042 FOR DAR |
| DA1 04 1 321 01 DEG DRIFT ANGLE SYS.1 |
| 04 2 321 10 DRIFT ANGLE SYS.1 |
| DATEDDA 17 1 260 00 DATE (DAY) |
| 7E 1 260 00 DATE (DAY) |
| DATEDDQ 17 1 260 00 DATE (DAY) FOR QAR RCDG. |
| 7E 1 260 00 DATE (DAY) FOR QAR RCDG. |
| DATEMMA 17 1 260 00 DATE (MONTH) |
| 7E 1 260 00 DATE (MONTH) |
| DATEMMQ 17 1 260 00 DATE (MONTH) FOR QAR RCDG. |
| 7E 1 260 00 DATE (MONTH) FOR QAR RCDG. |
| DATEYYA 17 1 260 00 DATE (YEAR) |
| 7E 1 260 00 DATE (YEAR) |
| DECELL01 6E 1 27 01 DECELERATION LO ARMED |
| 6E 2 27 10 DECELERATION LO ARMED |
| DECELMD1 6E 1 27 01 DECELERATION MED ARMED |
| 6E 2 27 10 DECELERATION MED ARMED |
| DECELMX1 6E 1 27 01 DECELERATION MAX ARMED |
| 6E 2 27 10 DECELERATION MAX ARMED |
| DECHGHT1 25 1 370 01 SELECTED DECISION HEIGHT |
| 25 2 370 10 SELECTED DECISION HEIGHT |
| DME1DST1 25 1 202 01 DME 1 DISTANCE |
| 25 2 202 01 DME 1 DISTANCE |
| DME1FRQ1 25 1 35 01 DME 1 FREQUENCY |
| 25 2 35 01 DME 1 FREQUENCY |
| DME2DST2 25 1 202 10 DME 2 DISTANCE |
| 25 2 202 10 DME 2 DISTANCE |
| DME2FRQ1 25 1 35 10 DME 2 FREQUENCY |
| 25 2 35 10 DME 2 FREQUENCY |
| DSW12611 26 1 126 11 FWC 1 VALID |
| EGT1 7C 1 345 01 DEG. C IAE EGT LPT EXIT TEMP SYS.1 |
| EGT1S 7C 1 345 01 DEG. C IAE EGT LPT EXIT TEMP SYS.1 |
| EGT2 7C 2 345 01 DEG. C IAE EGT LPT EXIT TEMP SYS.2 |
| EGT2S 7C 2 345 10 DEG. C IAE EGT LPT EXIT TEMP SYS.2 |
| EGTA 7A 1 175 01 DEG. C EGT (APU) |
| EGTSEL1 7C 1 345 01 DEG. C IAE EGT LPT EXIT TEMP SYS.1 |
| EGTSEL2 7C 2 345 10 DEG IAE EGT LPT EXIT TEMP SYS.2 |
| ELEV1 6C 1 314 01 ELEVATOR POSITION LEFT SYS.1 |
| 6C 2 314 10 ELEVATOR POSITION LEFT SYS.1 |
| ELEV2 6C 1 334 01 ELEVATOR POSITION RIGHT SYS.1 |
| 6C 2 334 10 ELEVATOR POSITION RIGHT SYS.1 |
| ENGICE1 26 1 17 01 ENG 1 SEVERITY ICE DETECTED |
| 26 2 17 01 ENG 1 SEVERITY ICE DETECTED |
| ENGICE2 26 1 17 10 ENG 2 SEVERITY ICE DETECTED |
| 26 2 17 10 ENG 2 SEVERITY ICE DETECTED |
| ERT1 7C 1 50 01 HOURS ENGINE RUNNING TIME |
| ERT2 7C 2 50 10 HOURS ENGINE RUNNING TIME |
| ESNL1 7C 1 46 01 ENGINE S/N LEFT DIGIT # 1 (LSD) |
| ESNL2 7C 1 46 01 ENGINE S/N LEFT DIGIT # 2 |
| ESNL3 7C 1 46 01 ENGINE S/N LEFT DIGIT # 3 |
| ESNL4 7C 1 47 01 ENGINE S/N LEFT DIGIT # 4 |
| ESNL5 7C 1 47 01 ENGINE S/N LEFT DIGIT # 5 |
| ESNL6 7C 1 47 01 ENGINE S/N LEFT DIGIT # 6 |
| ESNR1 7C 2 46 10 ENGINE S/N RIGHT DIGIT # 1 (LSD) |
| ESNR2 7C 2 46 10 ENGINE S/N RIGHT DIGIT # 2 |
| ESNR3 7C 2 46 10 ENGINE S/N RIGHT DIGIT # 3 |
| ESNR4 7C 2 47 10 ENGINE S/N RIGHT DIGIT # 4 |
| ESNR5 7C 2 47 10 ENGINE S/N RIGHT DIGIT # 5 |
| ESNR6 7C 2 47 10 ENGINE S/N RIGHT DIGIT # 6 |
| EVENT 17 1 350 00 EVENT BUTTON PRESSED |
| EVMB111 3D 1 35 01 N1 NB VIB. ABOVE ECAM ADVISORY SYS. 1 |
| EVMB112 3D 1 35 10 N1 NB VIB. ABOVE ECAM ADVISORY SYS. 2 |
| EVMB121 3D 1 35 01 N2 NB VIB. ABOVE ECAM ADVISORY SYS. 1 |
| EVMB122 3D 1 35 10 N2 NB VIB. ABOVE ECAM ADVISORY SYS. 2 |
| EVMB131 3D 1 35 01 TRF USED SYS. 1 |
| EVMB132 3D 1 35 10 TRF USED SYS. 2 |
| EVMB141 3D 1 35 01 INITIAL VALUES NOT USED SYS. 1 |
| EVMB142 3D 1 35 10 INITIAL VALUES NOT USED SYS. 2 |
| EVMB151 3D 1 35 01 FREQUENCY ANALYSIS DONE SYS. 1 |
| EVMB152 3D 1 35 10 FREQUENCY ANALYSIS DONE SYS. 2 |
| EVMB161 3D 1 35 01 N1 BEARING ACCEL CHANNEL FAULT SYS.1 |
| EVMB162 3D 1 35 10 N1 BEARING ACCEL CHANNEL FAULT SYS.2 |
| EVMB171 3D 1 35 01 TRF ACCEL CHANNEL FAULT SYS.1 |
| EVMB172 3D 1 35 10 TRF ACCEL CHANNEL FAULT SYS.2 |
| EVMB181 3D 1 35 01 N1 SPEED CHANNEL FAULT SYS.1 |
| EVMB182 3D 1 35 10 N1 SPEED CHANNEL FAULT SYS.2 |
| EVMB191 3D 1 35 01 N2 SPEED CHANNEL FAULT SYS.1 |
| EVMB192 3D 1 35 10 N2 SPEED CHANNEL FAULT SYS.2 |
| EVMB201 3D 1 35 01 UNBALANCE PROCESS FAULT SYS.1 |
| EVMB202 3D 1 35 10 UNBALANCE PROCESS FAULT SYS.2 |
| EVMB211 3D 1 35 01 FREQUENCY ANALYSIS FAULT SYS.1 |
| EVMB212 3D 1 35 10 FREQUENCY ANALYSIS FAULT SYS.2 |
| EVMB221 3D 1 35 01 NON-VOLATILE MEMORY FAULT SYS.1 |
| EVMB222 3D 1 35 10 NON-VOLATILE MEMORY FAULT SYS.2 |
| EVMB231 3D 1 35 01 PROVISION 1 SYS. 1 |
| EVMB232 3D 1 35 10 PROVISION 1 SYS. 2 |
| EVMB241 3D 1 35 01 PROVISION 2 SYS.1 |
| EVMB242 3D 1 35 10 PROVISION 2 SYS.2 |
| EVMB251 3D 1 35 01 PROVISION 3 SYS.1 |
| EVMB252 3D 1 35 10 PROVISION 3 SYS.2 |
| EVMB261 3D 1 35 01 PROVISION 4 SYS.1 |
| EVMB262 3D 1 35 10 PROVISION 4 SYS.2 |
| EVMB271 3D 1 35 01 ONE VIB DAT ABOVE ADVISORY SYS.1 |
| EVMB272 3D 1 35 10 ONE VIB DAT ABOVE ADVISORY SYS.2 |
| EVMB281 3D 1 35 01 EVMU CLASS 2 FAULT SYS.1 |
| EVMB282 3D 1 35 10 EVMU CLASS 2 FAULT SYS.2 |
| EVMB291 3D 1 35 01 EVMU CLASS 1 FAULT SYS.1 |
| EVMB292 3D 1 35 10 EVMU CLASS 1 FAULT SYS.2 |
| EVMBALL1 3D 1 35 01 HEX ENGINE VIBRATION STATUS WORD ENG.1 |
| EVMBALL2 3D 1 35 10 HEX ENGINE VIBRATION STATUS WORD ENG.2 |
| FD 5A 2 272 10 KG/L FUEL DENSITY (LEFT CNTR OR RIGHT TANK) |
| FDTANK2 5A 2 272 10 TANK FOR FUEL DENSITY |
| FFKG1 7C 1 244 01 KGPH FUEL MASS FLOW RATE SYS.1 (KG) |
| FFKG1S 7C 1 244 01 KGPH FUEL MASS FLOW RATE SYS.1 (KG) |
| FFKG2 7C 2 244 10 KGPH FUEL MASS FLOW RATE SYS.2 (KG) |
| FFKG2S 7C 2 244 10 KGPH FUEL MASS FLOW RATE SYS.2 (KG) |
| FLAP1 1B 1 137 01 DEG FLAP ACTUAL POSITION SYS.1 (LEFT) |
| FLAP2 1B 2 137 10 DEG FLAP ACTUAL POSITION SYS.2 (RIGHT) |
| FLTN233A 01 1 233 00 FLIGHT NUMBER LABEL 233 FOR DAR |
| FLTN234A 01 1 234 00 FLIGHT NUMBER LABEL 234 FOR DAR |
| 01 2 234 00 FLIGHT NUMBER LABEL 234 FOR DAR |
| FLTN235A 01 1 235 00 FLIGHT NUMBER LABEL 235 FOR DAR |
| 01 2 235 00 FLIGHT NUMBER LABEL 235 FOR DAR |
| FLTN236A 01 1 236 00 FLIGHT NUMBER LABEL 236 FOR DAR |
| 01 2 236 00 FLIGHT NUMBER LABEL 236 FOR DAR |
| FLTN01A 01 1 233 00 FLIGHT NUMBER DIGIT # 1 LEFTMOST |
| 01 2 233 00 FLIGHT NUMBER DIGIT # 1 LEFTMOST |
| FLTN02A 01 1 233 00 FLIGHT NUMBER DIGIT # 2 |
| 01 2 233 00 FLIGHT NUMBER DIGIT # 2 |
| FLTN03A 01 1 234 00 FLIGHT NUMBER DIGIT # 3 |
| 01 2 234 00 FLIGHT NUMBER DIGIT # 3 |
| FLTN04A 01 1 234 00 FLIGHT NUMBER DIGIT # 4 |
| 01 2 234 00 FLIGHT NUMBER DIGIT # 4 |
| FLTN05A 01 1 235 00 FLIGHT NUMBER DIGIT # 5 (MSD RECORDED) |
| 01 2 235 00 FLIGHT NUMBER DIGIT # 5 (MSD RECORDED) |
| FLTN06A 01 1 235 00 FLIGHT NUMBER DIGIT # 6 |
| 01 2 235 00 FLIGHT NUMBER DIGIT # 6 |
| FLTN07A 01 1 236 00 FLIGHT NUMBER DIGIT # 7 |
| 01 2 236 00 FLIGHT NUMBER DIGIT # 7 |
| FLTN08A 01 1 236 00 FLIGHT NUMBER DIGIT # 8 |
| 01 2 236 00 FLIGHT NUMBER DIGIT # 8 |
| FMV1 7C 1 347 01 SELECTED FMV POSITION SYS.1 |
| FMV2 7C 2 347 10 SELECTED FMV POSITION SYS.2 |
| FMVSEL1 7C 1 347 01 SELECTED FMV POSITION SYS.1 |
| FMVSEL2 7C 2 347 10 SELECTED FMV POSITION SYS.2 |
| FPASEL1 25 1 115 01 SELECTED FPA |
| 25 2 115 10 SELECTED FPA |
| FQ 5A 2 250 10 PRE-SELECTED FUEL QUANTITY |
| FROM1A 01 1 40 NA DEPARTURE AIRPORT CHAR.#1 LEFTMOST |
| 01 2 40 NA DEPARTURE AIRPORT CHAR.#1 LEFTMOST |
| FROM2A 01 1 40 NA DEPARTURE AIRPORT CHAR.#2 |
| 01 2 40 NA DEPARTURE AIRPORT CHAR.#2 |
| FROM3A 01 1 40 NA DEPARTURE AIRPORT CHAR.#3 |
| 01 2 40 NA DEPARTURE AIRPORT CHAR.#3 |
| FROM4A 01 1 41 NA DEPARTURE AIRPORT CHAR.#4 RIGHTMOST |
| 01 2 41 NA DEPARTURE AIRPORT CHAR.#4 RIGHTMOST |
| FT1 5A 2 177 10 DEG. C FUEL TEMPERATURE LH INNER CELL SYS.2 |
| FT2 5A 2 201 10 DEG. C FUEL TEMPERATURE RH INNER CELL SYS.2 |
| GLA 29 1 100 00 APU GEN LOAD SYS.1 |
| 29 2 100 00 APU GEN LOAD SYS.1 |
| GLE1 29 1 77 01 % GEN1 LOAD SYS.1 |
| 29 2 77 01 GEN1 LOAD SYS.1 |
| GLE2 29 1 77 10 % GEN1 LOAD SYS.2 |
| 29 2 77 10 GEN1 LOAD SYS.2 |
| GLS1 25 1 174 01 DDM ILS1 GLIDESLOPE DEVIATION SYS.1 |
| 25 2 174 01 ILS1 GLIDESLOPE DEVIATION SYS.1 |
| GLS2 25 1 174 10 DDM ILS1 GLIDESLOPE DEVIATION SYS.2 |
| 25 2 174 10 ILS1 GLIDESLOPE DEVIATION SYS.2 |
| GS1 04 1 312 01 KTS IAE GROUND SPEED SYS.1 |
| GS1S 04 1 312 01 KTS IAE GROUND SPEED SYS.1 |
| GS2 04 2 312 10 KTS IAE GROUND SPEED SYS.2 |
| GS2S 04 2 312 10 KTS IAE GROUND SPEED SYS.2 |
| GWKG 02 1 75 00 KG GROSS WEIGHT (KGS.) |
| 02 2 75 00 GROSS WEIGHT (KGS.) |
| GWKG1 02 1 75 00 GROSS WEIGHT (KGS.) SYS.1 |
| GWKG2 02 2 75 00 GROSS WEIGHT (KGS.) sys.2 |
| GWLBS1 02 1 75 00 LBS GROSS WEIGHT (LBS.) SYS.1 |
| 02 2 75 00 GROSS WEIGHT (LBS.) SYS.1 |
| HPT1 7C 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPT1S 7C 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPT2 7C 2 306 10 % SELECTED HPTC POSITION SYS.2 |
| HPT2S 7C 2 306 10 % SELECTED HPTC POSITION SYS.2 |
| HPTSEL1 7C 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPTSEL2 7C 2 306 10 % SELECTED HPTC POSITION SYS.2 |
| ICESW272 5D 2 61 10 DSW ANTI-ICE |
| ICESW27F 5D 2 61 10 DSW ANTI-ICE UNFILTERED |
| ICESW282 5D 2 61 10 DSW ANTI-ICE |
| ICESW28F 5D 2 61 10 DSW ANTI-ICE UNFILTERED |
| IGV 7A 1 130 01 DEG IGV POSITION |
| INSTB121 7E 1 155 00 ACARS INSTALLED SYS.1 |
| INSTBALL 7E 1 155 00 CFDIU LABEL 155 |
| IVV 04 1 365 01 FT/MIN INERTIAL VERTICAL SPEED |
| 04 2 365 10 INERTIAL VERTICAL SPEED |
| IVV01 04 1 365 01 FT/MIN INERTIAL VERTICAL SPEED SYS.1 |
| IVV02 04 2 365 10 FT/MIN INERTIAL VERTICAL SPEED SYS.2 |
| LAF 6C 1 41 01 LOAD ALLEVIATION ACTIVE (LAF) |
| 6C 2 41 10 LOAD ALLEVIATION ACTIVE (LAF) |
| LATA1 29 1 332 01 G LATERAL ACCELERATION SYS.1 |
| 29 2 332 01 LATERAL ACCELERATION SYS.1 |
| LAWB111 6C 1 40 01 NORMAL PITCH LAW |
| 6C 2 40 10 NORMAL PITCH LAW |
| LAWB121 6C 1 40 01 PITCH ALT 1 LAW |
| 6C 2 40 10 PITCH ALT 1 LAW |
| LAWB131 6C 1 40 01 PITCH ALT 2 LAW |
| 6C 2 40 10 PITCH ALT 2 LAW |
| LAWB151 6C 1 40 01 PITCH DIRECT LAW |
| 6C 2 40 10 PITCH DIRECT LAW |
| LCDT 7A 1 74 01 DEG. C BLEED AIR TEMP |
| LCIT 7A 1 110 01 DEG. C LOAD COMPRESSOR INLET TEMPERATURE |
| LDGWALL1 6D 1 21 01 MAIN (LH & RH) LANDING GEAR COMP SYS.1 |
| LDGWB111 6D 1 21 01 MAIN (LH & RH) LANDING GEAR COMP SYS.1 |
| 6D 2 21 10 MAIN (LH & RH) LANDING GEAR COMP SYS.1 |
| LDGWB121 6D 1 21 01 NOSE LANDING GEAR COMPRESSED SYS.1 |
| 6D 2 21 10 NOSE LANDING GEAR COMPRESSED SYS.1 |
| LDGWB131 6D 1 21 01 LH LANDING GEAR COMPRESSED SYS.1 |
| 6D 2 21 10 LH LANDING GEAR COMPRESSED SYS.1 |
| LDGWB141 6D 1 21 01 RH LANDING GEAR COMPRESSED SYS.1 |
| 6D 2 21 10 RH LANDING GEAR COMPRESSED SYS.1 |
| LDGWB151 6D 1 21 01 MAIN (LH & RH) LANDING GEAR DWNLCK SYS.1 |
| LDGWB161 6D 1 21 01 LH BOGIE BEAM NOT ALIGNED SYS.1 |
| LDGWB171 6D 1 21 01 RH BOGIE BEAM NOT ALIGNED SYS.1 |
| LDGWB201 6D 1 21 01 SYSTEM IN CONTROL SYS.1 |
| LDGWB211 6D 1 21 01 L/G RETR SOLENOID SUPPLY -VE SYS.1 |
| LDGWB221 6D 1 21 01 L/G RETR SOLENOID SUPPLY 28 V SYS.1 |
| LDGWB231 6D 1 21 01 L/G EXT SOLENOID SUPPLY -VE SYS.1 |
| LDGWB241 6D 1 21 01 L/G EXT SOLENOID SUPPLY 28 V SYS.1 |
| LDGWB251 6D 1 21 01 DOORS OPEN SOLENOID SPLY -VE SYS.1 |
| LDGWB261 6D 1 21 01 DOORS OPEN SOLENOID SPLY 28 V SYS.1 |
| LDGWB271 6D 1 21 01 DOORS CLOSE SOLENOID SPLY -VE SYS.1 |
| LDGWB281 6D 1 21 01 DOORS CLOSE SOLENOID SPLY 28 V SYS.1 |
| LDGWB291 6D 1 21 01 SYSTEM FAILED SYS.1 |
| LOC1 25 1 173 01 DDM ILS1 LOCALIZER DEVIATION SYS.1 |
| 25 2 173 01 ILS1 LOCALIZER DEVIATION SYS.1 |
| LOC2 25 1 173 10 DDM ILS1 LOCALIZER DEVIATION SYS.2 |
| 25 2 173 10 ILS1 LOCALIZER DEVIATION SYS.2 |
| LONA1 29 1 331 01 G LONGITUDINAL ACCELERATION SYS.1 |
| 29 2 331 01 LONGITUDINAL ACCELERATION SYS.1 |
| LOPP1 6E 1 331 01 DEG LEFT BRAKE PEDAL POSITION SYS.1 |
| LOPP2 6E 2 330 10 DEG LEFT BRAKE PEDAL POSITION SYS.2 |
| LPT1 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPT1S 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPT2 7C 2 307 10 % SELECTED LPTC POSITION SYS.2 |
| LPT2S 7C 2 307 10 % SELECTED LPTC POSITION SYS.2 |
| LPTSEL1 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPTSEL2 7C 2 307 10 % SELECTED LPTC POSITION SYS.2 |
| MN 06 1 205 01 MACH MACH |
| 06 2 205 10 MACH |
| MN1 06 1 205 01 MACH SYS.1 |
| MN1S 06 1 205 01 MACH SYS.1 |
| MN2 06 2 205 10 MACH SYS.2 |
| MN2S 06 2 205 10 MACH SYS.2 |
| MODEB111 26 1 275 01 RUNWAY MODE ACTIVE SYS.1 |
| MODEB121 26 1 275 01 NAV MODE ACTIVE SYS.1 |
| MODEB131 26 1 275 01 LOC CAPT MODE ACTIVE SYS.1 |
| MODEB141 26 1 275 01 LOC TRACK MODE ACTIVE SYS.1 |
| MODEB151 26 1 275 01 ROLL GO AROUND MODE ACTIVE SYS.1 |
| MODEB161 26 1 275 01 HDG MODE ACTICE SYS.1 |
| MODEB171 26 1 275 01 TRACK MODE ACTIVE SYS.1 |
| MW2ALL1 7C 1 351 01 IAE MAINTENANCE DATA #2 |
| MW2All2 7C 2 351 10 IAE MAINTENANCE DATA #2 |
| MW2B291 7C 1 351 01 FUEL OFF WRAPAROUND-FAILED SYS.1 |
| MW2B292 7C 2 351 10 FUEL OFF WRAPAROUND-FAILED SYS.2 |
| N11 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.1 |
| N11S 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.1 |
| N12 7C 2 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.2 |
| N12S 7C 2 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.2 |
| N1C1 7C 1 341 01 % RPM CFM N1 COMMAND SYS.1 |
| N1C2 7C 2 341 10 % RPM CFM N1 COMMAND SYS.2 |
| N1MX1 7C 1 342 01 % RPM N1 MAXIMUM SYS.1 |
| N1MX2 7C 2 342 10 % RPM N1 MAXIMUM SYS.2 |
| N1SEL1 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.1 |
| N1SEL2 7C 2 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS.2 |
| N21 7C 1 344 01 % RPM IAE N2 ACTUAL (HIGH ROTOR SPEED) SYS.1 |
| N21S 7C 1 344 01 % RPM IAE N2 ACTUAL (HIGH ROTOR SPEED) SYS.1 |
| N22 7C 2 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS.2 |
| N22S 7C 2 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS.2 |
| N2SEL1 7C 1 344 01 % RPM IAE N2 ACTUAL (HIGH ROTOR SPEED) SYS.1 |
| N2SEL2 7C 2 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS.2 |
| NA 7A 1 176 01 % RPM RPM |
| OILPRS1 26 1 17 01 ENG 1 OIL LOW PRESSURE |
| 26 2 17 01 ENG 1 OIL LOW PRESSURE |
| OILPRS2 26 1 17 10 ENG 2 OIL PRESSURE |
| 26 2 17 10 ENG 2 OIL PRESSURE |
| OIP1 26 1 317 01 ENG 1 OIL PRESSURE |
| 26 2 317 01 ENG 1 OIL PRESSURE |
| OIP2 26 1 317 10 PSI ENG 2 OIL RPESSURE |
| 26 2 317 10 ENG 2 OIL PRESSURE |
| OIQ1 29 1 73 11 QUART ENG 1 OIL QUANTITY SYS.1 |
| 29 2 73 11 ENG 1 OIL QUANTITY SYS.1 |
| OIQ2 29 1 73 00 QUART ENG 2 OIL QUANTITY SYS.1 |
| 29 2 73 00 ENG 2 OIL QUANTITY SYS.1 |
| QIT1 26 1 316 01 DEG. C ENG 1 OIL TEMPERATURE |
| 26 2 316 01 ENG 1 OIL TEMPERATURE |
| QIT2 26 1 316 10 DEG. C ENG 2 OIL TEMPERATURE |
| 26 2 316 10 ENG 2 OIL TEMPERATURE |
| OTA 7A 1 247 01 DEG. C APU OIL SUMP TEMP |
| OFVP1 5C 1 153 01 % OUTFLOW VALVE POS SYS.1 |
| OFVP2 5C 2 153 10 % OUTFLOW VALVE POS SYS.2 |
| P251 7C 1 262 01 PSIA P2.5 (LPC EXIT PRESSURE) SYS.1 |
| P252 7C 2 262 10 PSIA P2.5 (LPC EXIT PRESSURE) SYS.2 |
| P2A 7A 1 112 01 BAR INLET PRESSURE |
| P31 7C 1 264 01 PSIA PB BURNER PRESSURE SYS.1 |
| P32 7C 2 264 10 PSIA PB BURNER PRESSURE SYS.2 |
| P3SEL1 7C 1 264 01 PSIA PB BURNER PRESSURE SYS.1 |
| P3SEL2 7C 2 264 10 PSIA PB BURNER PRESSURE SYS.2 |
| PBV1 8E 1 112 11 % PACK BYPASS VALVE POSITION SYS.1 |
| PBV2 8E 2 112 00 % PACK BYPASS VALVE POSITION SYS.2 |
| PCSWALL1 5C 1 57 01 PRESSURE CONTROLLER STATUS WORD SYS.1 |
| PCSWALL2 5C 2 57 10 PRESSURE CONTROLLER STATUS WORD SYS.2 |
| PCSWB111 5C 1 57 01 SYSTEM IN CONTROL SYS.1 |
| PCSWB112 5C 2 57 10 SYSTEM IN CONTROL SYS.2 |
| PCSWB141 5C 1 57 01 EXCESSIVE CABIN ALTITUDE-WARN SYS. |
| PDC 5C 1 144 01 PSI CABIN DIFF. PRESSURE SYS.1 |
| 5C 2 144 10 PSI CABIN DIFF. PRESSURE SYS.2 |
| PDC1 5C 1 144 01 PSI CABIN DIFF. PREESURE SYS.1 |
| PDC2 5C 2 144 10 PSI CABIN DIFF. PRESSURE SYS.2 |
| PDE1 6F 1 143 01 PSI PRECOOLER ENG 1 INLET PRESS SYS.1 |
| 6F 2 143 10 PSI PRECOOLER ENG 1 INLET PERSS SYS.1 |
| PDE2 6F 1 142 01 PSI PRECCOLER ENG 2 INLET PRESS SYS.1 |
| 6F 2 142 10 PSI PRECOOLER ENG 2 INLET PRESS SYS.1 |
| PFAD 7A 1 4 01 HEX PERFORMANCE ADJUSTMENTS SYS.1 |
| PFADMSB 7A 1 4 01 HEX PERFORMANCE ADJUSTMENTS SYS.1 |
| PFLKG 8E 1 126 11 KG/SEC PACK FLOW SYS.1 |
| PFRKG 8E 2 126 00 KG/SEC PACK FLOW SYS.2 |
| PHA1 3D 1 226 01 DEG N1 PHASE UNBAL BRG1 OR TRF EN1 SYS.1 |
| PHA2 3D 1 226 10 DEG N1 PHASE UNBAL BRG1 OR TRF EN2 SYS.1 |
| PHASE1 26 1 126 01 FLIGHT PHASES (ACQUIRED) |
| 26 2 126 01 FLIGHT PHASES (ACQUIRED) |
| PHT1 3D 1 226 11 DEG N1 PHASE UNBAL TRF EN1 SYS.1 |
| PHT2 3D 1 226 00 DEG N1 PHASE UNBAL TRF EN2 SYS.2 |
| PO1 7C 1 114 01 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.1 |
| PO2 7C 2 114 10 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.2 |
| POSEL1 7C 1 114 01 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.1 |
| POSEL2 7C 2 114 10 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.2 |
| PS131 7C 1 127 01 PSIA PS13 STATIC AIR PRESSURE AT 1.3 SYS.1 |
| PS132 7C 2 127 10 PSIA PS13 STATIC AIR PRESSURE AT 1.3 SYS.2 |
| PSB1 26 1 320 01 ENG. 1 NO. 4 BEARING PRESSURE (IAE) |
| 26 2 320 01 ENG. 1 NO. 4 BEARING PRESSURE (IAE) |
| PSB2 26 1 320 10 ENG. 2 NO. 4 BEARING PRESSURE (IAE) |
| 26 2 320 10 ENG. 2 NO. 4 BEARING PRESSURE (IAE) |
| PSW1111 8E 1 62 11 FLOW CONTROL VALVE STATUS CLOSE SYS.1 |
| PSW1112 8E 2 62 00 FLOW CONTROL VALVE STATUS CLOSE SYS.2 |
| PSW1131 8E 1 62 11 PACK COMPRESSOR OUTLET TEMP SYS.1 |
| PSW1132 8E 2 62 00 PACK COMPRESSOR OUTLET TEMP SYS.2 |
| PSW1141 8E 1 62 11 PACK COMPRESSOR OUTLET TEMP SYS.1 |
| PSW1142 8E 2 62 00 PACK COMRPESSOR OUTLET TEMP SYS.2 |
| PT 7A 1 166 01 BAR BLEED AIR PRESSURE |
| PT21 7C 1 131 01 PSIA PT2 (FAN INLET PRESSURE) SYS.1 |
| PT21S 7C 1 131 01 PSIA PT2 (FAN INLET PRESSURE) SYS.1 |
| PT22 7C 2 131 10 PSIA PT2 (FAN INLET PRESSURE) SYS.2 |
| PT22S 7C 2 131 10 PSIA PT2 (FAN INLET PRESSURE) SYS.2 |
| PTCH1 04 1 324 01 DEG PITCH ANGLE SYS.1 |
| PTCH2 04 2 324 10 DEG PITCH ANGLE SYS.2 |
| QALT 25 1 203 01 FT ALTITUDE (DAR) |
| 25 2 203 10 FT ALTITUDE (DAR) |
| QAOA1 25 1 221 01 INDICATED ANGLE OF ATTACK SYS.1 |
| QAOA2 25 2 221 10 INDICATED ANGLE OF ATTACK SYS.2 |
| QCAS 25 1 206 01 COMPUTED AIRSPEED |
| 25 2 206 10 COMPUTED AIRSPEED |
| QDBB181 25 1 230 00 SELECTED DATA BASE |
| 25 2 230 00 SELECTED DATA BASE |
| QDBUPD1 25 1 230 01 NAV DATA BASE UPDATE |
| QDBUPDDA 25 1 230 00 DATA BASE DAY |
| 25 2 230 00 DATA BASE DAY |
| QDBUPDMO 25 1 230 00 DATA BASE MONTH |
| 25 2 230 00 DATA BASE MONTH |
| QE1IDLSD 25 1 46 01 ENG 1 ID LSD (FOR QAR RCDG) (CFM & IAE) |
| 25 2 46 01 ENG 1 ID LSD (FOR QAR RCDG) (CFM & IAE) |
| QE1IDMSD 25 1 47 01 ENG 1 ID MSD (FOR QAR RCDG) (IAE ONLY) |
| QE2IDLSD 25 1 46 10 ENG 2 ID LSD (FOR QAR ECDG) (CFM & IAE) |
| QE2IDMSD 25 1 47 10 ENG 2 ID MSD (FOR QAR RCDG) |
| QEPRA1 25 1 340 01 EPR ACTUAL ENGINE 1 |
| 25 2 340 01 EPR ACTUAL ENGINE 1 |
| QEPRA11 25 1 340 01 EPR ACTUAL ENGINE 1 SYS.1 (IAE) |
| QEPRA2 25 1 340 10 EPR ACTUAL ENGINE 2 |
| 25 2 340 10 EPR ACTUAL ENGINE 2 |
| QEPRA21 25 1 340 10 EPR ACTUAL ENGINE 2 SYS.1 (IAE) |
| QEPRC11 25 1 341 01 EPR COMMANDED ENG 1 |
| QEPRC21 25 2 341 01 EPR COMMANDED ENG 2 |
| QEPRT11 25 1 343 01 TARGET EPR ENGINE 1 (IAE) |
| 25 2 343 01 TARGET EPR ENGINE 1 (IAE) |
| QFDIUDB1 17 1 230 01 FDIU DATA BASE UPDATE |
| QFF1 25 1 244 01 FUEL FLOW ENGINE 1 |
| 25 2 244 01 FUEL FLOE ENGINE 1 |
| QFF2 25 1 244 10 FUEL FLOW ENGINE 2 |
| 25 2 244 10 FUEL FLOW ENGINE 2 |
| QFLAP 26 1 137 11 FLAPS POSITION LH |
| 26 2 137 11 FLAPS POSITION LH |
| QFLTPH1 26 1 126 01 FLIGHT PHASE FROM FWC FOR QAR RCDG. |
| QGS 25 1 312 01 GROUND SPEED |
| 25 2 312 10 GROUND SPEED |
| QIAEGT1 25 1 345 01 SELECTED T495 ENGINE 1 |
| 25 2 345 01 SELECTED T495 ENGINE 1 |
| QIAEGT11 25 1 345 01 SELECTED T495 ENGINE 1 SYS.1 (IAE) |
| QIAEGT21 25 1 345 10 SELECTED T495 ENGINE 2 SYS.1 (IAE) |
| QIAN1A1 25 1 346 01 SEL. N1 ACTUAL ENGINE 1 (IAE) |
| 25 2 346 01 SEL. N1 ACTUAL ENGINE 1 (IAE) |
| QIAN1A11 25 1 346 01 SEL. N1 ACTUAL ENGINE 1 SYS.1 (IAE) |
| QIAN1A2 25 1 346 10 SEL. N1 ACTUAL ENGINE 2 |
| 25 2 346 10 SEL. N1 ACTUAL ENGINE 2 |
| QIAN1A21 25 1 346 10 SEL. N1 ACTUAL ENGINE 2 SYS. 1 (IAE) |
| QIAN1C11 25 1 341 01 EPR COMMANDED ENG 1 |
| QIAN2A11 25 1 344 01 SEL. N2 ACTUAL ENGINE 1 SYS.1 (IAE) |
| QIAN2A2 25 1 344 10 SEL. N2 ACTUAL ENGINE 2 |
| 25 2 344 10 SEL. N2 ACTUAL ENGINE 2 |
| QIAN2A21 25 1 344 10 SEL. N2 ACTUAL ENGINE SYS. 1 (IAE) |
| QIATLA11 25 1 133 01 SELECTED TLA ENGINE 1 SYS.1 (IAE) |
| QIATLA21 25 1 133 10 SELECTED TLA ENGINE 2 SYS.1 (IAE) |
| QIAW1141 26 1 11 01 ENG1 POS. INDICATION FAULT SYS.1 (IAE) |
| QIAW1151 26 1 11 01 ENG1 START AIR VALVE POS OPEN SYS.1 |
| QIAW2141 26 1 11 10 ENG2 POS. INDICATION FAULT SYS.1 (IAE) |
| QIAW2151 26 1 11 10 ENG2 START AIR VALVE POS OPEN SYS.1 |
| QIAW3161 26 1 145 01 ENG1 FUEL VALVE POS OFF SYS.1 |
| QIAW4161 26 1 145 10 ENG2 FUEL VALVE POS OFF SYS.1 |
| QILS11 25 1 33 01 ILS 1 FREQUENCY SYS.1 |
| 25 2 33 01 ILS 1 FREQUENCY SYS.1 |
| QILS21 25 1 33 10 ILS 2 FREQUNECY SYS.1 |
| 25 2 33 10 ILS 2 FREQUENCY SYS.1 |
| QINALT1 04 1 361 NA FT INERTIAL ALTITUDE SYS 1 (QAR) |
| QINALT1S 04 1 361 NA FT INERTIAL ALTITUDE SYS 1 (QAR) |
| QINALT2 04 2 361 NA FT INERTIAL ALTITUDE SYS 2 (QAR) |
| QINALT2S 04 2 361 NA FT INERTIAL ALTITUDE SYS 2 (QAR) |
| QLATA1 29 1 332 01 LATERAL ACCELERATION AT 32/SEC |
| QLATP 04 1 310 NA DEG PRESENT POSITION LATITUDE (VARIABLE) |
| 04 2 310 NA DEG PRESENT POSITION LATITUDE (VARIABLE) |
| QLATP1 04 1 310 NA DEG PRESENT POSITION LATITUDE (QAR) |
| QLATP2 04 2 310 NA DEG PRESENT POSITION LATITUDE (QAR) |
| QLDGA291 6D 1 20 01 GEAR LEVER SELECTED DOWN |
| 6D 2 20 10 GEAR LEVER SELECTED DOWN |
| QLDGW111 6D 1 21 01 MAIN (LH & RH) LANDING GEAR COMP SYS.1 (32) |
| QLDGW131 6D 1 21 01 LH LANDING GEAR COMPRESSED SYS.1 (32) |
| QLDGW141 6D 1 21 01 RH LANDING GEAR COMPRESSED SYS.1 (32) |
| QLONA1 29 1 331 01 LONGITUDINAL ACCELERATION AT 32/SEC |
| QLONP 04 1 311 NA DEG PRESENT POSITION LONGITUDE (VARIABLE) |
| 04 2 311 NA DEG PRESENT POSITION LONGITUDE (VARIABLE) |
| QLONP1 04 1 311 NA DEG PRESENT POSITION LONGITUDE (QAR) |
| QLONP2 04 2 311 NA DEG PRESENT POSITION LONGITUDE (QAR) |
| QMH1 25 1 320 01 MAGNETIC HEADING SYS.1 |
| 25 2 320 10 MAGNETIC HEADING SYS.1 |
| QN1T11 25 1 343 01 TARGET N1 ENGINE 1 (IAE) |
| 25 2 343 01 TARGET N1 ENGINE 1 (IAE) |
| QNZ1 04 1 364 01 VERTICAL ACCEL. (FOR LOAD REPORT TRIGGER) |
| QPTCH 25 1 324 01 PITCH ANGLE |
| 25 2 324 10 PITCH ANGLE |
| QPTCHA01 04 1 324 01 PITCH ANGLE (LOAD REPORT TRIG) |
| QPTCR1 04 1 326 01 DEG/SEC BODY AXIS PITCH RATE (LOAD REPORT TRIG) |
| 04 2 326 10 DEG/SEC BODY AXIS PITCH RATE (LOAD REPORT TRIG) |
| QRALT1 25 1 164 01 RADIO HEIGHT (FOR LAOD REPORT TRIGGER) |
| QROLL 25 1 325 01 ROLL ANGLE |
| 25 2 325 10 ROLL ANGLE |
| QROLLA01 04 1 325 01 ROLL ANGLE SYS.1 (LOAD REPORT TRIGGER) |
| QROLR1 04 1 327 01 DEG/SEC BODY AXIS ROLL RATE (LOAD REPORT TRIG) |
| QRUDP 26 1 304 01 RUDDER PEDAL POSITION |
| 26 2 304 01 RUDDER PEDAL POSITION |
| QSPCP 26 1 305 01 PITCH CAPT CMD POSITION |
| 26 2 304 01 PITCH CAPT CMD POSITION |
| QSPCR 26 1 301 01 ROLL CAPT CMD POSITION |
| 26 2 301 01 ROLL CAPT CMD POSITION |
| QSPFP 26 1 306 01 PITCH F/O CMD POSITION |
| 26 2 306 01 PITCH F/O CMD POSITION |
| QSPFR 26 1 302 01 ROLL F/O CMD POSITION |
| 26 2 302 01 ROLL F/O CMD POSITION |
| QSTAB1 26 1 315 01 STABILIZER POSITION 1 |
| 26 2 315 01 STABILIZER POSITION 1 |
| QSW10111 25 1 302 01 CLIMB SYS.1 |
| 25 2 302 10 CLIMB SYS.1 |
| QSW10121 25 1 302 01 DECENT SYS.1 |
| 25 2 302 10 DECENT SYS.1 |
| QSW10131 25 1 302 01 IMMEDIATE SYS.1 |
| 25 2 302 10 IMMEDIATE SYS.1 |
| QSW10141 25 1 302 01 OPEN SYS.1 |
| 25 2 302 10 OPEN SYS.1 |
| QSW10151 25 1 302 01 PITCH TRACK OFF SYS.1 |
| 25 2 302 10 PITCH TRACK OFF SYS.1 |
| QSW10161 25 1 302 01 PITCH GO AROUND MODE SYS.1 |
| 25 2 302 10 PITCH GO AROUND MODE SYS.1 |
| QSW10171 25 1 302 01 VERTICAL SPEED MODE SYS.1 |
| 25 2 302 10 VERTICAL SPEED MODE SYS.1 |
| QSW10181 25 1 302 01 FPA MODE SYS.1 |
| 25 2 302 10 FPA MODE SYS.1 |
| QSW10191 25 1 302 01 ALT MODE SYS.1 |
| 25 2 302 10 ALT MODE SYS.1 |
| QSW10192 25 2 302 10 ALT MODE SYS.2 |
| QSW10201 25 1 302 01 TRK SYS.1 |
| 25 2 302 10 TRK SYS.1 |
| QSW10202 25 2 302 10 TRK SYS.2 |
| QSW10211 25 1 302 01 CAPT SYS.1 |
| 25 2 302 10 CAPT SYS.1 |
| QSW10212 25 2 302 10 CAPT SYS.2 |
| QSW10221 25 1 302 01 G/S SYS.1 |
| 25 2 302 10 G/S SYS.1 |
| QSW10222 25 2 302 10 G/S SYS.2 |
| QSW10231 25 1 302 01 FINAL DESCENT MODE SYS.1 |
| 25 2 302 10 FINAL DESCENT MODE SYS.1 |
| QSW10241 25 1 302 01 EXPEDITE MODE SYS.1 |
| 25 2 302 10 EXPEDITE MODE SYS.1 |
| QSW10251 25 1 302 01 FLARE MODE SYS.1 |
| 25 2 302 10 FLARE MODE SYS.1 |
| QSW11181 25 1 305 01 METRIC/ENGLISH SYSTEM (WEIGHT) |
| 25 2 305 10 METRIC/ENGLISH SYSTEM (WEIGHT) |
| QSW11271 25 1 305 01 METRIC/ENGLISH SYSTEM (DEGREES) |
| 25 2 305 10 METRIC/ENGLISH SYSTEM (DEGREES) |
| QSW11281 25 1 305 01 NO DATA FROM EEC1 SYS.1 (IAE) |
| 25 2 305 10 NO DATA FROM EEC1 SYS.1 (IAE) |
| QSW11291 25 1 305 01 NO DATA FROM EEC2 SYS.1 (IAE) |
| 25 2 305 10 NO DATA FROM EEC2 SYS.1 (IAE) |
| QSW1B111 25 1 270 01 ENG 1 REV UNLOCK (AMBER) SYS.1 |
| 25 2 270 10 ENG 1 REV UNLOCK (AMBER) SYS.1 |
| QSW1B121 25 1 270 01 ENG 2 REV UNLOCK (AMBER) SYS.1 |
| 25 2 270 10 ENG 2 REV UNLOCK (AMBER) SYS.1 |
| QSW1B131 25 1 270 01 ENG 1 REV DEPLOYED (GREEN) SYS.1 |
| 25 2 270 10 ENG 1 REV DEPLOYED (GREEN) SYS.1 |
| QSW1B141 25 1 270 01 ENG 2 REV DEPLOYED (GREEN) SYS.1 |
| 25 2 270 10 ENG 2 REV DEPLOYED (GREEN) SYS.1 |
| QSW1B151 25 1 270 01 ECAM DU 1 ANOMALY SYS.1 |
| 25 2 270 10 ECAM DU 1 ANOMALY SYS.1 |
| QSW1B161 25 1 270 01 ECAM DU 2 ANOMALY SYS.1 |
| 25 2 270 10 ECAM DU 2 ANOMALY SYS.1 |
| QSW1B171 25 1 270 01 SPOILER 1 POSITION VALIDITY SYS.1 |
| 25 2 270 10 SPOILER 1 POSITION VALIDITY SYS.1 |
| QSW1B181 25 1 270 01 SPOILER 2 POSITION VALIDITY SYS.1 |
| 25 2 270 10 SPOILER 2 POSITION VALIDITY SYS.1 |
| QSW1B191 25 1 270 01 SPOILER 3 POSITION VALIDITY SYS.1 |
| 25 2 270 10 SPOILER 3 POSITION VALIDITY SYS.1 |
| QSW1B201 25 1 270 01 SPOILER 4 POSITION VALIDITY SYS.1 |
| 25 2 270 10 SPOILER 4 POSITION VALIDITY SYS.1 |
| QSW1B211 25 1 270 01 SPOILER 5 POSITION VALIDITY SYS.1 |
| 25 2 270 10 SPOILER 5 POSITION VALIDITY SYS.1 |
| QSW1B241 25 1 270 01 AUTO LAND WARNING |
| 25 2 270 10 AUTO LAND WARNING |
| QSW1B251 25 1 270 01 ECU1 CHANNEL B IN CONTROL SYS.1 |
| 25 2 270 10 ECU1 CHANNEL B IN CONTROL SYS.1 |
| QSW1B261 25 1 270 01 ECU2 CHANNEL B IN CONTROL SYS.1 |
| 25 2 270 10 ECU2 CHANNEL B IN CONTROL SYS.1 |
| QSW20111 26 1 53 01 LAVATORY SMOKE DETECTED SYS.1 |
| 26 2 53 01 LAVATORY SMOKE DETECTED SYS.1 |
| QSW20161 26 1 16 01 AVIONICS SMOKE DETECTED SYS.1 |
| 26 2 16 01 AVIONICS SMOKE DETECTED SYS.1 |
| QSW20181 26 1 16 01 GPWS MODES ON SYS.1 |
| 26 2 16 01 GPWS MODES ON SYS.1 |
| QSW20281 26 1 51 01 FWD CARGO SMOKE DETECTED SYS.1 |
| 26 2 51 01 FWD CARGO SMOKE DETECTED SYS.1 |
| QSW21181 26 1 16 10 G/S VISUAL ALERT ON SYS.1 |
| 26 2 16 10 G(S VISUAL ALERT ON SYS.1 |
| QSW23121 26 1 21 01 NOSE LANDING GEAR COMPRESSED SYS.1 |
| 26 2 21 01 NOSE LANDING EGAR COMPRESSED SYS.1 |
| QSW23131 26 1 21 01 LH LANDING GEAR COMPRESSED SYS.1 |
| 26 2 21 01 LH LANDING GEAR COMPRESSED SYS.1 |
| QSW23141 26 1 21 01 RH LANDING GEAR COMPRESSED SYS.1 |
| 26 2 21 01 RH LANDING GEAR COMPRESSED SYS.1 |
| QSW24141 26 1 22 01 GEAR LEVER SELECTED UP SYS.1 |
| 26 2 22 01 GEAR LEVER SELECTED UP SYS.1 |
| QSW25191 26 1 40 01 ELAC1 PITCH FAULT SYS.1 |
| 26 2 40 01 ELAC1 PITCH FAULT SYS.1 |
| QSW25201 26 1 40 01 ELAC1 ROLL FAULT SYS.1 |
| 26 2 40 01 ELAC1 ROLL FAULT SYS.1 |
| QSW25211 26 1 40 01 ELAC2 PITCH FAULT SYS.1 |
| 26 2 40 01 ELAC2 PITCH FAULT SYS.1 |
| QSW25221 26 1 40 01 ELAC2 ROLL FAULT SYS.1 |
| 26 2 40 01 ELAC2 ROLL FAULT SYS.1 |
| QSW25231 26 1 40 01 ELAC1 FAULT SYS.1 |
| 26 2 40 01 ELAC1 FAULT SYS.1 |
| QSW25241 26 1 40 01 ELAC2 FAULT SYS.1 |
| 26 2 40 01 ELAC2 FAULT SYS.1 |
| QSW25251 26 1 40 01 SEC1 FAULT SYS.1 |
| 26 2 40 01 SEC1 FAULT SYS.1 |
| QSW25261 26 1 40 01 SEC2 FAULT SYS.1 |
| 26 2 40 01 SEC2 FAULT SYS.1 |
| QSW25291 26 1 40 01 SEC3 FAULT SYS.1 |
| 26 2 40 01 SEC3 FAULT SYS.1 |
| QSW26281 26 1 41 01 CAPT SIDESTICK INOPERATIVE SYS.1 |
| 26 2 41 01 CAPT SIDESTICK INOPERATIVE SYS.1 |
| QSW26291 26 1 41 01 F/O SIDESTICK INOPERATIVE SYS.1 |
| 26 2 41 01 F/O SIDESTICK INOPERATIVE SYS.1 |
| QSW27111 26 1 42 01 LH AIL BLUE AVAIL SYS.1 |
| 26 2 42 01 LH AIL BLUE AVAIL SYS.1 |
| QSW27121 26 1 42 01 LH AIL GREEN AVAIL SYS.1 |
| 26 2 42 01 LH AIL GREEN AVAIL SYS.1 |
| QSW27131 26 1 42 01 RH AIL GREEN AVAIL SYS.1 |
| 26 2 42 01 RH AIL GREEN AVAIL SYS.1 |
| QSW27141 26 1 42 01 RH AIL BLUE AVAIL SYS.1 |
| 26 2 42 01 RH AIL BLUE AVAIL SYS.1 |
| QSW28111 26 1 43 01 LEFT SPOILER 1 OUT SYS.1 |
| 26 2 43 01 LEFT SPOILER 1 OUT SYS.1 |
| QSW28121 26 1 43 01 RIGHT SPOILER 1 OUT SYS.1 |
| 26 2 43 01 RIGHT SPOILER 1 OUT SYS.1 |
| QSW28271 26 1 43 01 GROUND SPOILER ARMED SYS.1 |
| 26 2 43 01 GROUND SPOILER ARMED SYS.1 |
| QSW2B151 25 1 271 01 ATS ENGAGED SYS.1 |
| 25 2 271 10 ATS ENGAGED SYS.1 |
| QSW2B161 25 1 271 01 ATS ACTIVE SYS.1 |
| 25 2 271 10 ATS ACTIVE SYS.1 |
| QSW2B171 25 1 271 01 ATS SPEED MACH MODE SYS.1 |
| 25 2 271 10 ATS SPEED MACH MODE SYS.1 |
| QSW2B181 25 1 271 01 ATS RETARD MODE ACTIVATED SYS.1 |
| 25 2 271 10 ATS RETARD MODE ACTIVATED SYS.1 |
| QSW2B191 25 1 271 01 THRUST N1 MODE (CFMI ENGINES) SYS.1 |
| 25 2 271 10 THRUST N1 MODE (CFMI ENGINES) SYS.1 |
| QSW2B201 25 1 271 01 THRUST EPR MODE (IAE ENGINES) SYS.1 |
| 25 2 271 10 THRUST EPR MODE (IAE ENGINES) SYS.1 |
| QSW2B211 25 1 271 01 ATS ALPHA FLOOR |
| 25 2 271 10 ATS ALPHA FLOOR |
| QSW2B251 25 1 271 01 HEADING SELECTION SYS.1 |
| 25 2 271 10 HEADING SELECTION SYS.1 |
| QSW30181 29 1 1 00 RH WING ANTI-ICE VALVE CLOSED SYS.1 |
| 29 2 1 00 RH WING ANTI-ICE VALVE CLOSED SYS.1 |
| QSW3018F 29 1 1 00 RH WING ANTI-ICE VALVE CLOSED UNFILTERED |
| 29 2 1 00 RH WING ANTI-ICE VALVE CLOSED UNFILTERED |
| QSW30191 29 1 1 00 ENG2 ANTI ICE VALVE FAULT SYS.1 |
| 29 2 1 00 ENG2 ANTI ICE VALVE FAULT SYS.1 |
| QSW31181 29 1 1 11 LH WING ANTI-ICE VALVE CLOSED SYS.1 |
| 29 2 1 11 LH WING ANTI-ICE VALVE CLOSED SYS.1 |
| QSW3118F 29 1 1 11 LH WING ANTI-ICE VALVE CLOSED UNFILTERED |
| 29 2 1 11 LH WING ANTI-ICE VALVE CLOSED UNFILTERED |
| QSW31191 29 1 1 11 ENG1 ANTI-ICE VALVE FAULT SYS.1 |
| 29 2 1 11 ENG1 ANTI-ICE VALVE FAULT SYS.1 |
| QSW33281 29 1 2 01 HF1 EMITTING SYS.1 |
| 29 2 2 01 HF1 EMITTING SYS.1 |
| QSW33291 29 1 2 01 VHF1 EMITTING SYS.1 |
| 29 2 2 01 VHF1 EMITTING SYS.1 |
| QSW34201 29 1 2 10 AC2 BUS OFF SYS.1 |
| 29 2 2 10 AC2 BUS OFF SYS.1 |
| QSW34281 29 1 2 10 HF2 EMITTING SYS.1 |
| 29 2 2 10 HF2 EMITTING SYS.1 |
| QSW34291 29 1 2 10 VHF2 EMITTING SYS.1 |
| 29 2 2 10 VHF2 EMITTING SYS.1 |
| QSW35161 29 1 2 11 APU MASTER SWITCH P/B OFF SYS.1 |
| QSW35291 29 1 2 11 VHF3 EMITTING SYS.1 |
| 29 2 2 11 VHF3 EMITTING SYS.1 |
| QSW36181 29 1 3 01 ENG1 ANTI ICE P/B ON SYS.1 |
| 29 2 3 01 ENG1 ANTI ICE P/B ON SYS.1 |
| QSW36211 29 1 3 01 PACK 1 FLOW CTL VALVE NOT CLOSED |
| 29 2 3 01 PACK 1 FLOW CTL VALVE NOT CLOSED |
| QSW36212 29 1 3 10 PACK 2 FLOW CTL VALVE NOT CLOSED |
| 29 2 3 10 PACK 2 FLOW CTL VALVE NOT CLOSED |
| QSW36221 29 1 3 11 WING ANTI-ICE P/B OFF SYS.1 |
| 29 2 3 11 WING ANTI-ICE P/B OFF SYS.1 |
| QSW37181 29 1 3 10 ENG2 ANTI-ICE P/B ON SYS.1 |
| 29 2 3 10 ENG2 ANTI-ICE P/B ON SYS.1 |
| QSW38291 29 1 4 01 DC1 BUS OFF SYS.1 |
| 29 2 4 01 DC1 BUS OFF SYS.1 |
| QSW39291 29 1 4 10 DC2 BUS OFF SYS.1 |
| 29 2 4 10 DC2 BUS OFF SYS.1 |
| QSW3B161 25 1 272 01 DMC MARK2 IDENT SYS.1 |
| 25 2 272 10 DMC MARK2 IDENT SYS.1 |
| QSW3B221 25 1 272 01 DMC1 INVALID |
| 25 2 272 10 DMC1 INVALID |
| QSW3B231 25 1 272 01 DMC2 INVALID |
| 25 2 272 10 DMC2 INVALID |
| QSW3B241 25 1 272 01 DMC3 INVALID |
| 25 2 272 10 DMC3 INVALID |
| QSW3B251 25 1 272 01 DMC3 XFR SYS.1 |
| QSW3B252 25 2 272 10 DMC3 XFR SYS.2 |
| QSW3B261 25 1 272 01 PFD/ND XFR SYS.1 |
| QSW3B262 25 2 272 10 PFD/ND XFR SYS.2 |
| QSW3B271 25 1 272 01 ECAM/ND XFR SYS.1 |
| QSW3B272 25 2 272 10 ECAM/ND XFR SYS.2 |
| QSW42161 29 1 55 01 XFEED VALVE FULLY CLOSED SYS.1 |
| 29 2 55 01 XFEED VALVE FULLY CLOSED SYS.1 |
| QSW42162 29 1 55 10 XFEED VALVE FULLY CLOSED SYS.2 |
| 29 2 55 10 XFEED VALVE FULLY CLOSED SYS.2 |
| QSW43111 29 1 67 01 ENG1 OPV NOT FULLY OPEN |
| 29 2 67 01 ENG1 OPV NOT FULLY OPEN |
| QSW43112 29 1 66 01 ENG2 OPV NOT FULLY OPEN |
| QSW43151 29 1 66 01 ENG2 HP VALVE FULLY CLOSED SYS.1 |
| 29 2 66 01 ENG2 HP VALVE FULLY CLOSED SYS.1 |
| QSW43171 29 1 66 01 ENG2 PRESS REG VALVE FULLY CLOSED SYS.1 |
| 29 2 66 01 ENG2 PRESS REG VALVE FULLY CLOSED SYS.1 |
| QSW43211 29 1 66 01 ENG2 STARTER VALVE NOT CLOSED SYS.1 |
| 29 2 66 01 ENG2 STARTER VALVE NOT CLOSED SYS.1 |
| QSW44151 29 1 67 01 ENG1 HP VALVE FULLY CLOSED SYS.1 |
| 29 2 67 01 ENG1 HP VALVE FULLY CLOSED SYS.1 |
| QSW44171 29 1 67 01 ENG1 PRESS REG VALVE FULLY CLOSED SYS.1 |
| 29 2 67 01 ENG1 PRESS REG VALVE FULLY CLOSED SYS.1 |
| QSW44211 29 1 67 01 ENG1 STARTER VALVE NOT CLOSED SYS.1 |
| 29 2 67 01 ENG1 STARTER VALVE NOT CLOSED SYS.1 |
| QSW4B111 25 1 273 01 PLAN MODE SYS.1 |
| QSW4B112 25 2 273 10 PLAN MODE SYS.2 |
| QSW4B121 25 1 273 01 ARC SYS.1 |
| QSW4B122 25 2 273 10 ARC SYS.2 |
| QSW4B131 25 1 273 01 ROSE - NAV SYS.1 |
| QSW4B132 25 2 273 10 ROSE - NAV SYS.2 |
| QSW4B141 25 1 273 01 ROSE - VOR SYS.1 |
| QSW4B142 25 2 273 10 ROSE - VOR SYS.2 |
| QSW4B151 25 1 273 01 ROSE - ILS SYS.1 |
| QSW4B152 25 2 273 10 ROSE - ILS SYS.2 |
| QSW4B161 25 1 273 01 10 NM RANGE SYS.1 |
| QSW4B162 25 2 273 10 10 NM RANGE SYS.2 |
| QSW4B171 25 1 273 01 20 NM RANGE SYS.1 |
| QSW4B172 25 2 273 10 20 NM RANGE SYS.2 |
| QSW4B181 25 1 273 01 40 NM RANGE SYS.1 |
| QSW4B182 25 2 273 10 40 NM RANGE SYS.2 |
| QSW4B191 25 1 273 01 80 NM RANGE SYS.1 |
| QSW4B192 25 2 273 10 80 NM RANGE SYS.2 |
| QSW4B201 25 1 273 01 160 NM RANGE SYS.1 |
| QSW4B202 25 2 273 10 160 NM RANGE SYS.2 |
| QSW5B111 25 1 274 01 ND1 ANOMALY/OFF |
| QSW5B112 25 2 274 10 ND1 ANOMALY/OFF |
| QSW5B131 25 1 274 01 OUTER MARKER SYS.1 |
| 25 2 274 10 OUTER MARKER SYS.1 |
| QSW5B141 25 1 274 01 MIDDLE MARKER SYS.1 |
| 25 2 274 10 MIDDLE MARKER SYS.1 |
| QSW5B151 25 1 274 01 INNER MARKER (AIRWAYS) SYS.1 |
| 25 2 274 10 INNER AMRKER (AIRWAYS) SYS.1 |
| QSW6B111 25 1 275 01 CRUISE IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 CRUISE IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B121 25 1 275 01 ENG IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 ENG IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B131 25 1 275 01 BLEED IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 BLEED IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B141 25 1 275 01 PRESS IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 PRESS IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B151 25 1 275 01 HYD IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 HYD IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B161 25 1 275 01 ELEC IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 ELEC IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B171 25 1 275 01 FUEL IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 FUEL IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B181 25 1 275 01 APU IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 APU IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B191 25 1 275 01 COND IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 COND IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B201 25 1 275 01 DOOR IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 DOOR IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B211 25 1 275 01 F/CTL IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 F/CTL IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B221 25 1 275 01 WHEEL IMAGE DISPL OR ADV IN MONO SYS.1 |
| 25 2 275 10 WHELL IMAGE DISPL OR ADV IN MONO SYS.1 |
| QSW6B261 25 1 275 01 STATUS IMAGE DISPLAYED SYS.1 |
| 25 2 275 10 STATUS IMAGE DISPLAYED SYS.1 |
| QSW7B131 25 1 276 01 AP1 ENGAGED SYS.1 |
| 25 2 276 10 AP1 ENGAGED SYS.1 |
| QSW7B141 25 1 276 01 AP2 ENGAGED SYS.1 |
| 25 2 276 10 AP2 ENGAGED SYS.1 |
| QSW7B151 25 1 276 01 FD1 ENGAGED SYS.1 |
| 25 2 276 10 FD1 ENGAEGD SYS.1 |
| QSW7B161 25 1 276 01 FD2 ENGAGED SYS.1 |
| 25 2 276 10 FD2 ENGAGED SYS.1 |
| QSW7B221 25 1 276 01 PFD1 ANOMALY/OFF |
| QSW7B222 25 2 276 10 PFD1 ANOMALY/OFF |
| QSW7B261 25 1 276 01 ALT STD QNH QFE |
| 25 2 276 10 ALT STD QNH QFE |
| QSW7B271 25 1 276 01 ALT BARO SETTING CAPT COARSE |
| QSW7B272 25 2 276 10 ALT BARO SETTING F/O COARSE |
| QSW8B141 25 1 300 01 LAND TRACK MODE ACTIVE SYS.1 |
| 25 2 300 10 LAND TRACK MODE ACTICE SYS.1 |
| QTAT 25 1 211 01 TOTAL AIR TEMPERATURE |
| 25 2 211 10 TOTAL AIR TEMPERATURE |
| QTHDG 04 1 314 01 TRUE HEADING (DAR) |
| 04 2 314 10 TRUE HEADING (DAR) |
| QVOR11 25 1 34 01 VOR 1 FREQUENCY SYS.1 |
| 25 2 34 01 VOR 1 FREQUENCY SYS.1 |
| QVOR21 25 1 34 10 VOR 2 FREQUENCY SYS.1 |
| 25 2 34 10 VOR 2 FREQUENCY SYS.1 |
| QVRTA1 29 1 333 01 G NORMAL ACCELERATION AT 32/SEC |
| QVZBI1 04 1 365 01 INERTIAL VERTICAL SPEED (LOAD RPT TRIG) |
| QYAW01 04 1 330 01 BODY AXIS YAM RATE (LOAD REPORT TRIG) |
| RALT1 25 1 164 01 FT RADIO HEIGHT (R/A1) SYS.1 |
| 25 2 164 01 FT RADIO HEIGHT (R/A1) SYS.1 |
| RALT2 25 1 164 10 FT RADIO HEIGHT (R/A1) SYS.2 |
| 25 2 164 10 FT RADIO HEIGHT (R/A1) SYS.2 |
| RI1 8E 1 130 11 % PACK RAM AIR INLET POSITION SYS.1 |
| RI2 8E 2 130 00 % PACK RAM AIR INLET POSITION SYS.2 |
| RO1 8E 1 124 11 % PACK RAM AIR OUTLET POS. SYS.1 |
| RO2 8E 2 124 00 % PACK RAM AIR OUTLET POS. SYS.2 |
| ROLL 04 1 325 01 DEG ROLL ANGLE SYS.1 |
| 04 2 325 10 DEG ROLL ANGLE SYS.2 |
| ROLLR1 04 1 337 01 DEG ROLL ATTITUDE RATE |
| 04 2 337 10 DEG ROLL ATTITUDE RATE |
| ROLLS 04 1 325 01 DEG ROLL ANGLE SYS.1 |
| 04 2 325 10 DEG ROLL ANGLE SYS.2 |
| ROPP1 6E 1 330 01 DEG RIGHT BRAKE PEDAL POSITION SYS.1 |
| ROPP2 6E 2 330 10 DEG RIGHT BRAKE PEDAL POSITION SYS.2 |
| RSP21 6C 1 362 01 DEG LH SPL 2 POSITION SYS.1 |
| 6C 2 362 10 DEG LH SPL 2 POSITION SYS.1 |
| RSP22 6C 1 372 01 DEG RH SPL 2 POSITION SYS.2 |
| 6C 2 372 10 DEG RH SPL 2 POSITION SYS.2 |
| RSP31 6C 1 363 01 DEG LH SPL 3 POSITION SYS.1 |
| 6C 2 363 10 DEG LH SPL 3 POSITION SYS.1 |
| RSP32 6C 1 373 01 DEG RH SPL 3 POSITION SYS.2 |
| 6C 2 373 10 DEG RH SPL 3 POSITION SYS.2 |
| RSP41 6C 1 364 01 DEG LH SPL 4 POSITION SYS.1 |
| 6C 2 364 10 DEG LH SPL 4 POSITION SYS.1 |
| RSP42 6C 1 374 01 DEG RH SPL 4 POSITION SYS.2 |
| 6C 2 374 10 DEG RH SPL 4 POSITION SYS.2 |
| RSP4FLT 6C 1 44 01 1 SPOILER 4 FAULT |
| 6C 2 44 10 1 SPOILER 4 FAULT |
| RSP51 6C 1 365 01 DEG LH SPL 5 POSITION SYS.1 |
| 6C 2 365 10 DEG LH SPL 5 POSITION SYS.1 |
| RSP52 6C 1 375 01 DEG RH SPL 5 POSITION SYS.2 |
| 6C 2 375 10 DEG RH SPL 5 POSITION SYS.2 |
| RSP5FLT 6C 1 44 01 1 SPOILER 5 FAULT |
| 6C 2 44 10 1 SPOILER 5 FAULT |
| RUDD 29 1 312 00 DEG RUDDER POSITION SYS.1 |
| 29 2 312 00 DEG RUDDER POSITION SYS.1 |
| RUDT 0A 1 313 00 DEG RUDDER TRIM SYS.1 |
| 0A 2 313 00 DEG RUDDER TRIM SYS.1 |
| SAT 06 1 213 01 DEG. C STATIC AIR TEMPERATURE (BNR) |
| 06 2 213 10 DEG. C STATIC AIR TEMPERATURE (BNR) |
| SC1C 29 1 242 01 DEG. C SELECTED CKPT COMPT TEMP SYS.1 |
| 29 2 242 01 DEG. C SELECTED CKPT COMPT TEMP SYS.1 |
| SC2C 29 1 244 01 DEG. C SEL FWD CAB COMPT TEMP SYS.1 |
| 29 2 244 01 DEG. C SEL FWD CAB COMPT TEMP SYS.1 |
| SC3C 29 1 245 01 DEG. C SEL AFT CAB COMPT TEMP SYS.1 |
| 29 2 245 01 DEG. C SEL AFT CAB COMPT TEMP SYS.1 |
| SDS1B161 29 1 1 01 ENG1 OIL FILTER CLOGGED SYS.1 |
| 29 2 1 01 ENG1 OIL FILTER CLOGGED SYS.1 |
| SDS1B162 29 1 1 10 ENG1 OIL FILTER CLOGGED SYS.2 |
| 29 2 1 10 ENG1 OIL FILTER CLOGGED SYS.2 |
| SDS1B171 29 1 1 01 ENG1 FUEL FILTER CLOGGED SYS.1 |
| 29 2 1 01 ENG1 FUEL FILTER CLOGGED SYS.1 |
| SDS1B172 29 1 1 10 ENG1 FUEL FILTER CLOGGED SYS.2 |
| 29 2 1 10 ENG1 FUEL FILTER CLOGGED SYS.2 |
| SDS1B191 29 1 1 01 FUEL FIRE VALVE ENG1 FC SYS.1 |
| 29 2 1 01 FUEL FIRE VALVE ENG1 FC SYS.1 |
| SDS1B192 29 1 1 10 FUEL FIRE VALVE ENG2 FC SYS.1 |
| 29 2 1 10 FUEL FIRE VALVE ENG2 FC SYS.1 |
| SELMACH1 25 1 106 01 SELECTED MACH/MANUAL |
| 25 2 106 10 SELECTED MACH/MANUAL |
| SELSPD 01 1 103 00 PFD SELECTED SPEED |
| 01 2 103 00 PFD SELECTED SPEED |
| SLAT 1B 1 127 01 DEG SLAT ACTUAL POSITION |
| 1B 2 127 10 DEG SLAT ACTUAL POSITION |
| SLATINT1 1B 1 127 01 DEG SLAT ACTUAL POSITION SYS.1 (LEFT) |
| SLATINT2 1B 2 127 10 DEG SLAT ACTUAL POSITION SYS.2 (RIGHT) |
| SLHDG1 25 1 101 01 DEG SELECTED HEADING |
| 25 2 101 10 DEG SELECTED HEADING |
| SLP1 0A 1 226 00 DEG ESTIMD SIDESLIP SYS.1 |
| SLP2 0A 2 226 00 DEG ESTIMD SIDESLIP SYS.2 |
| SLTRK1 25 1 114 01 DEG SELECTED TRACK |
| 25 2 114 10 DEG SELECTED TRACK |
| SPDBRK1 6C 1 43 01 SPEED BRAKE COMMAND SYS.1 |
| 6C 2 43 10 SPEED BRAKE COMMAND SYS.1 |
| SPEED171 01 1 145 00 SPEED/MACH SELECTION SYS.1 |
| 01 2 145 00 SPEED/MACH SELECTION SYS.1 |
| SPEED191 01 1 145 00 AUTO SPEED CONTROL SYS.1 |
| 01 2 145 00 AUTO SPEED CONTROL SYS.1 |
| SPLRB111 6C 1 43 01 LH SPOILER 1 OUT SYS.1 |
| 6C 2 43 10 LH SPOILER 1 OUT SYS.1 |
| SPLRB121 6C 1 43 01 RH SPOILER 1 OUT SYS.1 |
| 6C 2 43 10 RH SPOILER 1 OUT SYS.1 |
| SPLRB271 6C 1 43 01 GROUND SPOILER ARMED SYS.1 |
| 6C 2 43 10 GROUND SPOILER ARMED SYS.1 |
| STAB 6C 1 315 01 DEG STABILIZER POSITION #1 SYS.1 |
| 6C 2 315 10 DEG STABILIZER POSITION #1 SYS.1 |
| SW1ALL1 7C 1 270 01 IAE DISCRETE STATUS WORD #1 |
| SW1ALL2 7C 2 270 10 IAE DISCRETE STATUS WORD #1 |
| SW1B111 7C 1 270 01 IGNITION 1 PRIMARY SELECTED SYS.1 |
| SW1B112 7C 2 270 10 IGNITION 1 PRIMARY SELECTED SYS.2 |
| SW1B131 7C 1 270 01 SAV OPEN LOCAL SWITCH SYS.1 |
| SW1B132 7C 2 270 10 SAV OPEN LOCAL SWITCH SYS.2 |
| SW1B141 7C 1 270 01 ENGINE POS. IND. - FAILED SYS.1 |
| SW1B142 7C 2 270 10 ENGINE POS. IND. - FAILED SYS.2 |
| SW1B151 7C 1 270 01 SAV NOT CLOSED SYS.1 |
| SW1B152 7C 2 270 10 SAV NOT CLOSED SYS.2 |
| SW1B161 7C 1 270 01 AUTO DEPOWER - SELECTED SYS.1 |
| SW1B162 7C 2 270 10 AUTO DEPOWER - SELECTED SYS.2 |
| SW1B171 7C 1 270 01 MANUAL THRUST MODE - ACTIVE SYS.1 |
| SW1B172 7C 2 270 10 MANUAL THRUST MODE - ACTIVE SYS.2 |
| SW1B181 7C 1 270 01 N1 BACKUP MODE - ENGAGED SYS.1 |
| SW1B182 7C 2 270 10 N1 BACKUP MODE - ENGAGED SYS.2 |
| SW1B191 7C 1 270 01 REVERSER SYSTEM FAILED SYS.1 |
| SW1B192 7C 2 270 10 REVERSER SYSTEM FAILED SYS.2 |
| SW1B201 7C 1 270 01 AUTOTHRUST MODE ACTIVATED SYS.1 |
| SW1B202 7C 2 270 10 AUTOTHRUST MODE ACTIVATED SYS.2 |
| SW1B211 7C 1 270 01 2.5 BLEED FAILSAFED - FAILSAFE SYS.1 |
| SW1B212 7C 2 270 10 2.5 BLEED FAILSAFED - FAILSAFE SYS.2 |
| SW1B221 7C 1 270 01 MEMO MODE ACTIVATED SYS.1 |
| SW1B222 7C 2 270 10 MEMO MODE ACTIVATED SYS.2 |
| SW1B231 7C 1 270 01 AUTOTHRUST TRA LIMITED SYS.1 |
| SW1B232 7C 2 270 10 AUTOTHRUST TRA LIMITED SYS.2 |
| SW1B241 7C 1 270 01 CHANNEL CONTROL - IN CONTROL SYS.1 |
| SW1B242 7C 2 270 10 CHANNEL CONTROL - IN CONTROL SYS.2 |
| SW1B251 7C 1 270 01 FLEX TAKEOFF MODE ENGAGED SYS.1 |
| SW1B252 7C 2 270 10 FLEX TAKEOFF MODE ENGAGED SYS.2 |
| SW1B261 7C 1 270 01 OIL COOLING SYSTEM - FAILED SYS.1 |
| SW1B262 7C 2 270 10 OIL COOLING SYSTEM - FAILED SYS.2 |
| SW1B281 7C 1 270 01 50% THRUST LIMIT ACTIVE SYS.1 |
| SW1B282 7C 2 270 10 ENGINE NOT RUNNING SYS.2 |
| SW3191 7C 1 273 01 START MODE SYS.1 |
| SW3192 7C 2 273 10 START MODE SYS.2 |
| SW3ALL1 7C 1 272 01 IAE DISCRETE STATUS WORD #3 |
| SW3ALL2 7C 2 272 10 IAE DISCRETE STATUS WORD #3 |
| SW3B121 7C 1 272 01 BUMP/OVERBOOT #1 ENABLE SYS.1 |
| SW3B122 7C 2 272 10 BUMP/OVERBOOT #1 ENABLE SYS.2 |
| SW3B131 7C 1 272 01 BUMP/OVERBOOT #2 ENABLE SYS.1 |
| SW3B132 7C 2 272 10 BUMP/OVERBOOT #2 ENABLE SYS.2 |
| SW3B141 7C 1 272 01 BUMP/OVERBOOT #3 ENABLE SYS.1 |
| SW3B142 7C 2 272 10 BUMP/OVERBOOT #3 ENABLE SYS.2 |
| SW3B191 7C 1 272 01 START MODE SYS.1 |
| SW3B192 7C 2 272 10 START MODE SYS.2 |
| SW3B221 7C 1 272 01 BLEED CONFIGURATION K1 - SELECT SYS.1 |
| SW3B222 7C 2 272 10 BLEED CONFIGURATION K1 - SELECT SYS.2 |
| SW3B231 7C 1 272 01 BLEED CONFIGURATION K2 - SELECT SYS.1 |
| SW3B232 7C 2 272 10 BLEED CONFIGURATION K2 - SELECT SYS.2 |
| SW3B251 7C 1 273 01 4 T/R DOORS STOWED AND LOCKED ENG.1 |
| SW3B252 7C 2 273 10 4 T/R DOORS STOWED AND LOCKED ENG.2 |
| SW3B261 7C 1 273 01 BLEED CONFIGURATION K5 - SELEC SYS.1 |
| SW3B262 7C 2 273 10 BLEED CONFIGURATION K5 - SELEC SYS.2 |
| SW5B151 7C 1 275 01 N1/N2 CONTROL ACTIVE |
| SW5B152 7C 2 275 10 N1/N2 CONTROL ACTIVE |
| SW5B201 7C 1 275 01 AUTO THRUST ACTIVE |
| SW5B202 7C 2 275 10 AUTO THRUST ACTIVE |
| SW5B261 7C 1 275 01 CHANNEL A ACTIVE |
| SW5B262 7C 2 275 10 N1/N2 CONTROL ACTIVE |
| SW5B271 7C 1 275 01 CHANNEL B ACTIVE |
| SW5B272 7C 2 275 10 N1/N2 CONTROL ACTIVE |
| SW5BALL1 7C 1 275 01 DISCRETE STATUS WORD #5 |
| SW5BALL2 7C 2 275 10 DISCRETE STATUS WORD #5 |
| T12A 7C 1 130 01 DEG. C T12 (INLET FAN TEMP) SYS.1 |
| T12B 7C 2 130 10 DEG. C T12 (INLET FAN TEMP) SYS.2 |
| T251 7C 1 263 01 DEG. C T2.5 (LPC EXIT TEMPERATURE) SYS.1 |
| T252 7C 2 263 10 DEG. C T2.5 (LPC EXIT TEMPERATURE) SYS.2 |
| T25SEL1 7C 1 263 01 DEG. C T2.5 (LPC EXIT TEMPERATURE) SYS.1 |
| T25SEL2 7C 2 263 10 DEG. C T2.5 (LPC EXIT TEMPERATURE) SYS.2 |
| T31 7C 1 265 01 DEG. C T3 (HPC EXIT TEMPERATURE) SYS.1 |
| T32 7C 2 265 10 DEG. C T3 (HPC EXIT TEMPERATURE) SYS.2 |
| T3SEL1 7C 1 265 01 DEG. C T3 (HPC EXIT TEMPERATURE) SYS.1 |
| T3SEL2 7C 2 265 10 DEG. C T3 (HPC EXIT TEMPERATURE) SYS.2 |
| T51 7C 1 260 01 DEG. C T5 TEMPERATURE AT POSITION 5 SYS.1 |
| T52 7C 2 260 10 DEG. C T5 TEMPERATURE AT POSITION 5 SYS.2 |
| TAT 06 1 211 01 DEG. C TOTAL AIR TEMPERATURE |
| 06 2 211 10 DEG. C TOTAL AIR TEMPERATURE |
| TAT1 06 1 211 01 TOTAL AIR TEMPERATURE SYS.1 |
| TAT1S 06 1 211 01 TOTAL AIR TEMPERATURE SYS.1 |
| TAT2 06 2 211 10 TOTAL AIR TEMPERATURE SYS.2 |
| TAT2S 06 2 211 10 TOTAL AIR TEMPERATURE SYS.2 |
| TATSEL1 06 1 211 01 TOTAL AIR TEMPERATURE SYS.1 |
| TATSEL2 06 2 211 10 TOTAL AIR TEMPERATURE SYS.2 |
| TCAS2181 25 1 306 01 TCAS RA 1 |
| 25 2 306 10 TCAS RA 1 |
| TCAS2191 25 1 306 01 TCAS RA 2 |
| 25 2 306 10 TCAS RA 2 |
| TCAS2201 25 1 306 01 TCAS RA 3 |
| 25 2 306 10 TCAS RA 3 |
| TCAS2211 25 1 306 01 TCAS RA 4 |
| 25 2 306 10 TCAS RA 4 |
| TCAS2221 25 1 306 01 TCAS RA 5 |
| 25 2 306 10 TCAS RA 5 |
| TCAS2231 25 1 306 01 TCAS RA 6 |
| 25 2 306 10 TCAS RA 6 |
| TCAS2241 25 1 306 01 TCAS RA 7 |
| 25 2 306 10 TCAS RA 7 |
| TCAS2251 25 1 306 01 TCAS RA 8 |
| 25 2 306 10 TCAS RA 8 |
| TCAS2261 25 1 306 01 TCAS RA 9 |
| 25 2 306 10 TCAS RA 9 |
| TCAS2271 25 1 306 01 TCAS RA 10 |
| 25 2 306 10 TCAS RA 10 |
| TCAS2281 25 1 306 01 TCAS RA 11 |
| 25 2 306 10 TCAS RA 11 |
| TCAS2291 25 1 306 01 TCAS RA 12 |
| 25 2 306 10 TCAS RA 12 |
| TCASB141 25 1 307 01 TCAS TA 1 |
| 25 2 307 10 TCAS TA 1 |
| TCASB151 25 1 307 01 TCAS TA 2 |
| 25 2 307 10 TCAS TA 2 |
| TCASB171 25 1 307 01 TCAS SENSITIVE 1 |
| 25 2 307 10 TCAS SENSITIVE 1 |
| TCASB181 25 1 307 01 TCAS SENSITIVE 2 |
| 25 2 307 10 TCAS SENSITIVE 2 |
| TCASB191 25 1 307 01 TCAS SENSITIVE 3 |
| 25 2 307 10 TCAS SENSITIVE 3 |
| THDG1 04 1 44 01 DEG TRUE HEADING 1 |
| THDG2 04 2 44 10 DEG TRUE HEADING 2 |
| THLA11 25 1 133 01 THROTTLE LEVER ANGLE ENGINE 1 (IAE) |
| 25 2 133 01 THROTTLE LEVER ANGLE ENGINE 1 (IAE) |
| THLA21 25 1 133 10 THROTTLE LEVER ANGLE ENGINE 2 (IAE) |
| 25 2 133 10 THROTTLE LEVER ANGLE ENGINE 2 (IAE) |
| TLA1 7C 1 133 01 DEG TLA (THROTTLE RESOLVER ANGLE) SYS.1 |
| TLA2 7C 2 133 10 DEG TLA (THROTTLE RESOLVER ANGLE) SYS.2 |
| TLASEL1 7C 1 133 01 DEG TLA (THROTTLE RESOLVER ANGLE) SYS.1 |
| TLASEL2 7C 2 133 10 DEG TLA (THROTTLE RESOLVER ANGLE) SYS.2 |
| TN1 26 1 322 01 DEG. C ENG 1 NACELLE TEMPERATURE |
| 26 2 322 01 DEG. C ENG 1 NACELLE TEMPERATURE |
| TN2 26 1 322 10 DEG. C ENG 2 NACELLE TEMPERATURE |
| 26 2 322 10 DEG. C ENG 2 NECELLE TEMPERATURE |
| TO1A 01 1 41 NA DESTINATION AIRPORT CHAR.#1 LEFTMOST |
| 01 2 41 NA DESTINATION AIRPORT CHAR.#1 LEFTMOST |
| TO2A 01 1 42 NA DESTINATION AIRPORT CHAR.#1 LEFTMOST |
| 01 2 42 NA DESTINATION AIRPORT CHAR.#1 LEFTMOST |
| TO3A 01 1 42 NA DESTINATION AIRPORT CHAR.#3 |
| 01 2 42 NA DESTIANTION AIRPORT CHAR.#3 |
| TO4A 01 1 42 NA DESTINATION AIRPORT CHAR.#4 RIGHTMOST |
| 01 2 42 NA DESTIANTION AIRPORT CHAR.#4 RIGHTMOST |
| TP1 8E 1 121 11 DEG. C PACK OUTLET TEMPERATURE SYS.1 |
| TP2 8E 2 121 00 DEG. C PACK OUTLET TEMPERATURE SYS.2 |
| TPOE11 6F 1 141 01 DEG. C PRECOOLER ENG 1 OUTLET TEMP SYS.1 |
| 6F 2 141 10 DEG. C PRECOOLER ENG 1 OUTLET TEMP SYS.1 |
| TPOE21 6F 1 140 01 DEG. C PRECOOLER ENG 2 OUTLET TEMP SYS.1 |
| 6F 2 140 10 DEG. C PRECOOLER ENG 2 OUTLET TEMP SYS.1 |
| TW1 8E 1 111 11 DEG. C PACK WATER EXTR. TEMPERATURE SYS.1 |
| TW2 8E 2 111 00 DEG. C PACK WATER EXTR. TEMPERATURE SYS.2 |
| UTCHHA 17 1 125 00 HH UTC HOURS |
| 7E 1 125 00 HH UTC HOURS |
| UTCMMA 17 1 125 00 MM UTC MINUTES |
| 7E 1 125 00 MM UTC MINUTES |
| UTCQAR1 17 1 125 00 UTC RECORDED IN QAR (HH:MM) |
| 7E 1 125 00 UTC RECORDED IN QAR (HH:MM) |
| UTCSSC 17 1 125 00 .M UTC SECONDS FROM FDIU/CFDIU (10THS/MIN.) |
| 7E 1 125 00 .M UTC SECONDS FROM FDIU/CFDIU (10THS/MIN.) |
| UTCSSF 17 1 150 00 SS UTC SECONDS FROM FDIU |
| VA2 5D 2 220 10 % CAB TEMP REG VLV POS GROUP 3 SYS.2 |
| VACC1 04 1 364 01 G VERTICAL ACCELERATION SYS.1 |
| VACC1S 04 1 364 01 G VERTICAL ACCELERATION SYS.1 |
| VACC2 04 2 364 10 G VERTICAL ACCELERATION SYS.2 |
| VACC2S 04 2 364 10 G VERTICAL ACCELERATION SYS.2 |
| VAT1 01 1 304 00 VAT (APPR SPEED TARGET) |
| 01 2 304 00 VAT (APPR SPEED TARGET) |
| VB11 3D 1 135 01 % N1 VIB ENG 1 BRG1 OR TRF SYS.1 |
| VB12 3D 1 135 10 % N1 VIB ENG 2 BRG1 OR TRF SYS.1 |
| VB21 3D 1 136 01 % N2 VIB ENG 1 BRG1 OR TRF SYS.1 |
| VB22 3D 1 136 10 % N2 VIB ENG 2 BRG1 OR TRF SYS.1 |
| VBV1 7C 1 71 01 DEG VARIABLE BLEED VALVE PSN SYS.1 |
| VBV2 7C 2 71 10 DEG VARIABLE BLEED VALVE PSN SYS.2 |
| VBVSEL1 7C 1 71 01 DEG VARIABLE BLEED VALVE PSN SYS.1 |
| VBVSEL2 7C 2 71 10 DEG VARIABLE CLEED VALVE PSN SYS.2 |
| VC1 3D 1 230 01 MILS FAN PICK UP N2 TRACK VIBRATION ENG 1 |
| VC2 3D 1 230 10 MILS FAN PICK UP N2 TRACK VIBRATION ENG 2 |
| VF2 5D 2 206 10 % CAB TEMP REG VLV POS GROUP 1 SYS.2 |
| VH1 3D 1 230 11 IPS TRF PICK UP N2 TRACK VIBRATION ENG 1 |
| VH2 3D 1 230 00 IPS TRF PICK UP N2 TRACK VIBRATION ENG 2 |
| VL1 3D 1 227 11 MILS TRF PICK UP N1 TRACK VIBRATION ENG.1 |
| VL2 3D 1 227 00 MILS TRF PICK UP N1 TRACK VIBRATION ENG.2 |
| VN1 3D 1 227 01 MILS FAN PICK UP N1 TRACK VIBRATION ENG.1 |
| VN2 3D 1 227 10 MILS FAN PICK UP N1 TRACK VIBRATION ENG.2 |
| VRTA1 29 1 333 01 G NORMAL ACCELERATION SYS.1 |
| 29 2 333 01 G NORMAL ACCELERATION SYS.1 |
| VSCB1 5C 1 150 01 FT/MIN CABIN V/S SYS.1 |
| VSCB2 5C 2 150 10 FT/MIN CABIN V/S SYS.2 |
| VSV1 7C 1 72 01 DEG SELECTED VARIABLE STATOR VANE PSN SYS.1 |
| VSV2 7C 2 72 10 DEG SELECTED VARIABLE STATOR VANE PSN SYS.2 |
| VSVSEL1 7C 1 72 01 DEG SELECTED VARIABLE STATOR VANE PSN SYS.1 |
| VSVSEL2 7C 2 72 10 DEG SELECTED VARIABLE STATOR VANE PSN SYS.2 |
| VW2 5D 2 207 10 % CAB TEMP REG VLV POS GROUP 2 SYS.2 |
| WARN1114 26 1 126 11 MASTER WARNING |
| 26 2 126 11 MASTER WARNING |
| WARN1117 26 1 126 11 STALL |
| 26 2 126 11 STALL |
| WARN1125 26 1 126 11 GEAR NOT LOCKED CLEAN |
| 26 2 126 11 GEAR NOT LOCKED CLEAN |
| WARNB111 26 1 126 11 SDAC 1 VALID SYS.1 |
| 26 2 126 11 SDAC 1 VALID SYS.1 |
| WARNB121 26 1 126 11 SDAC 2 VALID SYS.1 |
| 26 2 126 11 SDAC 2 VALID SYS.1 |
| WARNB131 26 1 126 00 SLATS FAULT SYS.1 |
| 26 2 126 00 SLATS FAULT SYS.1 |
| WARNB141 26 1 126 00 FLAPS FAULT SYS.1 |
| 26 2 126 00 FLAPS FAULT SYS.1 |
| WARNB151 26 1 126 00 YAW DAMPER1 FAULT SYS.1 |
| 26 2 126 00 YAW DAMPER1 FAULT SYS.1 |
| WARNB161 26 1 126 00 YAW DAMPER2 FAULT SYS.1 |
| 26 2 126 00 YAW DAMPER2 FAULT SYS.1 |
| WARNB171 26 1 126 00 ENG1 FIRE SYS.1 |
| 26 2 126 00 ENG1 FIRE SYS.1 |
| WARNB181 26 1 126 00 ENG2 FIRE SYS.1 |
| 26 2 126 00 ENG2 FIRE SYS.1 |
| WARNB191 26 1 126 00 APU FIRE SYS.1 |
| 26 2 126 00 APU FIRE SYS.1 |
| WARNB221 26 1 126 00 CABIN PRESS FAULT SYS.1 |
| 26 2 126 00 CABIN PRESS FAULT SYS.1 |
| WARNB231 26 1 126 00 BLUE HYD LOW PRESSURE SYS.1 |
| 26 2 126 00 BLUE HYD LOW PRESSURE SYS.1 |
| WARNB241 26 1 126 00 YELLOW HYD LOW PRESSURE SYS.1 |
| 26 2 126 00 YELLOW HYD LOW PRESSURE SYS.1 |
| WARNB251 26 1 126 00 GREEN HYD LOW PRESSURE SYS.1 |
| 26 2 126 00 GREEN HYD LOW PRESSURE SYS.1 |
| WARNB261 26 1 126 00 VMO/MMO OVERSPEED SYS.1 |
| 26 2 126 00 VMO/MMO OVERSPEED SYS.1 |
| WARNB291 26 1 126 00 SURF. NOT T.O. CONFIG |
| 26 2 126 00 SURF. NOT T.O. CONFIG |
| WBKG 7A 1 123 01 KG/SEC BLEED AIR FLOW |
| WD 04 1 316 01 DEG WIND DIRECTION - TRUE |
| 04 2 316 10 DEG WIND DIRECTION - TRUE |
| WD1 04 1 316 01 DEG WIND DIRECTION - TRUE SYS.1 |
| WD2 04 2 316 10 DEG WIND DIRECTION - TRUE SYS.2 |
| WFQKG1 5A 2 257 10 KG FUEL QUANTITY - LH INNER CELL SYS.2 (KG) |
| WFQKG2 5A 2 261 10 KG FUEL QUANTITY - RH INNER CELL SYS.2 (KG) |
| WFQKG3 5A 2 260 10 KG FUEL QUANTITY - CENTER TANK (KG) |
| WFQKG4 5A 2 256 10 KG FUEL QUANTITY - LH OUTER CELL (KG) |
| WFQKG5 5A 2 262 10 KG FUEL QUANTITY - RH OUTER CELL (KG) |
| WFQTOTKG 5A 2 247 10 KG TOTAL FUEL QUANTITY (KG) |
| WS 04 1 315 01 KTS WIND SPEED |
| 04 2 315 10 KTS WIND SPEED |
| WS1 04 1 315 01 KTS WIND SPEED SYS.1 |
| WS2 04 2 315 10 KTS WIND SPEED SYS.2 |
| WSD1 26 1 14 01 WIND SHEAR DETECTION SYS.1 |
| WSD2 26 2 14 01 WIND SHEAR DETECTION SYS.2 |
| YAW 04 1 330 01 DEG/SEC BODY AXIS YAW RATE SYS.1 |
| 04 2 330 10 DEG/SEC BODY AXIS YAW RATE SYS.1 |
| ZCB 5C 1 151 01 FT CABIN ALTITUDE |
| 5C 2 151 10 FT CABIN ALTITUDE |
| ZCB1 5C 1 151 01 FT CABIN ALTITUDE SYS.1 |
| ZCB2 5C 2 151 10 FT CABIN ALTITUDE SYS.2 |
| ZDW1B112 5D 2 60 10 DUCT OVERHEAT (88 DEG. C) WARN 1 SYS.2 |
| ZDW1B122 5D 2 60 10 DUCT OVERHEAT (88 DEG. C) WARN 2 SYS.2 |
| ZDW1B132 5D 2 60 10 DUCT OVERHEAT (88 DEG. C) WARN 3 SYS.2 |
| ZDW1B142 5D 2 60 10 4X LIMIT EXCEED. DUCT TEMP. GR. 1 SYS.2 |
| ZDW1B152 5D 2 60 10 4X LIMIT EXCEED. DUCT TEMP. GR. 2 SYS.2 |
| ZDW1B162 5D 2 60 10 4X LIMIT EXCEED. DUCT TEMP. GR. 3 SYS.2 |
| ZDW1B202 5D 2 60 10 TRIM AIR PRESS REG VALVE SYS.2 |
| ZDW1B212 5D 2 60 10 MAIN ZONE CONTROL INOP SYS.2 |
| ZDW1B222 5D 2 60 10 ZONE SECONDARY CONTROL INOP SYS.2 |
| ZLD1 5C 1 163 01 FT LANDING ELEVATION SYS.1 |
| ZLD2 5C 2 163 10 FT LANDING ELEVATION SYS.2 |
NOTE: Alpha Call-Up list is applicable for CFMI engines only.
| ------------------------------------------------------------------------------- |
| Alpha Parameter Unit Comment |
| ------------------------------------------------------------------------------- |
| ACID1 17 1 301 00 A/C TAIL NUMBER 1 2 3 CHARACTERS |
| ACID11 17 1 301 00 A/C TAIL NUMBER CHARS. 1 |
| ACID1G 17 1 301 00 A/C TAIL NUMBER GSM |
| ACID2 17 1 302 00 A/C TAIL NUMBER 4 5 6 CHARACTERS |
| ACID21 17 1 301 00 A/C TAIL NUMBER CHARS. 2 |
| ACID2G 17 1 302 00 A/C TAIL NUMBER GSM |
| ACID3 17 1 303 00 A/C ID 7TH CHAR |
| ACID31 17 1 301 00 A/C TAIL NUMBER CHARS. 3 |
| ACID3G 17 1 303 00 A/C TAIL NUMBER GSM |
| ACID41 17 1 302 00 A/C TAIL NUMBER CHARS. 4 |
| ACID4G 17 1 304 00 A/C TAIL NUMBER GSM |
| ACID51 17 1 302 00 A/C TAIL NUMBER CHARS. 5 |
| ACID61 17 1 302 00 A/C TAIL NUMBER CHARS. 6 |
| ACID71 17 1 303 00 A/C TAIL NUMBER CHARS. 7 |
| ACIDB111 17 1 304 00 A/C TYPE CODE BITS 11-16 SYS. 1 |
| ACIDB181 17 1 304 00 FLEET IDENT BITS 18-21 SYS. 1 |
| ACYI 7A 1 133 01 CYCLES START CYCLES |
| ADW1ALL1 7A 1 37 01 APU SW 1 |
| ADW1B111 7A 1 37 01 APU BLEED VALVE OPEN |
| ADW1B121 7A 1 37 01 APU BLEED VALVE CLOSED |
| ADW1B131 7A 1 37 01 APU FUEL LOW PRESSURE |
| ADW1B171 7A 1 37 01 AUTOMATIC SHUT DOWN |
| ADW1B181 7A 1 37 01 EMERGENCY (EXTERNAL) S/D |
| ADW1B201 7A 1 37 01 LOW OIL LEVEL |
| ADW1B211 7A 1 37 01 MAIN ENG START MODE |
| ADW1B221 7A 1 37 01 APU START IN PROGRESS |
| AHRI 7A 1 132 01 HOURS OPERATING HOURS |
| AILL 6C 1 310 01 DEG AILERON POSITION LEFT SYS. 1 |
| 6C 2 310 10 |
| AILR 6C 1 330 01 DEG AILERON POSITION RIGHT SYS. 1 |
| 6C 2 330 10 |
| ALT 06 1 203 01 FT ALTITUDE (1013.25MB) |
| 06 2 203 10 |
| ALT01 06 1 203 01 ALTITUDE (1013.25MB) SYS. 1 |
| ALT02 06 1 203 10 ALTITUDE (1013.25MB) SYS. 2 |
| ALT1GSM 06 1 203 01 FT ALTITUDE FOR GSM SYS 1 |
| ALT2GSM 06 1 203 10 FT ALTITUDE FOR GSM SYS 2 |
| ALTBARFN 25 1 222 01 ALT BARO SET CAPT FINE |
| 25 2 222 10 |
| ALTBARFO 25 1 223 01 ALT BARO SET F/O FINE |
| 25 2 223 10 |
| ALTDMC 25 1 102 01 FT SELECTED ALTITUDE (DAR) |
| 25 2 102 10 |
| ALTGSM 06 1 203 01 FT ALTITUDE FOR GSM |
| 06 2 203 10 |
| AMW1B111 7A 1 353 01 NO FLAME |
| AMW1B121 7A 1 353 01 REVERSE FLOW |
| AMW1B131 7A 1 353 01 LOSS OF DC POWER |
| AMW1B141 7A 1 353 01 HIGH OIL TEMPERATURE |
| AMW1B171 7A 1 353 01 INLET DOOR FAILURE |
| AMW1B181 7A 1 353 01 HIGH GEN. OIL TEMPERATURE |
| AMW1B201 7A 1 353 01 OVERTEMPERATURE |
| AMW1B211 7A 1 353 01 SENSOR FAILURE (EGT OR LOP) |
| AMW1B221 7A 1 353 01 NO ACCELERATION |
| AMW1B231 7A 1 353 01 SLOW START |
| AMW1B241 7A 1 353 01 OVERSPEED |
| AMW1B251 7A 1 353 01 ECB FAILURE |
| AMW1B261 7A 1 353 01 LOW OIL PRESSURE |
| AMW1B271 7A 1 353 01 LOSS OF OVERSPEED PROTECTION |
| AMW1B281 7A 1 353 01 INLET GUIDE VANES |
| AMW2ALL1 7A 1 351 01 APU CONTROL WORD |
| AMW2B111 7A 1 351 01 PT SENSOR |
| AMW2B121 7A 1 351 01 DELTA P SENSOR |
| AMW2B131 7A 1 351 01 SPEED SENSOR NO. 1 |
| AMW2B141 7A 1 351 01 SPEED SENSOR NO. 2 |
| AMW2B151 7A 1 351 01 HIGH OIL TEMP SWITCH |
| AMW2B161 7A 1 351 01 OIL TEMP SENSOR |
| AMW2B171 7A 1 351 01 FUEL CONTROL TORQUE MOTOR |
| AMW2B181 7A 1 351 01 SURGE VALVE TORQUE MOTOR |
| AMW2B191 7A 1 351 01 EGT RAKE NO. 1 |
| AMW2B201 7A 1 351 01 EGT RAKE NO. 2 |
| AMW2B211 7A 1 351 01 IGV ACTUATOR |
| AMW2B221 7A 1 351 01 IGNITION UNIT |
| AMW2B231 7A 1 351 01 DEOIL SOLENOID |
| AMW2B241 7A 1 351 01 GEN. OIL TEMP SENSOR |
| AMW2B251 7A 1 351 01 ECS DEMAND SIGNAL |
| AMW2B261 7A 1 351 01 APU STARTER |
| AMW2B271 7A 1 351 01 OIL PRESSURE SWITCH |
| AMW2B281 7A 1 351 01 P2 SENSOR |
| AMW2B291 7A 1 351 01 ECB |
| AMW3ALL1 7A 1 352 01 DISCRETE STATUS WORD |
| AMW3B121 7A 1 352 01 LOAD VALVE SOLENOID |
| AMW3B131 7A 1 352 01 LCDT SENSOR |
| AMW3B141 7A 1 352 01 LCIT SENSOR |
| AMW3B151 7A 1 352 01 FUEL SOLENOID |
| AMW3B161 7A 1 352 01 START CONTACTOR |
| AMW3B171 7A 1 352 01 BACK UP START CONTACTOR |
| AMW3B181 7A 1 352 01 APU S/N ENCODER |
| AMW3B201 7A 1 352 01 AIR INTAKE ACTUATOR |
| AMW3B221 7A 1 352 01 IGV LVDT |
| AOA1 06 1 241 01 DEG CORRECTED ANGLE OF ATTACK SYS. 1 |
| AOA2 06 1 241 10 DEG CORRECTED ANGLE OF ATTACK SYS. 2 |
| AOAMAX 0A 1 243 00 KTS MAX AOA SPEED |
| 0A 2 243 00 |
| AOAPROT 0A 1 247 00 KTS AOA PROTECTION SPEED |
| 0A 2 247 00 |
| AP1146 01 1 146 00 SYS 1 AP LAND TRACK |
| AP1274 01 1 274 00 AP SYS 1 LABEL 274 (ALL BITS) |
| AP127411 01 1 274 00 AP SYS 1 LABEL 274 BIT 11 |
| AP127412 01 1 274 00 AP SYS 1 LABEL 274 BIT 12 |
| AP127413 01 1 274 00 AP SYS 1 LABEL 274 BIT 13 |
| AP127414 01 1 274 00 AP SYS 1 LABEL 274 BIT 14 |
| AP127415 01 1 274 00 AP SYS 1 LABEL 274 BIT 15 |
| AP127416 01 1 274 00 AP SYS 1 LABEL 274 BIT 16 |
| AP127417 01 1 274 00 AP SYS 1 LABEL 274 BIT 17 |
| AP127418 01 1 274 00 AP SYS 1 LABEL 274 BIT 18 |
| AP127419 01 1 274 00 AP SYS 1 LABEL 274 BIT 19 |
| AP127420 01 1 274 00 AP SYS 1 LABEL 274 BIT 20 |
| AP127421 01 1 274 00 AP SYS 1 LABEL 274 BIT 21 |
| AP127422 01 1 274 00 AP SYS 1 LABEL 274 BIT 22 |
| AP127423 01 1 274 00 AP SYS 1 LABEL 274 BIT 23 |
| AP127424 01 1 274 00 AP SYS 1 LABEL 274 BIT 24 |
| AP1275 01 1 275 00 AP SYS 1 LABEL 275 (ALL BITS) |
| AP127511 01 1 275 00 AP SYS 1 LABEL 275 RUNWAY MODE |
| AP127512 01 1 275 00 AP SYS 1 LABEL 275 NAV MODE |
| AP127513 01 1 275 00 AP SYS 1 LABEL 275 LOC CAPTURE MODE |
| AP127514 01 1 275 00 AP SYS 1 LABEL 275 LOC TRACK MODE |
| AP127515 01 1 275 00 AP SYS 1 LABEL 275 ROLL GO AROUND MODE |
| AP127516 01 1 275 00 AP SYS 1 LABEL 275 HEADING MODE |
| AP127517 01 1 275 00 AP SYS 1 LABEL 275 TRACK MODE |
| AP2146 01 1 146 00 SYS 2 AP LAND TRACK |
| AP2274 01 1 274 00 AP SYS 2 LABEL 274 (ALL BITS) |
| AP227411 01 1 274 00 AP SYS 2 LABEL 274 BIT 11 |
| AP227412 01 1 274 00 AP SYS 2 LABEL 274 BIT 12 |
| AP227413 01 1 274 00 AP SYS 2 LABEL 274 BIT 13 |
| AP227414 01 1 274 00 AP SYS 2 LABEL 274 BIT 14 |
| AP227415 01 1 274 00 AP SYS 2 LABEL 274 BIT 15 |
| AP227416 01 1 274 00 AP SYS 2 LABEL 274 BIT 16 |
| AP227417 01 1 274 00 AP SYS 2 LABEL 274 BIT 17 |
| AP227418 01 1 274 00 AP SYS 2 LABEL 274 BIT 18 |
| AP227419 01 1 274 00 AP SYS 2 LABEL 274 BIT 19 |
| AP227420 01 1 274 00 AP SYS 2 LABEL 274 BIT 20 |
| AP227421 01 1 274 00 AP SYS 2 LABEL 274 BIT 21 |
| AP227422 01 1 274 00 AP SYS 2 LABEL 274 BIT 22 |
| AP227423 01 1 274 00 AP SYS 2 LABEL 274 BIT 23 |
| AP227424 01 1 274 00 AP SYS 2 LABEL 274 BIT 24 |
| AP2275 01 1 275 00 AP SYS 2 LABEL 275 (ALL BITS) |
| AP227511 01 1 275 00 AP SYS 2 LABEL 275 RUNWAY MODE BIT 11 |
| AP227512 01 1 275 00 AP SYS 2 LABEL 275 NAV MODE BIT 12 |
| AP227513 01 1 275 00 AP SYS 2 LABEL 275 LOC CAPTURE BIT 13 |
| AP227514 01 1 275 00 AP SYS 2 LABEL 275 LOC TRACK BIT 14 |
| AP227515 01 1 275 00 AP SYS 2 LABEL 275 ROLL GO AROUND BIT 15 |
| AP227516 01 1 275 00 AP SYS 2 LABEL 275 HEADING BIT 16 |
| AP227517 01 1 275 00 AP SYS 2 LABEL 275 TRACK BIT 17 |
| ASN 7A 1 50 01 APU SERIAL NUMBER SYS. 1 |
| AST 25 1 304 01 KTS APPROACH SPEED TARGET |
| AUTBRFF2 6E 1 26 10 AUTO BRAKE OFF |
| AUTBRFT2 6E 1 26 10 AUTO BRAKE FAULT |
| AUTBRKFF 6E 1 26 01 AUTO BRAKE OFF |
| AUTBRKFT 6E 1 26 01 AUTO BRAKE FAULT |
| BMCW4152 6F 1 66 01 BMC DISCRETE WORD # 4 |
| 6F 2 66 10 |
| BMCW4172 6F 1 66 01 BMC DISCRETE WORD # 4 |
| 6F 2 66 10 |
| BMCW5151 6F 1 67 01 BMC DISCRETE WORD # 5 |
| 6F 2 67 10 |
| BMCW5172 6F 1 67 01 BMC DISCRETE WORD # 5 |
| 6F 2 67 10 |
| BSCU281 6E 1 27 01 BSCU SYSTEM 1 ENGAGED |
| BSCU282 6E 1 27 10 BSCU SYSTEM 2 ENGAGED |
| BT1 6E 1 114 01 DEG C BRAKE 1 TEMP |
| 6E 2 114 10 |
| BT2 6E 1 115 01 DEG C BRAKE 2 TEMP |
| 6E 2 115 10 |
| BT3 6E 1 116 01 DEG C BRAKE 3 TEMP |
| 6E 2 116 10 |
| BT4 6E 1 117 01 DEG C BRAKE 4 TEMP |
| 6E 2 117 10 |
| BVP1B211 26 1 31 01 ENG1 MODE SELECT SYS. 1 |
| 26 2 31 01 |
| BVP1B212 26 1 31 10 ENG1 MODE SELECT SYS. 2 |
| 26 2 31 10 |
| BVP1B261 26 1 31 01 ENG1 SCAVENGE VLV OPEN SYS. 1 |
| 26 2 31 01 |
| BVP2B261 26 1 31 10 ENG2 SCAVENGE VLV OPEN SYS. 1 |
| 26 2 31 10 |
| CAS 06 1 206 01 KTS COMPUTED AIRSPEED |
| 06 2 206 10 |
| CAS1 06 1 206 01 COMPUTED AIRSPEED SYS. 1 |
| CAS2 06 1 206 10 COMPUTED AIRSPEED SYS. 2 |
| CG 02 1 77 00 % MAC LONG CENTER OF GRAVITY |
| 02 2 77 00 |
| CG1 02 1 77 00 LONG CENTER OF GRAVITY SYS. 1 |
| CG2 02 1 77 00 LONG CENTER OF GRAVITY SYS. 2 |
| CONSALT1 25 1 163 01 CONSTRAINT ALTITUDE |
| 25 2 163 10 |
| COT1 8E 1 123 11 DEG C PACK COMPR. OUTLET TEMPERATURE SYS. 1 |
| COT2 8E 1 123 00 DEG C PACK COMPR. OUTLET TEMPERATURE SYS. 2 |
| CROLL1 6C 1 301 01 DEG ROLL CAPT CMD POSITION |
| 6C 2 301 10 |
| CTYPR40A 01 1 40 NA CITY PAIR LABEL 040 FOR DAR |
| CTYPR40G 01 1 40 NA CITY PAIR LABEL 040 FOR GSM |
| CTYPR41A 01 1 41 NA CITY PAIR LABEL 041 FOR DAR |
| CTYPR41G 01 1 41 NA CITY PAIR LABEL 041 FOR GSM |
| CTYPR42A 01 1 42 NA CITY PAIR LABEL 042 FOR DAR |
| CTYPR42G 01 1 42 NA CITY PAIR LABEL 042 FOR GSM |
| DA1 04 1 321 01 DEG DRIFT ANGLE SYS. 1 |
| 04 2 321 10 |
| DATEDDA 17 1 260 00 DATE (DAY) |
| 7E 2 260 00 |
| DATEDDQ 17 1 260 00 DATE (DAY) FOR QAR RCDG. |
| 7E 2 260 00 |
| DATEGSM 17 1 260 00 DATE FOR GSM TRANSMISSION |
| DATEMMA 17 1 260 00 DATE (MONTH) |
| 7E 2 260 00 |
| DATEMMQ 17 1 260 00 DATE (MONTH) FOR QAR RCDG. |
| 7E 2 260 00 |
| DATEYYA 17 1 260 00 DATE (YEAR) |
| 7E 2 260 00 |
| DECELLO1 6E 1 27 01 DECELERATION LO ARMED |
| DECELLO2 6E 1 27 10 DECELERATION LO ARMED |
| DECELMD1 6E 1 27 01 DECELERATION MED ARMED |
| DECELMD2 6E 1 27 10 DECELERATION MED ARMED |
| DECELMX1 6E 1 27 01 DECELERATION MAX ARMED |
| DECELMX2 6E 1 27 10 DECELERATION MAX ARMED |
| DECHGHT1 25 1 370 01 SELECTED DECISION HEIGHT |
| 25 2 370 10 |
| DMC30111 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC30112 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC30113 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC30114 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC30115 25 1 301 01 DISCRETE STATUS WORD |
| 25 1 301 10 |
| DMC30116 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC30117 25 1 301 01 DISCRETE STATUS WORD |
| 25 2 301 10 |
| DMC301AL 25 1 301 01 FMA SUBMODES 1 |
| 25 2 301 10 |
| DMC35025 25 1 350 01 USE MAN PITCH TRIM STATUS |
| 25 2 350 10 |
| DMCSSPD 25 1 103 01 KTS PFD SELECTED SPEED |
| 25 2 103 10 |
| DME1DST1 25 1 202 01 DME 1 DISTANCE |
| 25 2 202 10 |
| DME1FRA 25 1 35 01 DME 1 FREQUENCY |
| 25 2 35 01 |
| DME1FRB 25 1 35 01 DME 1 FREQUENCY |
| 25 2 35 01 |
| DME1FRC 25 1 35 01 DME 1 FREQUENCY |
| 25 2 35 01 |
| DME2DST2 25 1 202 10 DME 2 DISTANCE |
| 25 2 202 10 |
| DME2FRA 25 1 35 10 DME 2 FREQUENCY |
| 25 2 35 10 |
| DME2FRB 25 1 35 10 DME 2 FREQUENCY |
| 25 2 35 10 |
| DME2FRC 25 1 35 10 DME 2 FREQUENCY |
| 25 2 35 10 |
| DSW12611 26 1 126 11 FWC 1 VALID |
| 26 2 126 11 |
| EGT1 7C 1 345 01 DEG C EGT LPT EXIT TEMP SYS. 1 |
| EGT1S 7C 1 345 01 DEG C EGT LPT EXIT TEMP SYS. 1 |
| EGT2 7C 1 345 10 DEG C EGT LPT EXIT TEMP SYS. 2 |
| EGT2S 7C 1 345 10 DEG C EGT LPT EXIT TEMP SYS. 2 |
| EGTA 7A 1 175 01 DEG C EGT (APU) |
| EGTSEL1 7C 1 345 01 DEG C EGT LPT EXIT TEMP SYS. 1 |
| EGTSEL2 7C 1 345 10 DEG C EGT LPT EXIT TEMP SYS. 2 |
| ELEV1 6C 1 314 01 DEG ELEVATOR POSITION LEFT SYS. 1 |
| 6C 2 314 10 |
| ELEV2 6C 1 334 01 DEG ELEVATOR POSITION RIGHT SYS. 1 |
| 6C 2 334 10 |
| ENGICE1 26 1 17 01 ENG 1 SEVERITY ICE DETECTED |
| 26 2 17 01 |
| ENGICE2 26 1 17 10 ENG 2 SEVERITY ICE DETECTED |
| 26 2 17 10 |
| ERT1 7C 1 50 01 HOURS ENGINE RUNNING TIME |
| ERT2 7C 1 50 10 HOURS ENGINE RUNNING TIME |
| ESNL1 7C 1 46 01 ENGINE S/N LEFT DIGIT # 1 (LSD) |
| ESNL2 7C 1 46 01 ENGINE S/N LEFT DIGIT # 2 |
| ESNL3 7C 1 46 01 ENGINE S/N LEFT DIGIT # 3 |
| ESNL4 7C 1 47 01 ENGINE S/N LEFT DIGIT # 4 |
| ESNL5 7C 1 47 01 ENGINE S/N LEFT DIGIT # 5 |
| ESNL6 7C 1 47 01 ENGINE S/N LEFT DIGIT # 6 |
| ESNR1 7C 1 46 10 ENGINE S/N RIGHT DIGIT # 1 (LSD) |
| ESNR2 7C 1 46 10 ENGINE S/N RIGHT DIGIT # 2 |
| ESNR3 7C 1 46 10 ENGINE S/N RIGHT DIGIT # 3 |
| ESNR4 7C 1 47 10 ENGINE S/N RIGHT DIGIT # 4 |
| ESNR5 7C 1 47 10 ENGINE S/N RIGHT DIGIT # 5 |
| ESNR6 7C 1 47 10 ENGINE S/N RIGHT DIGIT # 6 |
| EVENT 17 1 350 00 EVENT BUTTON PRESSED |
| EVMB111 3D 1 35 01 N1 NB VIB. ABOVE ECAM ADVISORY SYS. 1 |
| EVMB112 3D 1 35 10 N1 NB VIB. ABOVE ECAM ADVISORY SYS. 2 |
| EVMB121 3D 1 35 01 N2 NB VIB. ABOVE ECAM ADVISORY SYS. 1 |
| EVMB122 3D 1 35 10 N2 NB VIB. ABOVE ECAM ADVISORY SYS. 2 |
| EVMB131 3D 1 35 01 TRF USED SYS. 1 |
| EVMB132 3D 1 35 10 TRF USED SYS. 2 |
| EVMB141 3D 1 35 01 INITIAL VALUES NOT USED SYS. 1 |
| EVMB142 3D 1 35 10 INITIAL VALUES NOT USED SYS. 2 |
| EVMB151 3D 1 35 01 FREQUENCY ANALYSIS DONE SYS. 1 |
| EVMB152 3D 1 35 10 FREQUENCY ANALYSIS DONE SYS. 2 |
| EVMB161 3D 1 35 01 N1 BEARING ACCEL CHANNEL FAULT SYS. 1 |
| EVMB162 3D 1 35 10 N1 BEARING ACCEL CHANNEL FAULT SYS. 2 |
| EVMB171 3D 1 35 01 TRF ACCEL CHANNEL FAULT SYS. 1 |
| EVMB172 3D 1 35 10 TRF ACCEL CHANNEL FAULT SYS. 2 |
| EVMB181 3D 1 35 01 N1 SPEED CHANNEL FAULT SYS. 1 |
| EVMB182 3D 1 35 10 N1 SPEED CHANNEL FAULT SYS. 2 |
| EVMB191 3D 1 35 01 N2 SPEED CHANNEL FAULT SYS. 1 |
| EVMB192 3D 1 35 10 N2 SPEED CHANNEL FAULT SYS. 2 |
| EVMB201 3D 1 35 01 UNBALANCE PROCESS FAULT SYS. 1 |
| EVMB202 3D 1 35 10 UNBALANCE PROCESS FAULT SYS. 2 |
| EVMB211 3D 1 35 01 FREQUENCY ANALYSIS FAULT SYS. 1 |
| EVMB212 3D 1 35 10 FREQUENCY ANALYSIS FAULT SYS. 2 |
| EVMB221 3D 1 35 01 NON-VOLATILE MEMORY FAULT SYS. 1 |
| EVMB222 3D 1 35 10 NON-VOLATILE MEMORY FAULT SYS. 2 |
| EVMB231 3D 1 35 01 PROVISION 1 SYS. 1 |
| EVMB232 3D 1 35 10 PROVISION 1 SYS. 2 |
| EVMB241 3D 1 35 01 PROVISION 2 SYS. 1 |
| EVMB242 3D 1 35 10 PROVISION 2 SYS. 2 |
| EVMB251 3D 1 35 01 PROVISION 3 SYS. 1 |
| EVMB252 3D 1 35 10 PROVISION 3 SYS. 2 |
| EVMB261 3D 1 35 01 PROVISION 4 SYS. 1 |
| EVMB262 3D 1 35 10 PROVISION 4 SYS. 2 |
| EVMB271 3D 1 35 01 ONE VIB DAT ABOVE ADVISORY SYS. 1 |
| EVMB272 3D 1 35 10 ONE VIB DAT ABOVE ADVISORY SYS. 2 |
| EVMB281 3D 1 35 01 EVMU CLASS 2 FAULT SYS. 1 |
| EVMB282 3D 1 35 10 EVMU CLASS 2 FAULT SYS. 2 |
| EVMB291 3D 1 35 01 EVMU CLASS 1 FAULT SYS. 1 |
| EVMB292 3D 1 35 10 EVMU CLASS 1 FAULT SYS. 2 |
| EVMBALL1 3D 1 35 01 HEX ENGINE VIBRATION STATUS WORD ENG. 1 |
| EVMBALL2 3D 1 35 10 HEX ENGINE VIBRATION STATUS WORD ENG. 2 |
| FC411920 6C 1 41 01 CAPT/FO PRIORITY LOCKED |
| 6C 2 41 10 |
| FCU2721 A1 1 272 00 FCU DISCRETE LABEL 272 BITS 23-26 SYS.1 |
| FCU2722 A1 1 272 00 FCU DISCRETE LABEL 272 BITS 23-26 SYS.2 |
| FCU273 A1 1 273 00 FCU DISCRETE LABEL 273 |
| A1 2 273 00 |
| FCU274 A1 1 274 00 FCU DISCRETE LABEL 274 |
| A1 2 274 00 |
| FD 5A 1 272 10 KG/L FUEL DENSITY (LEFT CNTR OR RIGHT TANK) |
| FDPTCH 01 1 141 00 DEG FD PITCH ORDER |
| 01 2 141 00 |
| FDROLL 01 1 140 00 DEG FD ROLL ORDER |
| 01 2 140 00 |
| FDTANK2 5A 1 272 10 TANK FOR FUEL DENSITY |
| FDYAW 01 1 143 00 DEG FD YAW ORDER |
| 01 2 143 00 |
| FFKG1 7C 1 244 01 KGPH FUEL MASS FLOW RATE SYS. 1 (KG) |
| FFKG1S 7C 1 244 01 KGPH FUEL MASS FLOW RATE SYS. 1 (KG) |
| FFKG2 7C 1 244 10 KGPH FUEL MASS FLOW RATE SYS. 2 (KG) |
| FFKG2S 7C 1 244 10 KGPH FUEL MASS FLOW RATE SYS. 2 (KG) |
| FGC041A 01 1 41 NA FGC LABEL 041 BITS 22-16 |
| 01 2 41 NA |
| FGC273 01 1 273 00 FMA ARMED MODES |
| 01 2 273 00 |
| FGC274 01 1 274 00 FMA MODES ADDITIONAL |
| 01 2 274 00 |
| FLAP 1B 1 137 01 DEG FLAP ACTUAL POSITION |
| 1B 2 137 10 |
| FLAP1 1B 1 137 01 DEG FLAP ACTUAL POSITION SYS. 1 (LEFT) |
| FLAP2 1B 1 137 10 DEG FLAP ACTUAL POSITION SYS. 2 (RIGHT) |
| FLAPCON1 1B 1 137 01 FLAP SLAT CONF COMMAND SDI 01 |
| FLAPCON2 1B 1 137 10 FLAP SLAT CONF COMMAND SDI 10 |
| FLT233GS 01 1 233 00 FLIGHT NUMBER LABEL 233 FOR GSM |
| FLT234GS 01 1 234 00 FLIGHT NUMBER LABEL 234 FOR GSM |
| FLT235GS 01 1 235 00 FLIGHT NUMBER LABEL 235 FOR GSM |
| FLT236GS 01 1 236 00 FLIGHT NUMBER LABEL 236 FOR GSM |
| FLTN233A 01 1 233 00 FLIGHT NUMBER LABEL 233 FOR DAR |
| 01 2 233 00 |
| FLTN234A 01 1 234 00 FLIGHT NUMBER LABEL 234 FOR DAR |
| 01 2 234 00 |
| FLTN235A 01 1 235 00 FLIGHT NUMBER LABEL 235 FOR DAR |
| 01 2 235 00 |
| FLTN236A 01 1 236 00 FLIGHT NUMBER LABEL 236 FOR DAR |
| 01 2 236 00 |
| FLTNO1A 01 1 233 00 FLIGHT NUMBER DIGIT # 1 LEFTMOST |
| 01 2 233 00 |
| FLTNO2A 01 1 233 00 FLIGHT NUMBER DIGIT # 2 |
| 01 2 233 00 |
| FLTNO3A 01 1 234 00 FLIGHT NUMBER DIGIT # 3 |
| 01 2 234 00 |
| FLTNO4A 01 1 234 00 FLIGHT NUMBER DIGIT # 4 RIGHTMOST |
| 01 2 234 00 |
| FLTNO5A 01 1 235 00 FLIGHT NUMBER DIGIT # 5 (MSD RECORDED) |
| 01 2 235 00 |
| FLTNO6A 01 1 235 00 FLIGHT NUMBER DIGIT # 6 |
| 01 2 235 00 |
| FLTNO7A 01 1 236 00 FLIGHT NUMBER DIGIT # 7 |
| 01 2 236 00 |
| FLTNO8A 01 1 236 00 FLIGHT NUMBER DIGIT # 8 (LSD) |
| 01 2 236 00 |
| FMC270 02 1 270 00 NAVIGATION MODE |
| 02 2 270 00 |
| FMC271 02 1 271 00 FGC LABEL 271 |
| 02 2 271 00 |
| FMV1 7C 1 347 01 % SELECTED FMV POSITION SYS.1 |
| FMV2 7C 1 347 10 % SELECTED FMV POSITION SYS.2 |
| FMVSEL1 7C 1 347 01 % SELECTED FMV POSITION SYS.1 |
| FMVSEL2 7C 1 347 10 % SELECTED FMV POSITION SYS.2 |
| FPA 25 1 322 NA DEG FLIGHT PATH ANGLE |
| 25 2 322 NA |
| FPASEL1 25 1 115 01 SELECTED FPA |
| 25 2 115 10 |
| FQ 5A 1 250 10 LBS PRE-SELECTED FUEL QUANTITY |
| FROLL1 6C 1 302 01 ROLL F/O CMD POSITION |
| 6C 2 302 10 |
| FROM1A 01 1 40 NA DEPARTURE AIRPORT CHAR.# 1 LEFTMOST |
| 01 2 40 NA |
| FROM2A 01 1 40 NA DEPARTURE AIRPORT CHAR.# 2 |
| 01 2 40 NA |
| FROM3A 01 1 40 NA DEPARTURE AIRPORT CHAR.# 3 |
| 01 2 40 NA |
| FROM4A 01 1 41 NA DEPARTURE AIRPORT CHAR.# 4 RIGHTMOST |
| 01 2 41 NA |
| FT1 5A 1 177 10 DEG C FUEL TEMPERATURE LH INNER CELL SYS. 2 |
| FT2 5A 1 201 10 DEG C FUEL TEMPERATURE RH INNER CELL SYS. 2 |
| FW271001 26 1 271 00 LOW ENERGY WARNING SDI 00 |
| FW271002 26 1 271 00 LOW ENERGY WARNING SDI 00 |
| FW271111 26 1 271 11 LOW ENERGY WARNING SDI 11 |
| FW271112 26 1 271 11 LOW ENERGY WARNING SDI 11 |
| FWC01510 26 1 15 10 ALT AUTO CALLOUT 5-400 FT |
| 26 2 15 10 |
| FWC14601 26 1 146 01 LAND CAPACITY FAILURE |
| 26 2 146 01 |
| FWC17200 26 1 17 00 FO MASTER WARNING CANCEL |
| 26 2 17 00 |
| FWC17203 26 1 17 11 CAPT MASTER WARNING CANCEL |
| 26 2 17 11 |
| FWC17280 26 1 17 00 FO MASTER CAUTION CANCEL |
| 26 2 17 00 |
| FWC17283 26 1 17 11 CAPT MASTER CAUTION CANCEL |
| 26 2 17 11 |
| FWCCLPB 26 1 17 11 FWC CLEAR PB ACTIVATED |
| 26 2 17 11 |
| GLA 29 1 100 00 APU GEN LOAD SYS. 1 |
| 29 2 100 00 |
| GLE1 29 1 77 01 % GEN1 LOAD SYS. 1 |
| 29 2 77 01 |
| GLE2 29 1 77 10 % GEN1 LOAD SYS. 2 |
| 29 2 77 10 |
| GLS1 25 1 174 01 DDM ILS1 GLIDESLOPE DEVIATION SYS. 1 |
| 25 2 174 01 |
| GLS2 25 1 174 10 DDM ILS1 GLIDESLOPE DEVIATION SYS. 2 |
| 25 2 174 10 |
| GPWS270 23 1 270 00 GPWS ALERTS |
| GPWS271 23 1 271 00 GPWS MODES |
| GS 04 1 312 01 KTS GROUND SPEED SYS. 1 |
| 04 2 312 10 |
| GS1 04 1 312 01 KTS GROUND SPEED SYS. 1 |
| GS1S 04 1 312 01 KTS GROUND SPEED SYS. 1 |
| GS2 04 1 312 10 KTS GROUND SPEED SYS. 2 |
| GS2S 04 1 312 10 KTS GROUND SPEED SYS. 2 |
| GWDARLSH 02 1 75 00 LBS GROSS WEIGHT (LBS.) LSH DAR |
| 02 2 75 00 |
| GWDARMSH 02 1 75 00 LBS GROSS WEIGHT (LBS.) MSH DAR |
| 02 2 75 00 |
| GWKG 02 1 75 00 KG GROSS WEIGHT (KGS.) |
| 02 2 75 00 |
| GWKG1 02 1 75 00 GROSS WEIGHT (KGS.) SYS. 1 |
| GWKG2 02 1 75 00 GROSS WEIGHT (KGS.) SYS. 2 |
| HIGHSPDT 01 1 307 00 KTS HIGH SPEED TARGET MARGIN |
| 01 2 307 00 |
| HPT1 A1 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPT1S A1 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPT2 A1 1 306 10 % SELECTED HPTC POSITION SYS.2 |
| HPT2S A1 1 306 10 % SELECTED HPTC POSITION SYS.2 |
| HPTSEL1 A1 1 306 01 % SELECTED HPTC POSITION SYS.1 |
| HPTSEL2 A1 1 306 10 % SELECTED HPTC POSITION SYS.2 |
| HUDINST 29 1 5 00 HUD INSTALLED |
| 29 2 5 00 |
| HUDINST1 26 1 1 01 SINGLE OR NO HUD INSTALLED |
| 26 2 1 10 |
| IAOA1 06 1 221 01 DEG INDICATED ANGLE OF ATTACK SYS. 1 |
| IAOA2 06 1 221 10 DEG INDICATED ANGLE OF ATTACK SYS. 2 |
| ICESW272 5D 1 61 10 DSW ANTI-ICE |
| ICESW27F 5D 1 61 10 DSW ANTI-ICE UNFILTERED |
| ICESW282 5D 1 61 10 DSW ANTI-ICE |
| ICESW28F 5D 1 61 10 DSW ANTI-ICE UNFILTERED |
| IGV 7A 1 130 01 DEG IGV POSITION |
| ILS1RUNH 25 1 105 01 DEG ILS1 RUNWAY HEADING |
| 25 2 105 01 |
| INSTB121 7E 1 155 00 ACARS INSTALLED SYS. 1 |
| INSTBALL 7E 1 155 00 CFDIU LABEL 155 |
| IVV 04 1 365 01 FT/MIN INERTIAL VERTICAL SPEED |
| 04 2 365 10 |
| IVV01 04 1 365 01 FT/MIN INERTIAL VERTICAL SPEED SYS. 1 |
| IVV02 04 1 365 10 FT/MIN INERTIAL VERTICAL SPEED SYS. 2 |
| IVVDMC 25 1 104 01 FT/MIN SELECTED VERTICAL SPEED |
| 25 2 104 10 |
| L066TOF1 7C 1 66 01 DERATE T/OFF LIMIT MODE SELECTED |
| 7C 2 66 10 |
| LAF 6C 1 41 01 LOAD ALLEVIATION ACTIVE (LAF) |
| 6C 2 41 10 |
| LATA1 29 1 332 01 G LATERAL ACCELERATION SYS. 1 |
| 29 2 332 01 |
| LAWB111 6C 1 40 01 NORMAL PITCH LAW |
| 6C 2 40 10 |
| LAWB121 6C 1 40 01 PITCH ALT 1 LAW |
| 6C 2 40 10 |
| LAWB131 6C 1 40 01 PITCH ALT 2 LAW |
| 6C 2 40 10 |
| LAWB151 6C 1 40 01 PITCH DIRECT LAW |
| 6C 2 40 10 |
| LCDT 7A 1 74 01 DEG C BLEED AIR TEMP |
| LCIT 7A 1 110 01 DEG C LOAD COMPRESSOR INLET TEMPERATURE |
| LDGWALL1 6D 1 21 01 MAIN (LH&RH) LANDING GEAR COMP SYS. 1 |
| LDGWB111 6D 1 21 01 MAIN (LH&RH) LANDING GEAR COMP SYS. 1 |
| 6D 2 21 10 |
| LDGWB121 6D 1 21 01 NOSE LANDING GEAR COMPRESSED SYS. 1 |
| 6D 2 21 10 |
| LDGWB131 6D 1 21 01 LH LANDING GEAR COMPRESSED SYS. 1 |
| 6D 2 21 10 |
| LDGWB141 6D 1 21 01 RH LANDING GEAR COMPRESSED SYS. 1 |
| 6D 2 21 10 |
| LDGWB151 6D 1 21 01 MAIN (LH&RH) LANDING GEAR DWNLCK SYS. 1 |
| LDGWB161 6D 1 21 01 LH BOGIE BEAM NOT ALIGNED SYS. 1 |
| LDGWB171 6D 1 21 01 RH BOGIE BEAM NOT ALIGNED SYS. 1 |
| LDGWB201 6D 1 21 01 SYSTEM IN CONTROL SYS. 1 |
| LDGWB211 6D 1 21 01 L/G RETR SOLENOID SUPPLY -VE SYS. 1 |
| LDGWB221 6D 1 21 01 L/G RETR SOLENOID SUPPLY 28 V SYS. 1 |
| LDGWB231 6D 1 21 01 L/G EXT SOLENOID SUPPLY -VE SYS. 1 |
| LDGWB241 6D 1 21 01 L/G EXT SOLENOID SUPPLY 28 V SYS. 1 |
| LDGWB251 6D 1 21 01 DOORS OPEN SOLENOID SPLY -VE SYS. 1 |
| LDGWB261 6D 1 21 01 DOORS OPEN SOLENOID SPLY 28 V SYS. 1 |
| LDGWB271 6D 1 21 01 DOORS CLOSE SOLENOID SPLY -VE SYS. 1 |
| LDGWB281 6D 1 21 01 DOORS CLOSE SOLENOID SPLY 28 V SYS. 1 |
| LDGWB291 6D 1 21 01 SYSTEM FAILED SYS. 1 |
| LGC02214 6D 1 22 01 DISCRETE WORD |
| 6D 2 22 10 |
| LOC1 25 1 173 01 DDM ILS1 LOCALIZER DEVIATION SYS. 1 |
| 25 2 173 01 |
| LOC2 25 1 173 10 DDM ILS1 LOCALIZER DEVIATION SYS. 2 |
| 25 2 173 10 |
| LONA1 29 1 331 01 G LONGITUDINAL ACCELERATION SYS. 1 |
| 29 2 331 01 |
| LOPP1 6E 1 331 01 DEG LEFT BRAKE PEDAL POSITION SYS. 1 |
| LOPP2 6E 1 331 10 DEG LEFT BRAKE PEDAL POSITION SYS. 2 |
| LOWSPDT 01 1 306 00 KTS LOW SPEED TARGET MARGIN |
| 01 2 306 00 |
| LPT1 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPT1S 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPT2 7C 1 307 10 % SELECTED LPTC POSITION SYS.2 |
| LPT2S 7C 1 307 10 % SELECTED LPTC POSITION SYS.2 |
| LPTSEL1 7C 1 307 01 % SELECTED LPTC POSITION SYS.1 |
| LPTSEL2 7C 1 307 10 % SELECTED LPTC POSITION SYS.2 |
| MH1 04 1 320 01 MAGNETIC HEADING |
| 04 2 320 10 |
| MN 06 1 205 01 MACH MACH |
| 06 2 205 10 |
| MN1 06 1 205 01 MACH SYS. 1 |
| MN1S 06 1 205 01 MACH SYS. 1 |
| MN2 06 1 205 10 MACH SYS. 2 |
| MN2S 06 1 205 10 MACH SYS. 2 |
| MW2ALL1 7C 1 351 01 MAINTENANCE DATA #2 |
| MW2ALL2 7C 1 351 10 MAINTENANCE DATA #2 |
| MW2B291 7C 1 351 01 FUEL OFF WRAPAROUND-FAILED SYS. 1 |
| MW2B292 7C 1 351 10 FUEL OFF WRAPAROUND-FAILED SYS. 2 |
| N11 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 1 |
| N11S 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 1 |
| N12 7C 1 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 2 |
| N12S 7C 1 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 2 |
| N1C1 7C 1 341 01 % RPM N1 COMMAND SYS. 1 |
| N1C2 7C 1 341 10 % RPM N1 COMMAND SYS. 2 |
| N1MX1 7C 1 342 01 % RPM N1 MAXIMUM SYS. 1 |
| N1MX2 7C 1 342 10 % RPM N1 MAXIMUM SYS. 2 |
| N1SEL1 7C 1 346 01 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 1 |
| N1SEL2 7C 1 346 10 % RPM N1 ACTUAL (LOW ROTOR SPEED) SYS. 2 |
| N1T1 7C 1 343 01 % RPM N1 TARGET FEEDBACK |
| N21 7C 1 344 01 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 1 |
| N21S 7C 1 344 01 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 1 |
| N22 7C 1 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 2 |
| N22S 7C 1 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 2 |
| N2SEL1 7C 1 344 01 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 1 |
| N2SEL2 7C 1 344 10 % RPM N2 ACTUAL (HIGH ROTOR SPEED) SYS. 2 |
| NA 7A 1 176 01 % RPM RPM |
| NWCFO 6E 1 341 01 DEG NWS F/O ORDER |
| 6E 2 341 10 |
| NWSA 6E 1 336 01 DEG NOSE WHEEL SYS ORDER ANGLE |
| 6E 2 336 10 |
| NWSCO 6E 1 340 01 DEG NWS CAPTAIN ORDER |
| 6E 2 340 10 |
| OILPRS1 26 1 17 01 ENG 1 OIL LOW PRESSURE |
| 26 2 17 01 |
| OILPRS2 26 1 17 10 ENG 2 OIL LOW PRESSURE |
| 26 2 17 10 |
| OIP1 26 1 317 01 PSI ENG 1 OIL PRESSURE |
| 26 2 317 01 |
| OIP2 26 1 317 10 PSI ENG 2 OIL PRESSURE |
| 26 2 317 10 |
| OIQ1 29 1 73 11 QUART ENG 1 OIL QUANTITY SYS. 1 |
| 29 2 73 11 |
| OIQ2 29 1 73 00 QUART ENG 2 OIL QUANTITY SYS. 1 |
| 29 2 73 00 |
| OIQDAR1 26 1 73 01 QUART ENG 1 OIL QUANTITY |
| 26 2 73 01 |
| OIQDAR2 26 1 73 10 QUART ENG 2 OIL QUANTITY |
| 26 2 73 10 |
| OIT1 26 1 316 01 DEG C ENG 1 OIL TEMPERATURE |
| 26 2 316 01 |
| OIT2 26 1 316 10 DEG C ENG 2 OIL TEMPERATURE |
| 26 2 316 10 |
| OTA 7A 1 247 01 DEG C APU OIL SUMP TEMP |
| OVP1 5C 1 153 01 % OUTFLOW VALVE POS SYS. 1 |
| OVP2 5C 1 153 10 % OUTFLOW VALVE POS SYS. 2 |
| OVPS 29 1 153 11 % OUTFLOW VALVE POS SDAC |
| 29 2 153 11 |
| P251 7C 1 262 01 PSIA P2.5 (LPC EXIT PRESSURE) SYS.1 |
| P252 7C 1 262 10 PSIA P2.5 (LPC EXIT PRESSURE) SYS. 2 |
| P2A 7A 1 112 01 BAR INLET PRESSURE |
| P31 7C 1 264 01 PSIA PB BURNER PRESSURE SYS. 1 |
| P32 7C 1 264 10 PSIA PB BURNER PRESSURE SYS. 2 |
| P3SEL1 7C 1 264 01 PSIA PB BURNER PRESSURE SYS. 1 |
| P3SEL2 7C 1 264 10 PSIA PB BURNER PRESSURE SYS. 2 |
| PBV1 8E 1 112 11 % PACK BYPASS VALVE POSITION SYS. 1 |
| PBV2 8E 1 112 00 % PACK BYPASS VALVE POSITION SYS. 2 |
| PCP1 6C 1 305 01 DEG PITCH CAPT CMD POSITION |
| 6C 2 305 10 |
| PCP2 6C 1 306 01 DEG PITCH F/O CMD POSITION |
| 6C 2 306 10 |
| PCSWALL1 5C 1 57 01 PRESSURE CONTROLLER STATUS WORD SYS.1 |
| PCSWALL2 5C 1 57 10 PRESSURE CONTROLLER STATUS WORD SYS. 2 |
| PCSWB111 5C 1 57 01 SYSTEM IN CONTROL SYS. 1 |
| PCSWB112 5C 1 57 10 SYSTEM IN CONTROL SYS. 2 |
| PCSWB141 5C 1 57 01 EXCESSIVE CABIN ALTITUDE - WARN SYS. 1 |
| PCSWB142 5C 1 57 10 EXCESSIVE CABIN ALTITUDE - WARN SYS. 2 |
| PDC 5C 1 144 01 PSI CABIN DIFF. PRESSURE SYS. 1 |
| 5C 2 144 10 |
| PDC1 5C 1 144 01 PSI CABIN DIFF. PRESSURE SYS. 1 |
| PDC2 5C 1 144 10 PSI CABIN DIFF. PRESSURE SYS. 2 |
| PDCA 06 1 246 01 MB CORR AVE STATIC PRESSURE ADC |
| 06 2 246 10 |
| PDCS 29 1 152 11 PSI CABIN PRESSURE SDAC |
| 29 2 152 11 |
| PDE1 6F 1 143 01 PSI PRECOOLER ENG 1 INLET PRESS SYS. 1 |
| 6F 2 143 10 |
| PDE2 6F 1 142 01 PSI PRECOOLER ENG 2 INLET PRESS SYS. 1 |
| 6F 2 142 10 |
| PFAD 7A 1 4 01 HEX PERFORMANCE ADJUSTMENTS SYS. 1 |
| PFADMSB 7A 1 4 01 HEX PERFORMANCE ADJUSTMENTS SYS. 1 |
| PFLKG 8E 1 126 11 KG/SEC PACK FLOW SYS. 1 |
| PFRKG 8E 1 126 00 KG/SEC PACK FLOW SYS. 2 |
| PHA1 3D 1 226 01 DEG N1 PHASE UNBAL BRG1 OR TRF EN1 SYS. 1 |
| PHA2 3D 1 226 10 DEG N1 PHASE UNBAL BRG1 OR TRF EN2 SYS. 1 |
| PHASE1 26 1 126 01 FLIGHT PHASES (ACQUIRED) |
| 26 2 126 01 |
| PHASEGSM 26 1 126 01 FLIGHT PHASES FOR GSM |
| PHT1 3D 1 226 11 DEG N1 PHASE UNBAL TRF EN1 SYS. 1 |
| PHT2 3D 1 226 00 DEG N1 PHASE UNBAL TRF EN2 SYS. 1 |
| PO1 7C 1 114 01 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.1 |
| PO2 7C 1 114 10 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.2 |
| POSEL1 7C 1 114 01 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.1 |
| POSEL2 7C 1 114 10 PSIA SELECTED PO (AMBIENT PRESSURE) SYS.2 |
| PS131 7C 1 127 01 PSIA PS13 STATIC AIR PRESSURE AT 1.3 SYS.1 |
| PS132 7C 1 127 10 PSIA PS13 STATIC AIR PRESSURE AT 1.3 SYS.2 |
| PSB1 26 1 320 01 ENG 1 NO. 4 BEARING PRESSURE |
| 26 2 320 01 |
| PSB2 26 1 320 10 ENG 2 NO. 4 BEARING PRESSURE |
| 26 2 320 10 |
| PSW1111 8E 1 62 11 FLOW CONTROL VALVE STATUS CLOSE SYS. 1 |
| PSW1112 8E 1 62 00 FLOW CONTROL VALVE STATUS CLOSE SYS. 2 |
| PSW1131 8E 1 62 11 PACK COMPRESSOR OUTLET TEMP SYS. 1 |
| PSW1132 8E 1 62 00 PACK COMPRESSOR OUTLET TEMP SYS. 2 |
| PSW1141 8E 1 62 11 PACK COMPRESSOR OUTLET TEMP SYS. 1 |
| PSW1142 8E 1 62 00 PACK COMPRESSOR OUTLET TEMP SYS. 2 |
| PT 7A 1 166 01 BAR BLEED AIR PRESSURE |
| PT21 7C 1 131 01 PSIA PT2 (FAN INLET PRESSURE) SYS. 1 |
| PT21S 7C 1 131 01 PSIA PT2 (FAN INLET PRESSURE) SYS. 1 |
| PT22 7C 1 131 10 PSIA PT2 (FAN INLET PRESSURE) SYS. 2 |
| PT22S 7C 1 131 10 PSIA PT2 (FAN INLET PRESSURE) SYS. 2 |
| PTCH1 04 1 324 01 DEG PITCH ANGLE SYS. 1 |
| 04 2 324 10 |
| QARLOW 17 1 350 00 QAR TAPE LOW |
| QDBCYC 25 1 230 00 SELECTED DATABASE CYCLE |
| 25 2 230 00 |
| QDBMO1 25 1 230 00 DATA BASE MONTH 1ST DIGIT |
| 25 2 230 00 |
| QDBMO2 25 1 230 00 DATA BASE MONTH 2ND DIGIT |
| 25 2 230 00 |
| QDBUPD1 25 1 230 00 NAV DATA BASE UPDATE |
| QDBUPDDA 25 1 230 00 DATA BASE DAY |
| 25 2 230 00 |
| QDBUPDMO 25 1 230 00 DATA BASE MONTH |
| 25 2 230 00 |
| QE1I46A 7C 1 46 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE1I46B 7C 1 46 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE1I46C 7C 1 46 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE1I47A 7C 1 47 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE1I47B 7C 1 47 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE1I47C 7C 1 47 01 ENG 1 ID LSD (FOR QAR RCDG) |
| QE2I46A 7C 1 46 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QE2I46B 7C 1 46 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QE2I46C 7C 1 46 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QE2I47A 7C 1 47 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QE2I47B 7C 1 47 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QE2I47C 7C 1 47 10 ENG 2 ID LSD (FOR QAR RCDG) |
| QFDIUDB1 17 1 230 01 FDIU DATA BASE UPDATE |
| QFLTPH1 26 1 126 01 FLIGHT PHASE FROM FWC FOR QAR RCDG. |
| QIAW1141 26 1 11 01 ENG1 POS. INDICATION FAULT SYS. 1 |
| 26 2 11 01 |
| QIAW2141 26 1 11 10 ENG2 POS. INDICATION FAULT SYS. 1 |
| 26 2 11 10 |
| QILS11A 25 1 33 01 ILS 1 FREQUENCY SYS. 1 |
| 25 2 33 01 |
| QILS11B 25 1 33 01 ILS 1 FREQUENCY SYS. 1 |
| 25 2 33 01 |
| QILS11C 25 1 33 01 ILS 1 FREQUENCY SYS. 1 |
| 25 2 33 01 |
| QILS11D 25 1 33 01 ILS 1 FREQUENCY SYS. 1 |
| 25 2 33 01 |
| QILS21A 25 1 33 10 ILS 2 FREQUENCY SYS. 1 |
| 25 2 33 10 |
| QILS21B 25 1 33 10 ILS 2 FREQUENCY SYS. 1 |
| 25 2 33 10 |
| QILS21C 25 1 33 10 ILS 2 FREQUENCY SYS. 1 |
| 25 2 33 10 |
| QILS21D 25 1 33 10 ILS 2 FREQUENCY SYS. 1 |
| 25 2 33 10 |
| QINALT1 04 1 361 NA FT INERTIAL ALTITUDE SYS 1 (QAR) |
| QINALT1S 04 1 361 NA FT INERTIAL ALTITUDE SYS 1 (QAR) |
| QINALT2 04 1 361 NA FT INERTIAL ALTITUDE SYS 2 (QAR) |
| QINALT2S 04 1 361 NA FT INERTIAL ALTITUDE SYS 2 (QAR) |
| QLATA1 29 1 332 01 LATERAL ACCELERATION AT 32/SEC |
| QLATP 04 1 310 NA DEG PRESENT POSITION LATITUDE (VARIABLE) |
| 04 2 310 NA |
| QLATP1 04 1 310 NA DEG PRESENT POSITION LATITUDE (QAR) |
| QLATP2 04 1 310 NA DEG PRESENT POSITION LATITUDE (QAR) |
| QLATPGSM 04 1 310 NA DEG PRESENT POSITION LATITUDE GSM |
| 04 2 310 NA |
| QLDGA291 6D 1 20 01 GEAR LEVER SELECTED DOWN |
| 6D 2 20 10 |
| QLDGW111 6D 1 21 01 MAIN (LH&RH) LANDING GEAR COMP SYS.1(32) |
| QLDGW131 6D 1 21 01 LH LANDING GEAR COMPRESSED SYS. 1 (32) |
| QLDGW141 6D 1 21 01 RH LANDING GEAR COMPRESSED SYS. 1 (32) |
| QLONA1 29 1 331 01 LONGITUDINAL ACCELERATION AT 32/SEC |
| QLONP 04 1 311 NA DEG PRESENT POSITION LONGITUDE (VARIABLE) |
| 04 2 311 NA |
| QLONP1 04 1 311 NA DEG PRESENT POSITION LONGITUDE (QAR) |
| QLONP2 04 1 311 NA DEG PRESENT POSITION LONGITUDE (QAR) |
| QLONPGSM 04 1 311 NA DEG PRESENT POSITION LONGITUDE GSM |
| 04 2 311 NA |
| QNZ1 04 1 364 01 VERTICAL ACCEL.(FOR LOAD REPORT TRIGGER) |
| QPTCHA01 04 1 324 01 PITCH ANGLE (LOAD REPORT TRIG) |
| QPTCR1 04 1 326 01 DEG/SEC BODY AXIS PITCH RATE (LOAD REPORT TRIG) |
| 04 2 326 10 |
| QRALT1 25 1 164 01 RADIO HEIGHT (FOR LOAD REPORT TRIGGER) |
| QROLLA01 04 1 325 01 ROLL ANGLE SYS. 1 (LOAD REPORT TRIGGER) |
| QROLR1 04 1 327 01 DEG/SEC BODY AXIS ROLL RATE (LOAD REPORT TRIG) |
| 04 2 327 10 |
| QSW10111 25 1 302 01 CLIMB SYS. 1 |
| 25 2 302 10 |
| QSW10121 25 1 302 01 DECENT SYS. 1 |
| 25 2 302 10 |
| QSW10131 25 1 302 01 IMMEDIATE SYS. 1 |
| 25 2 302 10 |
| QSW10141 25 1 302 01 OPEN SYS. 1 |
| 25 2 302 10 |
| QSW10151 25 1 302 01 PITCH TRACK OFF SYS. 1 |
| 25 2 302 10 |
| QSW10161 25 1 302 01 PITCH GO AROUND MODE SYS. 1 |
| 25 2 302 10 |
| QSW10171 25 1 302 01 VERTICAL SPEED MODE SYS. 1 |
| 25 2 302 10 |
| QSW10181 25 1 302 01 FPA MODE SYS. 1 |
| 25 2 302 10 |
| QSW10191 25 1 302 01 ALT MODE SYS. 1 |
| 25 2 302 10 |
| QSW10201 25 1 302 01 TRK SYS. 1 |
| 25 2 302 10 |
| QSW10211 25 1 302 01 CAPT SYS. 1 |
| 25 2 302 10 |
| QSW10221 25 1 302 01 G/S SYS. 1 |
| 25 2 302 10 |
| QSW10231 25 1 302 01 FINAL DESCENT MODE SYS. 1 |
| 25 2 302 10 |
| QSW10241 25 1 302 01 EXPEDITE MODE SYS. 1 |
| 25 2 302 10 |
| QSW10251 25 1 302 01 FLARE MODE SYS. 1 |
| 25 2 302 10 |
| QSW10261 25 1 302 01 FMA DASH DISPLAY |
| 25 2 302 10 |
| QSW10262 25 1 302 01 FMA SPD/MACH PRESET DISPLAY |
| 25 2 302 10 |
| QSW11181 25 1 305 01 METRIC/ENGLISH SYSTEM (WEIGHT) |
| 25 2 305 10 |
| QSW11271 25 1 305 01 METRIC/ENGLISH SYSTEM (DEGREES) |
| 25 2 305 10 |
| QSW11281 25 1 305 01 NO DATA FROM EEC1 SYS. 1 |
| 25 2 305 10 |
| QSW11291 25 1 305 01 NO DATA FROM EEC2 SYS. 1 |
| 25 2 305 10 |
| QSW1B111 25 1 270 01 ENG 1 REV UNLOCK (AMBER) SYS. 1 |
| 25 2 270 10 |
| QSW1B121 25 1 270 01 ENG 2 REV UNLOCK (AMBER) SYS. 1 |
| 25 2 270 10 |
| QSW1B131 25 1 270 01 ENG 1 REV DEPLOYED (GREEN) SYS. 1 |
| 25 2 270 10 |
| QSW1B141 25 1 270 01 ENG 2 REV DEPLOYED (GREEN) SYS. 1 |
| 25 2 270 10 |
| QSW1B151 25 1 270 01 ECAM DU 1 ANOMALY SYS. 1 |
| 25 2 270 10 |
| QSW1B161 25 1 270 01 ECAM DU 2 ANOMALY SYS. 1 |
| 25 2 270 10 |
| QSW1B241 25 1 270 01 AUTO LAND WARNING |
| 25 2 270 10 |
| QSW1B251 25 1 270 01 ECU1 CHANNEL B IN CONTROL SYS. 1 |
| 25 2 270 10 |
| QSW1B261 25 1 270 01 ECU2 CHANNEL B IN CONTROL SYS. 1 |
| 25 2 270 10 |
| QSW20181 26 1 16 01 GPWS MODES ON SYS. 1 |
| 26 2 16 01 |
| QSW21181 26 1 16 10 G/S VISUAL ALERT ON SYS. 1 |
| 26 2 16 10 |
| QSW25191 6C 1 40 01 ELAC1 PITCH FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25201 6C 1 40 01 ELAC1 ROLL FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25211 6C 1 40 01 ELAC2 PITCH FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25221 6C 1 40 01 ELAC2 ROLL FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25231 6C 1 40 01 ELAC1 FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25241 6C 1 40 01 ELAC2 FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25251 6C 1 40 01 SEC1 FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25261 6C 1 40 01 SEC2 FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW25291 6C 1 40 01 SEC3 FAULT SYS. 1 |
| 6C 2 40 10 |
| QSW26281 6C 1 41 01 CAPT SIDESTICK INOPERATIVE SYS. 1 |
| 6C 2 41 10 |
| QSW26291 6C 1 41 01 F/O SIDESTICK INOPERATIVE SYS. 1 |
| 6C 2 41 10 |
| QSW27111 6C 1 42 01 LH AIL BLUE AVAIL SYS. 1 |
| 6C 2 42 10 |
| QSW27121 6C 1 42 01 EFCS STATUS WORD |
| 6C 2 42 10 |
| QSW27131 6C 1 42 01 EFCS STATUS WORD |
| 6C 2 42 10 |
| QSW27141 6C 1 42 01 EFCS STATUS WORD |
| 6C 2 42 10 |
| QSW2B131 25 1 271 01 DISCRETE WORD |
| 25 2 271 10 |
| QSW2B151 25 1 271 01 ATS ENGAGED SYS. 1 |
| 25 2 271 10 |
| QSW2B161 25 1 271 01 ATS ACTIVE SYS. 1 |
| 25 2 271 10 |
| QSW2B171 25 1 271 01 ATS SPEED MACH MODE SYS. 1 |
| 25 2 271 10 |
| QSW2B181 25 1 271 01 ATS RETARD MODE ACTIVATED SYS. 1 |
| 25 2 271 10 |
| QSW2B191 25 1 271 01 THRUST N1 MODE SYS. 1 |
| 25 2 271 10 |
| QSW2B201 25 1 271 01 THRUST EPR MODE SYS. 1 |
| 25 2 271 10 |
| QSW2B211 25 1 271 01 ATS ALPHA FLOOR |
| 25 2 271 10 |
| QSW2B221 25 1 271 01 DISCRETE WORD |
| 25 2 271 10 |
| QSW2B251 25 1 271 01 HEADING SELECTION SYS. 1 |
| 25 2 271 10 |
| QSW30181 29 1 1 00 RH WING ANTI ICE VALVE CLOSED SYS. 1 |
| 29 2 1 00 |
| QSW3018F 29 1 1 00 RH WING ANTI ICE VALVE CLOSED UNFILTERED |
| 29 2 1 00 |
| QSW30191 29 1 1 00 ENG2 ANTI ICE VALVE FAULT SYS. 1 |
| QSW31181 29 1 1 11 LH WING ANTI ICE VALVE CLOSED SYS. 1 |
| 29 2 1 11 |
| QSW3118F 29 1 1 11 LH WING ANTI ICE VALVE CLOSED UNFILTERED |
| 29 2 1 11 |
| QSW31191 29 1 1 11 ENG1 ANTI ICE VALVE FAULT SYS. 1 |
| QSW33281 29 1 2 01 HF1 EMITTING SYS. 1 |
| 29 2 2 01 |
| QSW33291 29 1 2 01 VHF1 EMITTING SYS. 1 |
| 29 2 2 01 |
| QSW34201 29 1 2 10 AC2 BUS OFF SYS. 1 |
| 29 2 2 10 |
| QSW34281 29 1 2 10 HF2 EMITTING SYS. 1 |
| 29 2 2 10 |
| QSW34291 29 1 2 10 VHF2 EMITTING SYS. 1 |
| 29 2 2 10 |
| QSW3516 29 1 2 11 APU MASTER SWITCH P/B OFF |
| QSW35161 29 1 2 11 APU MASTER SWITCH P/B OFF SYS. 1 |
| QSW35291 29 1 2 11 VHF3 EMITTING SYS. 1 |
| 29 2 2 11 |
| QSW36181 29 1 3 01 ENG1 ANTI ICE P/B ON SYS. 1 |
| 29 2 3 01 |
| QSW36211 29 1 3 01 PACK 1 FLOW CTL VALVE NOT CLOSED |
| 29 2 3 01 |
| QSW36212 29 1 3 10 PACK 2 FLOW CTL VALVE NOT CLOSED |
| 29 2 3 10 |
| QSW36221 29 1 3 11 WING ANTI ICE P/B OFF SYS. 1 |
| 29 2 3 11 |
| QSW37181 29 1 3 10 ENG2 ANTI ICE P/B ON SYS. 1 |
| 29 2 3 10 |
| QSW38291 29 1 4 01 DC1 BUS OFF SYS. 1 |
| 29 2 4 01 |
| QSW39291 29 1 4 10 DC2 BUS OFF SYS. 1 |
| 29 2 4 10 |
| QSW3B161 25 1 272 01 DMC MARK2 IDENT SYS. 1 |
| 25 2 272 10 |
| QSW3B221 25 1 272 01 DMC1 INVALID |
| 25 2 272 10 |
| QSW3B231 25 1 272 01 DMC2 INVALID |
| 25 2 272 10 |
| QSW3B241 25 1 272 01 DMC3 INVALID |
| 25 2 272 10 |
| QSW3B251 25 1 272 01 DMC3 XFR SYS. 1 |
| QSW3B252 25 1 272 10 DMC3 XFR SYS. 2 |
| QSW3B261 25 1 272 01 PFD/ND XFR SYS. 1 |
| QSW3B262 25 1 272 10 PFD/ND XFR SYS. 2 |
| QSW3B271 25 1 272 01 ECAM/ND XFR SYS. 1 |
| QSW3B272 25 1 272 10 ECAM/ND XFR SYS. 2 |
| QSW42161 29 1 55 01 XFEED VALVE FULLY CLOSED SYS. 1 |
| 29 2 55 01 |
| QSW42162 29 1 55 10 XFEED VALVE FULLY CLOSED SYS. 2 |
| 29 2 55 10 |
| QSW43111 29 1 67 01 ENG1 OPV NOT FULLY OPEN |
| 29 2 67 01 |
| QSW43112 29 1 66 01 ENG2 OPV NOT FULLY OPEN |
| 29 2 66 01 |
| QSW43151 29 1 66 01 ENG2 HP VALVE FULLY CLOSED SYS. 1 |
| 29 2 66 01 |
| QSW43171 29 1 66 01 ENG2 PRESS REG VALVE FULLY CLOSED SYS. 1 |
| 29 2 66 01 |
| QSW43211 29 1 66 01 ENG2 STARTER VALVE NOT CLOSED SYS. 1 |
| 29 2 66 01 |
| QSW44151 29 1 67 01 ENG1 HP VALVE FULLY CLOSED SYS. 1 |
| 29 2 67 01 |
| QSW44171 29 1 67 01 ENG1 PRESS REG VALVE FULLY CLOSED SYS. 1 |
| 29 2 67 01 |
| QSW44211 29 1 67 01 ENG1 STARTER VALVE NOT CLOSED SYS. 1 |
| 29 2 67 01 |
| QSW4B111 25 1 273 01 PLAN MODE SYS. 1 |
| QSW4B112 25 1 273 10 PLAN MODE SYS. 2 |
| QSW4B121 25 1 273 01 ARC SYS. 1 |
| QSW4B122 25 1 273 10 ARC SYS. 2 |
| QSW4B131 25 1 273 01 ROSE - NAV SYS. 1 |
| QSW4B132 25 1 273 10 ROSE - NAV SYS. 2 |
| QSW4B141 25 1 273 01 ROSE - VOR SYS. 1 |
| QSW4B142 25 1 273 10 ROSE - VOR SYS. 2 |
| QSW4B151 25 1 273 01 ROSE - ILS SYS. 1 |
| QSW4B152 25 1 273 10 ROSE - ILS SYS. 2 |
| QSW4B161 25 1 273 01 10 NM RANGE SYS. 1 |
| QSW4B162 25 1 273 10 10 NM RANGE SYS. 2 |
| QSW4B171 25 1 273 01 20 NM RANGE SYS. 1 |
| QSW4B172 25 1 273 10 20 NM RANGE SYS. 2 |
| QSW4B181 25 1 273 01 40 NM RANGE SYS. 1 |
| QSW4B182 25 1 273 10 40 NM RANGE SYS. 2 |
| QSW4B191 25 1 273 01 80 NM RANGE SYS. 1 |
| QSW4B192 25 1 273 10 80 NM RANGE SYS. 2 |
| QSW4B201 25 1 273 01 160 NM RANGE SYS. 1 |
| QSW4B202 25 1 273 10 160 NM RANGE SYS. 2 |
| QSW5B111 25 1 274 01 ND1 ANOMALY/OFF |
| QSW5B112 25 1 274 01 DISCRETE WORD |
| QSW5B122 25 1 274 10 DMC 274 BIT 12 SYS 2 |
| QSW5B131 25 1 274 01 OUTER MARKER SYS. 1 |
| 25 2 274 10 |
| QSW5B141 25 1 274 01 MIDDLE MARKER SYS. 1 |
| 25 2 274 10 |
| QSW5B151 25 1 274 01 INNER MARKER (AIRWAYS) SYS. 1 |
| 25 2 274 10 |
| QSW6B111 25 1 275 01 CRUISE IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B112 25 1 275 10 CRUISE IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B121 25 1 275 01 ENG IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B122 25 1 275 10 ENG IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B131 25 1 275 01 BLEED IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B132 25 1 275 10 BLEED IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B141 25 1 275 01 PRESS IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B142 25 1 275 10 PRESS IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B151 25 1 275 01 HYD IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B152 25 1 275 10 HYD IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B161 25 1 275 01 ELEC IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B162 25 1 275 10 ELEC IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B171 25 1 275 01 FUEL IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B172 25 1 275 10 FUEL IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B181 25 1 275 01 APU IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B182 25 1 275 10 APU IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B191 25 1 275 01 COND IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B192 25 1 275 10 COND IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B201 25 1 275 01 DOOR IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B202 25 1 275 10 DOOR IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B211 25 1 275 01 F/CTL IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B212 25 1 275 10 F/CTL IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B221 25 1 275 01 WHEEL IMAGE DISPL OR ADV IN MONO SYS. 1 |
| 25 2 275 10 |
| QSW6B222 25 1 275 10 WHEEL IMAGE DISPL OR ADV IN MONO SYS. 2 |
| QSW6B261 25 1 275 01 STATUS IMAGE DISPLAYED SYS. 1 |
| 25 2 275 10 |
| QSW6B262 25 1 275 10 STATUS IMAGE DISPLAYED SYS. 2 |
| QSW7B131 25 1 276 01 AP1 ENGAGED SYS. 1 |
| 25 2 276 10 |
| QSW7B141 25 1 276 01 AP2 ENGAGED SYS. 1 |
| 25 2 276 10 |
| QSW7B151 25 1 276 01 FD1 ENGAGED SYS 1 |
| 25 2 276 10 |
| QSW7B161 25 1 276 01 FD2 ENGAGED SYS 1 |
| 25 2 276 10 |
| QSW7B201 25 1 276 01 DISCRETE WORD |
| 25 2 276 10 |
| QSW7B211 25 1 276 01 DISCRETE WORD |
| 25 2 276 10 |
| QSW7B221 25 1 276 01 PFD1 ANOMALY/OFF |
| QSW7B231 25 1 276 10 DISCRETE WORD |
| QSW81625 25 1 300 01 LAND CAPABILITY DISPLAY |
| 25 2 300 10 |
| QSW8B111 25 1 300 01 AP INSTINCTIVE DISCONECTION |
| 25 2 300 10 |
| QSW8B141 25 1 300 01 LAND TRACK MODE ACTIVE SYS. 1 |
| 25 2 300 10 |
| QTAT 25 1 211 01 TOTAL AIR TEMPERATURE |
| 25 2 211 10 |
| QTHDG 04 1 314 01 TRUE HEADING (DAR) |
| 04 2 314 10 |
| QVOR11A 25 1 34 01 VOR 1 FREQUENCY SYS. 1 |
| 25 2 34 01 |
| QVOR11B 25 1 34 01 VOR 1 FREQUENCY SYS. 1 |
| 25 2 34 01 |
| QVOR11C 25 1 34 01 VOR 1 FREQUENCY SYS. 1 |
| 25 2 34 01 |
| QVOR11D 25 1 34 01 VOR 1 FREQUENCY SYS. 1 |
| 25 2 34 01 |
| QVOR21A 25 1 34 10 VOR 2 FREQUENCY SYS. 1 |
| 25 2 34 10 |
| QVOR21B 25 1 34 10 VOR 2 FREQUENCY SYS. 1 |
| 25 2 34 10 |
| QVOR21C 25 1 34 10 VOR 2 FREQUENCY SYS. 1 |
| 25 2 34 10 |
| QVOR21D 25 1 34 10 VOR 2 FREQUENCY SYS. 1 |
| 25 2 34 10 |
| QVRTA1 29 1 333 01 G NORMAL ACCELERATION AT 32/SEC |
| QVZBI1 04 1 365 01 INERTIAL VERTICAL SPEED (LOAD RPT TRIG) |
| QYAW01 04 1 330 01 BODY AXIS YAW RATE (LOAD REPORT TRIG) |
| RAC1 7C 1 55 01 % ROTOR ACTIVE CLEARANCE CNTL |
| RAC2 7C 1 55 10 % ROTOR ACTIVE CLEARANCE CNTL |
| RALT1 25 1 164 01 FT RADIO HEIGHT (R/A1) SYS. 1 |
| 25 2 164 01 |
| RALT2 25 1 164 10 FT RADIO HEIGHT (R/A1) SYS. 2 |
| 25 2 164 10 |
| RI1 8E 1 130 11 % PACK RAM AIR INLET POSITION SYS. 1 |
| RI2 8E 1 130 11 % PACK RAM AIR INLET POSITION SYS. 2 |
| RO1 8E 1 130 11 % PACK RAM AIR OUTLET POS. SYS. 1 |
| RO2 8E 1 130 11 % PACK RAM AIR OUTLET POS. SYS. 2 |
| ROLL 04 1 325 01 DEG ROLL ANGLE SYS. 1 |
| 04 2 325 10 |
| ROLLS 04 1 325 01 DEG ROLL ANGLE SYS. 1 |
| 04 2 325 10 |
| ROPP1 6E 1 330 01 DEG RIGHT BRAKE PEDAL POSITION SYS. 1 |
| ROPP2 6E 1 330 10 DEG RIGHT BRAKE PEDAL POSITION SYS. 2 |
| RSP11 6C 1 361 01 DEG LH SPL 1 POSITION |
| 6C 2 361 10 |
| RSP12 6C 1 371 01 DEG RH SPL 1 POSITION |
| 6C 2 371 10 |
| RSP21 6C 1 362 01 DEG LH SPL 2 POSITION SYS. 1 |
| 6C 2 362 10 |
| RSP22 6C 1 372 01 DEG RH SPL 2 POSITION SYS. 2 |
| 6C 2 372 10 |
| RSP31 6C 1 363 01 DEG LH SPL 3 POSITION SYS. 1 |
| 6C 2 363 10 |
| RSP32 6C 1 373 01 DEG RH SPL 3 POSITION SYS. 2 |
| 6C 2 373 10 |
| RSP41 6C 1 364 01 DEG LH SPL 4 POSITION SYS. 1 |
| 6C 2 364 10 |
| RSP42 6C 1 374 01 DEG RH SPL 4 POSITION SYS. 2 |
| 6C 2 374 10 |
| RSP4FLT 6C 1 44 01 1 SPOILER 4 FAULT |
| 6C 2 44 10 |
| RSP51 6C 1 365 01 DEG LH SPL 5 POSITION SYS. 1 |
| 6C 2 365 10 |
| RSP52 6C 1 375 01 DEG RH SPL 5 POSITION SYS. 2 |
| 6C 2 375 10 |
| RSP5FLT 6C 1 44 01 1 SPOILER 5 FAULT |
| 6C 2 44 10 |
| RUDD 29 1 312 00 DEG RUDDER POSITION SYS. 1 |
| 29 2 312 00 |
| RUDT 0A 1 313 00 DEG RUDDER TRIM SYS. 1 |
| 0A 2 313 00 |
| SAT 06 1 213 01 DEG C STATIC AIR TEMPERATURE (BNR) |
| 06 2 213 10 |
| SC1C 29 1 242 01 DEG C SELECTED CKPT COMPT TEMP SYS. 1 |
| 29 2 242 01 |
| SC2C 29 1 244 01 DEG C SEL FWD CAB COMPT TEMP SYS. 1 |
| 29 2 244 01 |
| SC3C 29 1 245 01 DEG C SEL AFT CAB COMPT TEMP SYS. 1 |
| 29 2 245 01 |
| SDC46B26 29 1 46 01 FLAP RELIEF ENGAGED |
| 29 2 46 01 |
| SDS1B161 29 1 1 01 ENG1 OIL FILTER CLOGGED SYS. 1 |
| 29 2 1 01 |
| SDS1B162 29 1 1 10 ENG1 OIL FILTER CLOGGED SYS. 2 |
| 29 2 1 10 |
| SDS1B171 29 1 1 01 ENG1 FUEL FILTER CLOGGED SYS. 1 |
| 29 2 1 01 |
| SDS1B172 29 1 1 10 ENG1 FUEL FILTER CLOGGED SYS. 2 |
| 29 2 1 10 |
| SDS1B191 29 1 1 01 FUEL FIRE VALVE ENG1 FC SYS. 1 |
| 29 2 1 01 |
| SDS1B192 29 1 1 10 FUEL FIRE VALVE ENG2 FC SYS. 1 |
| 29 2 1 10 |
| SELMACH1 25 1 106 01 SELECTED MACH/MANUAL |
| 25 2 206 10 |
| SLAT 1B 1 127 01 DEG SLAT ACTUAL POSITION |
| 1B 2 127 10 |
| SLATINT1 1B 1 127 01 DEG SLAT ACTUAL POSITION SYS. 1 (LEFT) |
| SLATINT2 1B 1 127 10 DEG SLAT ACTUAL POSITION SYS. 2 (RIGHT) |
| SLHDG1 25 1 101 01 DEG SELECTED HEADING |
| 25 2 101 10 |
| SLP1 0A 1 226 00 DEG ESTIMD SIDESLIP SYS. 1 |
| SLP2 0A 1 226 00 DEG ESTIMD SIDESLIP SYS. 2 |
| SLPDAR 0A 1 226 00 DEG ESTIMD SIDESLIP DAR |
| 0A 2 226 00 |
| SLTRK1 25 1 114 01 DEG SELECTED TRACK |
| 25 2 114 10 |
| SPLRB111 6C 1 43 01 LH SPOILER1 OUT |
| 6C 2 43 10 |
| SPLRB121 6C 1 43 01 RH SPOILER1 OUT |
| 6C 2 43 10 |
| SPLRB211 6C 1 43 01 SPOILER 1 POSITION VALID |
| 6C 2 43 10 |
| SPLRB221 6C 1 43 01 SPOILER 2 POSITION VALID |
| 6C 2 43 10 |
| SPLRB231 6C 1 43 01 SPOILER 3 POSITION VALID |
| 6C 2 43 10 |
| SPLRB241 6C 1 43 01 SPOILER 4 POSITION VALID |
| 6C 2 43 10 |
| SPLRB251 6C 1 43 01 SPOILER 5 POSITION VALID |
| 6C 2 43 10 |
| SPLRB271 6C 1 43 01 GROUND SPOILER ARMED |
| 6C 2 43 10 |
| SPLRB281 6C 1 43 01 SPEED BRAKE COMMAND |
| 6C 2 43 10 |
| SST 0A 1 77 00 DEG SIDESLIP TARGET |
| 0A 2 77 00 |
| STAB 6C 1 315 01 DEG STABILIZER POSITION #1 SYS. 1 |
| 6C 2 315 10 |
| STALLSPD 0A 1 246 00 KTS STALL SPEED |
| 0A 2 246 00 |
| SW1ALL1 7C 1 270 01 IAE DISCRETE STATUS WORD #1 |
| SW1ALL2 7C 1 270 10 IAE DISCRETE STATUS WORD #1 |
| SW1B111 7C 1 270 01 IGNITION 1 PRIMARY SELECTED SYS. 1 |
| SW1B112 7C 1 270 10 IGNITION 1 PRIMARY SELECTED SYS. 2 |
| SW1B131 7C 1 270 01 SAV OPEN LOCAL SWITCH SYS. 1 |
| SW1B132 7C 1 270 10 SAV OPEN LOCAL SWITCH SYS. 2 |
| SW1B141 7C 1 270 01 ENGINE POS. IND. - FAILED SYS. 1 |
| SW1B142 7C 1 270 10 ENGINE POS. IND. - FAILED SYS. 2 |
| SW1B151 7C 1 270 01 SAV NOT CLOSED SYS. 1 |
| SW1B152 7C 1 270 10 SAV NOT CLOSED SYS. 2 |
| SW1B161 7C 1 270 01 AUTO DEPOWER - SELECTED SYS. 1 |
| SW1B162 7C 1 270 10 AUTO DEPOWER - SELECTED SYS. 2 |
| SW1B171 7C 1 270 01 MANUAL THRUST MODE - ACTIVE SYS. 1 |
| SW1B172 7C 1 270 10 MANUAL THRUST MODE - ACTIVE SYS. 2 |
| SW1B181 7C 1 270 01 N1 BACKUP MODE - ENGAGED SYS. 1 |
| SW1B182 7C 1 270 10 N1 BACKUP MODE - ENGAGED SYS. 2 |
| SW1B191 7C 1 270 01 REVERSER SYSTEM FAILED SYS. 1 |
| SW1B192 7C 1 270 10 REVERSER SYSTEM FAILED SYS. 2 |
| SW1B201 7C 1 270 01 AUTOTHRUST MODE ACTIVITATED SYS. 1 |
| SW1B202 7C 1 270 10 AUTOTHRUST MODE ACTIVITATED SYS. 2 |
| SW1B211 7C 1 270 01 2.5 BLEED FAILSAFED -FAILSAFE SYS. 1 |
| SW1B212 7C 1 270 10 2.5 BLEED FAILSAFED -FAILSAFE SYS. 2 |
| SW1B221 7C 1 270 01 MEMO MODE ACTIVITATED SYS. 1 |
| SW1B222 7C 1 270 10 MEMO MODE ACTIVITATED SYS. 2 |
| SW1B231 7C 1 270 01 AUTOTHRUST TRA LIMITED SYS. 1 |
| SW1B232 7C 1 270 10 AUTOTHRUST TRA LIMITED SYS. 2 |
| SW1B241 7C 1 270 01 CHANNEL CONTROL - IN CONTROL SYS. 1 |
| SW1B242 7C 1 270 10 CHANNEL CONTROL - IN CONTROL SYS. 2 |
| SW1B251 7C 1 270 01 FLEX TAKEOFF MODE ENGAGED SYS. 1 |
| SW1B252 7C 1 270 10 FLEX TAKEOFF MODE ENGAGED SYS. 2 |
| SW1B261 7C 1 270 01 OIL COOLING SYSTEM - FAILED SYS. 1 |
| SW1B262 7C 1 270 10 OIL COOLING SYSTEM - FAILED SYS. 2 |
| SW1B281 7C 1 270 01 50% THRUST LIMIT ACTIVE SYS. 1 |
| SW1B282 7C 1 270 10 ENGINE NOT RUNNING SYS. 2 |
| SW3191 7C 1 273 01 START MODE SYS. 1 |
| SW3192 7C 1 273 10 START MODE SYS. 2 |
| SW3ALL1 7C 1 272 01 IAE DISCRETE STATUS WORD #3 |
| SW3ALL2 7C 1 272 10 IAE DISCRETE STATUS WORD #3 |
| SW3B121 7C 1 272 01 BUMP/OVERBOOST #1 ENABLE SYS. 1 |
| SW3B122 7C 1 272 10 BUMP/OVERBOOST #1 ENABLE SYS. 2 |
| SW3B131 7C 1 272 01 BUMP/OVERBOOST #2 ENABLE SYS. 1 |
| SW3B132 7C 1 272 10 BUMP/OVERBOOST #2 ENABLE SYS. 2 |
| SW3B141 7C 1 272 01 BUMP/OVERBOOST #3 ENABLE SYS. 1 |
| SW3B142 7C 1 272 10 BUMP/OVERBOOST #3 ENABLE SYS. 2 |
| SW3B191 7C 1 272 01 START MODE SYS. 1 |
| SW3B192 7C 1 272 10 START MODE SYS. 2 |
| SW3B221 7C 1 272 01 BLEED CONFIGURATION K1 - SELEC SYS. 1 |
| SW3B222 7C 1 272 10 BLEED CONFIGURATION K1 - SELEC SYS. 2 |
| SW3B231 7C 1 272 01 BLEED CONFIGURATION K2 - SELEC SYS. 1 |
| SW3B232 7C 1 272 10 BLEED CONFIGURATION K2 - SELEC SYS. 2 |
| SW3B251 7C 1 273 01 4 T/R DOORS STOWED AND LOCKED ENG. 1 |
| SW3B252 7C 1 273 10 4 T/R DOORS STOWED AND LOCKED ENG. 2 |
| SW3B261 7C 1 273 01 BLEED CONFIGURATION K5 - SELEC SYS. 1 |
| SW3B262 7C 1 273 10 BLEED CONFIGURATION K5 - SELEC SYS. 2 |
| SW5B151 7C 1 275 01 N1/N2 CONTROL ACTIVE |
| SW5B152 7C 1 275 10 N1/N2 CONTROL ACTIVE |
| SW5B201 7C 1 275 01 AUTO THRUST ACTIVE |
| SW5B202 7C 1 275 10 AUTO THRUST ACTIVE |
| SW5B261 7C 1 275 01 CHANNEL A ACTIVE |
| SW5B262 7C 1 275 10 N1/N2 CONTROL ACTIVE |
| SW5B271 7C 1 275 01 CHANNEL B ACTIVE |
| SW5B272 7C 1 275 10 N1/N2 CONTROL ACTIVE |
| SW5BALL1 7C 1 275 01 DISCRETE STATUS WORD #5 |
| SW5BALL2 7C 1 273 10 DISCRETE STATUS WORD #5 |
| T12A 7C 1 130 01 DEG C T12 (INLET FAN TEMP) SYS. 1 |
| T12B 7C 1 130 10 DEG C T12 (INLET FAN TEMP) SYS. 2 |
| T251 7C 1 263 01 DEG C T2.5 (LPC EXIT TEMPERATURE) SYS. 1 |
| T252 7C 1 263 10 DEG C T2.5 (LPC EXIT TEMPERATURE) SYS. 2 |
| T25SEL1 7C 1 263 01 DEG C T2.5 (LPC EXIT TEMPERATURE) SYS. 1 |
| T25SEL2 7C 1 263 10 DEG C T2.5 (LPC EXIT TEMPERATURE) SYS. 2 |
| T31 7C 1 265 01 DEG C T3 (HPC EXIT TEMPERATURE) SYS. 1 |
| T32 7C 1 265 10 DEG C T3 (HPC EXIT TEMPERATURE) SYS. 2 |
| T3SEL1 7C 1 265 01 DEG C T3 (HPC EXIT TEMPERATURE) SYS. 1 |
| T3SEL2 7C 1 265 10 DEG C T3 (HPC EXIT TEMPERATURE) SYS. 2 |
| T51 7C 1 260 01 DEG C T5 TEMPERATURE AT POSITION 5 SYS. 1 |
| T52 7C 1 260 10 DEG C T5 TEMPERATURE AT POSITION 5 SYS. 2 |
| TAT 06 1 211 01 DEG C TOTAL AIR TEMPERATURE |
| 06 2 211 10 |
| TAT1 06 1 211 01 TOTAL AIR TEMPERATURE SYS. 1 |
| TAT1S 06 1 211 01 TOTAL AIR TEMPERATURE SYS. 1 |
| TAT2 06 1 211 10 TOTAL AIR TEMPERATURE SYS. 2 |
| TAT2S 06 1 211 10 TOTAL AIR TEMPERATURE SYS. 2 |
| TATSEL1 06 1 211 01 TOTAL AIR TEMPERATURE SYS. 1 |
| TATSEL2 06 1 211 10 TOTAL AIR TEMPERATURE SYS. 2 |
| TCAS2181 25 1 306 01 TCAS RA 1 |
| 25 2 306 10 |
| TCAS2191 25 1 306 01 TCAS RA 2 |
| 25 2 306 10 |
| TCAS2201 25 1 306 01 TCAS RA 3 |
| 25 2 306 10 |
| TCAS2211 25 1 306 01 TCAS RA 4 |
| 25 2 306 10 |
| TCAS2221 25 1 306 01 TCAS RA 5 |
| 25 2 306 10 |
| TCAS2231 25 1 306 01 TCAS RA 6 |
| 25 2 306 10 |
| TCAS2241 25 1 306 01 TCAS RA 7 |
| 25 2 306 10 |
| TCAS2251 25 1 306 01 TCAS RA 8 |
| 25 2 306 10 |
| TCAS2261 25 1 306 01 TCAS RA 9 |
| 25 2 306 10 |
| TCAS2271 25 1 306 01 TCAS RA 10 |
| 25 2 306 10 |
| TCAS2281 25 1 306 01 TCAS RA 11 |
| 25 2 306 10 |
| TCAS2291 25 1 306 01 TCAS RA 12 |
| 25 2 306 10 |
| TCASB141 25 1 307 01 TCAS TA 1 |
| 25 2 307 10 |
| TCASB151 25 1 307 01 TCAS TA 2 |
| 25 2 307 10 |
| TCASB171 25 1 307 01 TCAS SENSITIV 1 |
| 25 2 307 10 |
| TCASB181 25 1 307 01 TCAS SENSITIV 2 |
| 25 2 307 10 |
| TCASB191 25 1 307 01 TCAS SENSITIV 3 |
| 25 2 307 10 |
| THDG1 04 1 44 01 DEG TRUE HEADING 1 |
| THDG2 04 1 44 10 DEG TRUE HEADING 2 |
| THLA11 25 1 133 01 THROTTLE LEVER ANGLE ENGINE 1 |
| 25 2 133 01 |
| THLA21 25 1 133 10 THROTTLE LEVER ANGLE ENGINE 2 |
| 25 2 133 10 |
| TLA1 7C 1 133 01 DEG TLA (THROTTLE RESOLVER ANGLE) SYS. 1 |
| TLA2 7C 1 133 10 DEG TLA (THROTTLE RESOLVER ANGLE) SYS. 2 |
| TLASEL1 7C 1 133 01 DEG TLA (THROTTLE RESOLVER ANGLE) SYS. 1 |
| TLASEL2 7C 1 133 10 DEG TLA (THROTTLE RESOLVER ANGLE) SYS. 2 |
| TN1 26 1 322 01 DEG C ENG 1 NACELLE TEMPERATURE |
| 26 2 322 01 |
| TN2 26 1 322 10 DEG C ENG 2 NACELLE TEMPERATURE |
| 26 2 322 10 |
| TO1A 01 1 41 NA DESTINATION AIRPORT CHAR.# 1 LEFTMOST |
| 01 2 41 NA |
| TO2A 01 1 42 NA DESTINATION AIRPORT CHAR.# 1 LEFTMOST |
| 01 2 42 NA |
| TO3A 01 1 42 NA DESTINATION AIRPORT CHAR.# 3 |
| 01 2 42 NA |
| TO4A 01 1 42 NA DESTINATION AIRPORT CHAR.# 4 RIGHTMOST |
| 01 2 42 NA |
| TP1 8E 1 121 11 DEG C PACK OUTLET TEMPERATURE SYS. 1 |
| TP2 8E 1 121 00 DEG C PACK OUTLET TEMPERATURE SYS. 2 |
| TPOE11 6F 1 141 01 DEG C PRECOOLER ENG 1 OUTLET TEMP SYS. 1 |
| 6F 2 141 10 |
| TPOE21 6F 1 140 01 DEG C PRECOOLER ENG 2 OUTLET TEMP SYS. 1 |
| 6F 2 140 10 |
| TRKANGTR 04 1 313 01 DEG TRACK ANGLE TRUE |
| 04 2 313 10 |
| TW1 8E 1 111 11 DEG C PACK WATER EXTR. TEMPERATURE SYS. 1 |
| TW2 8E 1 111 00 DEG C PACK WATER EXTR. TEMPERATURE SYS. 2 |
| UTCGSM 17 1 125 00 UTC FOR GSM |
| UTCHHA 17 1 125 00 HH UTC HOURS |
| 7E 2 125 00 |
| UTCMMA 17 1 125 00 MM UTC MINUTES |
| 7E 2 125 00 |
| UTCMMO 17 1 150 00 HH UTC MINUTES (OIQH) |
| UTCQAR1 17 1 125 00 UTC RECORDED IN QAR (HH:MM) |
| 7E 2 125 00 |
| UTCSSC 17 1 125 00 .M UTC SECONDS FROM FDIU/CFDIU (10THS MIN.) |
| 7E 2 125 00 |
| UTCSSF 17 1 150 00 SS UTC SECONDS FROM FDIU |
| VA2 5D 1 220 10 % CAB TEMP REG VLV POS GROUP 3 SYS. 2 |
| VACC1 04 1 364 01 G VERTICAL ACCELERATION SYS. 1 |
| VACC1S 04 1 364 01 G VERTICAL ACCELERATION SYS. 1 |
| VACC2 04 1 364 10 G VERTICAL ACCELERATION SYS. 2 |
| VACC2S 04 1 364 10 G VERTICAL ACCELERATION SYS. 2 |
| VAT1 01 1 304 00 VAT (APPR SPEED TARGET) |
| 01 2 304 00 |
| VB11 3D 1 135 01 % N1 VIB ENG 1 BRG1 OR TRF SYS. 1 |
| VB12 3D 1 135 10 % N1 VIB ENG 2 BRG1 OR TRF SYS. 1 |
| VB21 3D 1 136 01 % N2 VIB ENG 1 BRG1 OR TRF SYS. 1 |
| VB22 3D 1 136 10 % N2 VIB ENG 1 BRG1 OR TRF SYS. 1 |
| VBV1 7C 1 71 01 DEG VARIABLE BLEED VALVE PSN SYS.1 |
| VBV2 7C 1 71 10 DEG VARIABLE BLEED VALVE PSN SYS.2 |
| VBVSEL1 7C 1 71 01 DEG VARIABLE BLEED VALVE PSN SYS.1 |
| VBVSEL2 7C 1 71 10 DEG VARIABLE BLEED VALVE PSN SYS.2 |
| VC1 3D 1 230 01 MILS FAN PICK UP N2 TRACK VIBRATION ENG 1 |
| VC2 3D 1 230 10 MILS FAN PICK UP N2 TRACK VIBRATION ENG 2 |
| VCTRENDS 25 1 262 01 KTS VC TRENDS |
| 25 2 262 10 |
| VF2 5D 1 206 10 % CAB TEMP REG VLV POS GROUP 1 SYS. 2 |
| VH1 3D 1 230 11 IPS TRF PICK UP N2 TRACK VIBRATION ENG 1 |
| VH2 3D 1 230 00 IPS TRF PICK UP N2 TRACK VIBRATION ENG 2 |
| VL1 3D 1 227 11 MILS TRF PICK UP N1 TRACK VIBRATION ENG.1 |
| VL2 3D 1 227 00 MILS TRF PICK UP N1 TRACK VIBRATION ENG.2 |
| VLS 25 1 245 01 KTS VLS LANDING SPEED |
| 25 2 245 10 |
| VN1 3D 1 227 01 MILS FAN PICK UP N1 TRACK VIBRATION ENG.1 |
| VN2 3D 1 227 10 MILS FAN PICK UP N1 TRACK VIBRATION ENG.2 |
| VRTA1 29 1 333 01 G NORMAL ACCELERATION SYS. 1 |
| 29 2 333 01 |
| VSCB1 5C 1 150 01 FT/MIN CABIN V/S SYS. 1 |
| VSCB2 5C 1 150 10 FT/MIN CABIN V/S SYS. 2 |
| VSCBS 29 1 150 11 FT/MIN CABIN V/S SDAC |
| 29 2 150 11 |
| VSV1 7C 1 72 01 DEG SELECTED VARIABLE STATOR VANE PSN SYS.1 |
| VSV2 7C 1 72 10 DEG SELECTED VARIABLE STATOR VANE PSN SYS.2 |
| VSVSEL1 7C 1 72 01 DEG SELECTED VARIABLE STATOR VANE PSN SYS.1 |
| VSVSEL2 7C 1 72 10 DEG SELECTED VARIABLE STATOR VANE PSN SYS.2 |
| VW2 5D 1 207 10 % CAB TEMP REG VLV POS GROUP 2 SYS. 2 |
| WARN1113 26 1 126 00 DISCRETE BIT |
| 26 2 126 00 |
| WARN1114 26 1 126 11 MASTER WARNING |
| 26 2 126 11 |
| WARN1115 26 1 126 11 CAPTAIN MASTER CAUTION |
| 26 2 126 11 |
| WARN1117 26 1 126 11 STALL |
| 26 2 126 11 |
| WARN1122 26 1 126 11 FO MASTER WARNING |
| 26 2 126 11 |
| WARN1123 26 1 126 11 FO MASTER CAUTION |
| 26 2 126 11 |
| WARN1125 26 1 126 11 GEAR NOT LOCKED CLEAN |
| 26 2 126 11 |
| WARNB111 26 1 126 11 SDAC 1 VALID SYS. 1 |
| 26 2 126 11 |
| WARNB11A 26 1 126 00 CARGO SMOKE WARNING |
| 26 2 126 00 |
| WARNB121 26 1 126 11 SDAC 2 VALID SYS. 1 |
| 26 2 126 11 |
| WARNB12A 26 1 126 00 LAVATORY SMOKE WARNING |
| 26 2 126 00 |
| WARNB141 26 1 126 00 FLAPS FAULT SYS. 1 |
| 26 2 126 00 |
| WARNB151 26 1 126 00 YAW DAMPER1 FAULT SYS. 1 |
| 26 2 126 00 |
| WARNB161 26 1 126 00 YAW DAMPER2 FAULT SYS. 1 |
| 26 2 126 00 |
| WARNB171 26 1 126 00 ENG1 FIRE SYS. 1 |
| 26 2 126 00 |
| WARNB181 26 1 126 00 ENG2 FIRE SYS. 1 |
| 26 2 126 00 |
| WARNB191 26 1 126 00 APU FIRE SYS. 1 |
| 26 2 126 00 |
| WARNB20A 26 1 126 00 AVIONIC SMOKE WARNING |
| 26 2 126 00 |
| WARNB221 26 1 126 00 CABIN PRESS FAULT SYS. 1 |
| 26 2 126 00 |
| WARNB231 26 1 126 00 BLUE HYD LOW PRESSURE SYS. 1 |
| 26 2 126 00 |
| WARNB241 26 1 126 00 YELLOW HYD LOW PRESSURE SYS. 1 |
| 26 2 126 00 |
| WARNB251 26 1 126 00 GREEN HYD LOW PRESSURE SYS. 1 |
| 26 2 126 00 |
| WARNB261 26 1 126 00 VMO/MMO OVERSPEED SYS. 1 |
| 26 2 126 00 |
| WARNB291 26 1 126 00 SURF. NOT T.O. CONFIG |
| 26 2 126 00 |
| WBKG 7A 1 123 01 KG/SEC BLEED AIR FLOW |
| WD 04 1 316 01 DEG WIND DIRECTION - TRUE |
| 04 2 316 10 |
| WD1 04 1 316 01 DEG WIND DIRECTION - TRUE SYS. 1 |
| WD2 04 1 316 10 DEG WIND DIRECTION - TRUE SYS. 2 |
| WFQKG1 5A 1 257 10 KG FUEL QUANTITY - LH INNER CELL SYS. 2(KG) |
| WFQKG2 5A 1 261 10 KG FUEL QUANTITY - RH INNER CELL SYS. 2(KG) |
| WFQKG3 5A 1 260 10 KG FUEL QUANTITY - CENTER TANK(KG) |
| WFQKG4 5A 1 256 10 KG FUEL QUANTITY - LH OUTER CELL(KG) |
| WFQKG5 5A 1 262 10 KG FUEL QUANTITY - RH OUTER CELL(KG) |
| WFQTOTKG 5A 1 247 10 KG TOTAL FUEL QUANTITY (KG) |
| WS 04 1 315 01 KTS WIND SPEED |
| 04 2 315 10 |
| WS1 04 1 315 01 KTS WIND SPEED SYS. 1 |
| WS2 04 1 315 10 KTS WIND SPEED SYS. 2 |
| WSD1 26 1 14 01 WIND SHEAR DETECTION SYS.1 |
| WSD2 26 1 14 10 WIND SHEAR DETECTION SYS.2 |
| XBLV1 29 1 55 01 XFEED VALVE FULLY CLOSED SYS. 1 DAR ONLY |
| 29 2 55 01 |
| XBLV2 29 1 55 10 XFEED VALVE FULLY CLOSED SYS. 2 DAR ONLY |
| 29 2 55 10 |
| YAW 04 1 330 01 DEG/SEC BODY AXIS YAW RATE SYS. 1 |
| 04 2 330 10 |
| ZCB 5C 1 151 01 FT CABIN ALTITUDE |
| 5C 2 151 10 |
| ZCB1 5C 1 151 01 FT CABIN ALTITUDE SYS. 1 |
| ZCB2 5C 1 151 10 FT CABIN ALTITUDE SYS. 2 |
| ZCBS 29 1 151 11 FT CABIN ALTITUDE SDAC |
| 29 2 151 11 |
| ZDW1 5D 1 60 10 HEX ZONE LABEL 060 |
| ZDW1B112 5D 1 60 10 DUCT OVERHEAT (88 DEG C) WARN 1 SYS. 2 |
| ZDW1B122 5D 1 60 10 DUCT OVERHEAT (88 DEG C) WARN 2 SYS. 2 |
| ZDW1B132 5D 1 60 10 DUCT OVERHEAT (88 DEG C) WARN 3 SYS. 2 |
| ZDW1B202 5D 1 60 10 TRIM AIR PRESS REG VALVE SYS. 2 |
| ZDW1B212 5D 1 60 10 MAIN ZONE CONTROL INOP SYS. 2 |
| ZDW1B222 5D 1 60 10 ZONE SECONDARY CONTROL INOP SYS. 2 |
| ZDW1B292 5D 1 60 10 ACSC INSTALLED |
| ZFCG 29 1 124 01 % MAC ZERO FUEL CG |
| 29 2 124 01 |
| ZFW 29 1 167 01 KG ZERO FUEL WEIGHT |
| 29 2 167 01 |
| ZLD1 5C 1 163 01 FT LANDING ELEVATION SYS. 1 |
| ZLD2 5C 1 163 10 FT LANDING ELEVATION SYS. 2 |
NOTE: This Alpha Call-Up list is for IAE engines only.
| ------------------------------------------------------------------------------- |
| Alpha Source Eq/Sys/Lab SDI Unit Parameter Comment |
| Call Up /SDI |
| ------------------------------------------------------------------------------- |
| ACC EEC 1 07C.1.330.01 % HPT1 IAE ACC Feedback Sys. 1 |
| ACC EEC 2 07C.2.330.10 % HPT2 IAE ACC Feedback Sys. 2 |
| ACID ACID ACID Alpha Call Up |
| ACW1 HEX ACW1P1 ACW 1 Sys. 1 Print |
| ACW2 HEX ACW2P1 ACW 2 Sys. 1 Print |
| ACW3 HEX ACW3P1 Aileron Position Right |
| Sys. 1 |
| ACW4 HEX ACW4P1 ACW 4 Sys. 1 Print |
| ACYC CYCLES ACYC Start Cycles |
| ACYI APU 1 07A.1.133.01 CYCLES ACYI Start Cycles |
| ACYI APU 1 07A.1.136.01 CYCLES ACYI2 Start Cycles |
| ADIR1 ADIR1P/N 0ADIR1P1 ADIRU P/N For ACU P.1 |
| Sys.1 |
| ADIR1 ADIR1P/N 0ADIR1P2 ADIRU P/N For ACU P.2 |
| Sys.1 |
| ADIR1 ADIR1P/N 0ADIR1P3 ADIRU P/N For ACU P.3 |
| Sys.1 |
| ADIR2 ADIR2P/N 0ADIR2P1 ADIRU P/N For ACU P.1 |
| Sys.2 |
| ADIR2 ADIR2P/N 0ADIR2P2 ADIRU P/N For ACU P.2 |
| Sys.2 |
| ADIR2 ADIR2P/N 0ADIR2P3 ADIRU P/N For ACU P.3 |
| Sys.2 |
| ADIR3 ADIR3P/N 0ADIR3P1 ADIRU P/N For ACU P.1 |
| Sys.3 |
| ADIR3 ADIR3P/N 0ADIR3P2 ADIRU P/N For ACU P.2 |
| Sys.3 |
| ADIR3 ADIR3P/N 0ADIR3P3 ADIRU P/N For ACU P.3 |
| Sys.3 |
| AHRI APU 1 07A.1.132.01 HOURS AHRI Operating Hours |
| AHRI APU 1 07A.1.135.01 HOURS AHRI2 Operating Hours |
| (Label 132) |
| AHRS HOURS AHRS Operating Hours |
| AILL FCDC 1 06C.1.310.01 DEG AILL Aileron Position Left |
| Sys. 1 |
| AILL FCDC 2 06C.2.310.10 |
| AILR FCDC 1 06C.1.330.01 DEG AILR Aileron Position Right |
| Sys. 1 |
| AILR FCDC 2 06C.2.330.10 |
| ALT ADC 1 006.1.203.01 FT ALT Altitude(1013.25MB) |
| ALT ADC 2 006.2.203.10 |
| AOA ADC 1 006.1.241.01 DEG AOA1 Corrected Angle of |
| Attack Sys. 1 |
| AOA ADC 2 006.2.241.10 DEG AOA2 Corrected Angle of |
| Attack Sys. 2 |
| AP AP1 Auto Pilot Alpha Call Up |
| AP AP2 Auto Pilot Alpha Call Up |
| APU APU 1 07A.1.037.01 DISCRETE ADW1B111 APU Bleed Valve Open |
| ASN APU 1 07A.1.050.01 ASN APU Serial Numbers |
| Sys. 1 |
| BAF EEC 1 07C.1.335.01 % BAF1 IAE 2.5 Bleed Actuator |
| Feedback Sys. 1 |
| BAF EEC 2 07C.2.335.10 % BAF2 IAE 2.5 Bleed Actuator |
| Feedback Sys. 2 |
| CAS ADC 1 006.1.206.01 KTS CAS Computed Airspeed |
| CAS ADC 2 006.2.206.10 |
| CFPG G CFPG1 CFPG Sys. 1 |
| CFPG G CFPG2 CFPG Sys. 2 |
| CG FMC 1 002.1.077.00 %MAC CG Long Center Of Gravity |
| CG FMC 2 002.2.077.00 |
| CIVV FT/MIN CIVV1 CIVV Sys. 1 |
| CIVV FT/MIN CIVV2 CIVV Sys. 2 |
| COT PC/ 08E.1.123.11 DEG C COT1 Pack Compr. Outlet |
| ACSC1 Temperature Sys. 1 |
| COT PC/ 08E.2.123.00 DEG C COT2 Pack Compr. Outlet |
| ACSC2 Temperature Sys. 2 |
| CPC DISCRETE CPC System In Control |
| DATE MMMDD DATE Date Alpha Callup |
| DIV DIVRGNCE DIV Parameter Divergency |
| Alpha Call Up Report 09 |
| DT1A1 S/W P/N 0DT1A1P1 DT1 P/N For ACU P.1 |
| Sys. 1 |
| DT1A1 S/W P/N 0DT1A1P2 DT1 P/N For ACU P.2 |
| Sys. 1 |
| DT1A1 S/W P/N 0DT1A1P3 DT1 P/N For ACU P.3 |
| Sys. 1 |
| DT1A2 S/W P/N 0DT1A2P1 DT1 P/N For ACU P.1 |
| Sys. 2 |
| DT1A2 S/W P/N 0DT1A2P2 DT1 P/N For ACU P.2 |
| Sys. 2 |
| DT1A2 S/W P/N 0DT1A2P3 DT1 P/N For ACU P.3 |
| Sys. 2 |
| DT1A3 S/W P/N 0DT1A3P1 DT1 P/N For ACU P.1 |
| Sys. 3 |
| DT1A3 S/W P/N 0DT1A3P2 DT1 P/N For ACU P.2 |
| Sys. 3 |
| DT1A3 S/W P/N 0DT1A3P3 DT1 P/N For ACU P.3 |
| Sys. 3 |
| DT2A1 S/W P/N 0DT2A1P1 DT2 P/N For ACU P.1 |
| Sys. 1 |
| DT2A1 S/W P/N 0DT2A1P2 DT2 P/N For ACU P.2 |
| Sys. 1 |
| DT2A1 S/W P/N 0DT2A1P3 DT2 P/N For ACU P.3 |
| Sys. 1 |
| DT2A2 S/W P/N 0DT2A2P1 DT2 P/N For ACU P.1 |
| Sys. 2 |
| DT2A2 S/W P/N 0DT2A2P2 DT2 P/N For ACU P.2 |
| Sys. 2 |
| DT2A2 S/W P/N 0DT2A2P3 DT2 P/N For ACU P.3 |
| Sys. 2 |
| DT2A3 S/W P/N 0DT2A3P1 DT2 P/N For ACU P.1 |
| Sys. 3 |
| DT2A3 S/W P/N 0DT2A3P2 DT2 P/N For ACU P.2 |
| Sys. 3 |
| DT2A3 S/W P/N 0DT2A3P3 DT2 P/N For ACU P.3 |
| Sys. 3 |
| ECW1 HEX ECW1P1 Eng Control Word 1 Eng 1 |
| Sys.1 Print |
| ECW1 HEX ECW1P2 Eng Control Word 1 Eng 2 |
| Sys.2 Print |
| ECW2 HEX ECW2P1 Eng Control Word 2 Eng 1 |
| Sys.1 Print |
| ECW2 HEX ECW2P2 Eng Control Word 2 Eng 2 |
| Sys.2 Print |
| ECW3 HEX ECW3P1 Eng Control Word 3 Eng 1 |
| Sys.1 Print |
| ECW3 HEX ECW3P2 Eng Control Word 3 Eng 2 |
| Sys.2 Print |
| ECW4 HEX ECW4P1 Eng Control Word 4 Eng 1 |
| Sys.1 Print |
| ECW4 HEX ECW4P2 Eng Control Word 4 Eng 2 |
| Sys.2 Print |
| ECW5 HEX ECW5P1 Eng Control Word 5 Eng 1 |
| Sys.1 Print |
| ECW5 HEX ECW5P2 Eng Control Word 5 Eng 2 |
| Sys.2 Print |
| ECYC CYCLES ECYC1 Engine Cycles Engine 1 |
| System 1 |
| ECYC CYCLES ECYC2 Engine Cycles Engine 2 |
| System 1 |
| EGT ECU/ 07C.1.345.01 DEG C EGT1 EGT LPT Exit Temp Sys. 1 |
| EEC1 |
| EGT ECU/ 07C.2.345.10 DEG C EGT2 EGT LPT Exit Temp Sys. 2 |
| EEC2 |
| EGTA APU1 07A.1.175.01 DEG C EGTA EGT(APU) |
| EGTB EEC1 07C.1.321.01 EGTB1 Unbiased IAE EGT LPT |
| Exit Temp Sys. 1 |
| EGTB EEC2 07C.2.321.10 EGTB2 Unbiased IAE EGT LPT |
| Exit Temp Sys. 2 |
| EGTK DEG C EGTK1 Corrected EGT |
| EGTK DEG C EGTK2 Corrected EGT |
| EGTM DEG C EGTM1 Max IAE EGT LPT Exit |
| Temp Sys. 1 |
| EGTM DEG C EGTM2 Max IAE EGT LPT Exit |
| Temp Sys. 2 |
| EGTP DEG C EGTP1 IAE EGT LPT Exit Temp |
| Sys. 1 Print |
| EGTP DEG C EGTP2 IAE EGT LPT Exit Temp |
| Sys. 2 Print |
| EHRS HOURS EHRS1P1 Flight Hours Engine 1 |
| Sys. 1 Print |
| EHRS HOURS EHRS2P1 Flight Hours Engine 2 |
| Sys. 1 Print |
| ELA1 ELAC1P/N 0ELA1P1 ELAC P/N For ACU P.1 |
| Sys.1 |
| ELA1 ELAC1P/N 0ELA1P2 ELAC P/N For ACU P.2 |
| Sys.1 |
| ELA2 ELAC2P/N 0ELA2P1 ELAC P/N For ACU P.1 |
| Sys.2 |
| ELA2 ELAC2P/N 0ELA2P2 ELAC P/N For ACU P.2 |
| Sys.2 |
| ELEV FCDC1 06C.1.314.01 DEG ELEV1 Elevator Position Left |
| Sys. 1 |
| ELEV FCDC2 06C.2.314.10 |
| ELEV FCDC1 06C.1.334.01 DEG ELEV2 Elevator Position Right |
| Sys. 1 |
| ELEV FCDC2 06C.2.334.10 |
| EPR EEC1 07C.1.340.01 EPR1 IAE EPR Actual Sys. 1 |
| EPR EEC2 07C.2.340.10 EPR2 IAE EPR Actual Sys. 2 |
| EPRC EEC1 07C.1.341.01 EPRC1 IAE EPR Command Sys. 1 |
| EPRC EEC2 07C.2.341.10 EPRC2 IAE EPR Command Sys. 2 |
| EPRT EEC1 07C.1.342.01 EPRT1 IAE EPR Takeoff Sys. 1 |
| EPRT EEC2 07C.2.342.10 EPRT2 IAE EPR Takeoff Sys. 2 |
| ESN SERIAL# ESNL Left Engine Serial |
| Number Alpha |
| NOTE: If the ESN displayed on the MCDU is in the range between |
| 13191 and 15000, then add 5000 to this value to get the |
| actual ESN. |
| ESN SERIAL# ESNR Right Engine Serial |
| Number Alpha |
| EVM EVM1 03D.1.035.01 HEX EVMBALL1 Engine Vibration Status |
| Word Eng. 1 |
| EVM EVM1 03D.1.035.10 HEX EVMBALL2 Engine Vibration Status |
| Word Eng. 2 |
| EXSWPN Extended Software |
| Part number |
| FCV PC/ 08E.1.062.11 DISCRETE PSW1111 FLow Control Valve |
| ACSC1 Status Close Sys. 1 |
| FCV PC/ 08E.2.062.00 DISCRETE PSW1112 FLow Control Valve |
| ACSC2 Status Close Sys. 2 |
| FD KG/L FDINT1 Fuel Density Left Tank |
| Internal Parameter |
| FD KG/L FDINT2 Fuel Density Right Tank |
| Internal Parameter |
| FF ECU/ 07C.1.244.01 KGPH FFKG1 Fuel Mass FLow Rate |
| EEC1 Sys. 1 (KG) |
| FF ECU/ 07C.2.244.10 KGPH FFKG2 Fuel Mass FLow Rate |
| EEC2 Sys. 2 (KG) |
| FFK KG/P/HR FFK1 Corrected FF |
| FFK KG/P/HR FFK2 Corrected FF |
| FLAP DEG FLAPLC FLAP Actual Position |
| Sys. 1(Left) |
| FLAP DEG FLAPRC FLAP Actual Position |
| Sys. 1(Right) |
| FLT FLT NUM FLT Flight Number For Alpha |
| Callup |
| FRTO CITYPAIR FRTO FRTO Alpha Call Up |
| FT FQU 2 05A.2.177.10 DEG C FT1 Fuel Temperature LH |
| Inner Cell Sys. 2 |
| FT FQU 2 05A.2.201.10 DEG C FT2 Fuel Temperature RH |
| Inner Cell Sys. 2 |
| GLA SDAC1 029.1.100.00 GLA APU Gen Load Sys. 1 |
| GLA SDAC2 029.2.100.00 |
| GLE SDAC1 029.1.077.01 % GLE1 Gen 1 Load Sys. 1 |
| GLE SDAC1 029.1.077.10 % GLE2 Gen 1 Load Sys. 2 |
| GLE SDAC2 029.2.077.01 |
| GLE SDAC2 029.2.077.10 |
| GLS DMC 1 025.1.174.01 DDM GLS1 ILS1 Glideslope |
| Deviation Sys. 1 |
| GLS DMC 1 025.1.174.10 DDM GLS2 ILS1 Glideslope |
| Deviation Sys. 2 |
| GLS DMC2 025.2.174.01 |
| GLS DMC2 025.2.174.10 |
| GS IRS 1 004.1.312.01 KTS GS1 IAE Ground Speed Sys. 1 |
| GS IRS 2 004.2.312.10 KTS GS2 IAE Ground Speed Sys. 2 |
| GW FMC 1 002.1.075.00 KG GWKG Gross Weight(KGS.) |
| GW FMC 2 002.2.075.00 |
| HUD1 HUD1SWPN 0HUD1P1 HUD P/N For ACU P.1 |
| Sys.1 |
| HUD1 HUD1SWPN 0HUD1P2 HUD P/N For ACU P.2 |
| Sys.1 |
| HUD1 HUD1SWPN 0HUD1P3 HUD P/N For ACU P.1 |
| Sys.1 |
| HUD2 HUD2SWPN 0HUD2P1 HUD P/N For ACU P.1 |
| Sys.2 |
| HUD2 HUD2SWPN 0HUD2P2 HUD P/N For ACU P.2 |
| Sys.2 |
| IGV APU 1 07A.1.130.01 DEG IGV IGV Position |
| IVV IRS 1 004.1.365.01 FT/MIN IVV01 Inertial Vertical Speed |
| Sys. 1 |
| IVV IRS 2 004.2.365.10 FT/MIN IVV02 Inertial Vertical Speed |
| Sys. 2 |
| LATA SDAC 1 029.1.332.01 G LATA1 Lateral Acceleration |
| Sys. 1 |
| LATA SDAC 2 029.2.332.01 |
| LATP IRS 1 004.1.310.NA DEG QLATP Present Position |
| Latitude (Variable) |
| LATP IRS 1 004.2.310.NA |
| LCDT APU 1 07A.1.074.01 DEG C LCDT Bleed Air Temp |
| LCIT APU 1 07A.1.110.01 DEG C LCIT Load Compressor Inlet |
| Temperature |
| LOC DMC 1 025.1.173.01 DDM LOC1 ILS1 Localizer Deviation |
| Sys. 1 |
| LOC DMC 1 025.1.173.10 DDM LOC2 ILS1 Localizer Deviation |
| Sys. 2 |
| LOC DMC 2 025.2.173.01 |
| LOC DMC 2 025.2.173.10 |
| LONA SDAC 1 029.1.331.01 G LONA1 Longitudinal |
| Acceleration Sys. 1 |
| LONA SDAC 2 029.2.331.01 |
| LONP IRS 1 004.1.311.NA DEG QLONP Present Position |
| Longitude (Variable) |
| LONP IRS 2 004.2.311.NA |
| LP EEC 1 07C.1.271.01 DISCRETE SW2B171 Low ACC Solenoid- Close |
| Sys. 1 |
| LP EEC 2 07C.2.271.10 DISCRETE SW2B172 Low ACC Solenoid- Close |
| Sys. 2 |
| MN ADC 1 006.1.205.01 MACH MN Mach |
| MN ADC 2 006.2.205.10 |
| N1 EEC 1 07C.1.346.01 %RPM N11 N1 Actual (Low Rotor |
| Speed) Sys. 1 |
| N1 EEC 2 07C.2.346.10 %RPM N12 N1 Actual (Low Rotor |
| Speed) Sys. 2 |
| N1K %RPM N1K1 Corrected N1 |
| N1K %RPM N1K2 Corrected N1 |
| N2 ECU/ 07C.1.344.01 %RPM N21 N2 Actual (High Rotor |
| EEC1 Speed) Sys. 1 |
| N2 ECU/ 07C.2.344.10 %RPM N22 N2 Actual (High Rotor |
| EEC2 Speed) Sys. 2 |
| N2K %RPM N2K1 Corrected N2 |
| N2K %RPM N2K2 Corrected N2 |
| NA APU1 07A.1.176.01 %RPM NA RPM |
| NL DATA NL Number of Data Lines |
| In Report 19 |
| NPA %RPM NAEGTP1 NA At EGTP (RPM) |
| OF DISCRETE OF1 Oil And Fuel Filter |
| Clogged Alpha Call Up |
| OF DISCRETE OF2 Oil And Fuel Filter |
| Clogged Alpha Call Up |
| OIP FWC 1 026.1.317.01 PSI OIP1 Eng 1 Oil Pressure |
| OIP FWC 1 026.1.317.10 PSI OIP2 Eng 2 Oil Pressure |
| OIP FWC 2 026.2.317.01 |
| OIP FWC 2 026.2.317.10 |
| OIQ SDAC 1 029.1.073.11 QUART OIQ1 Eng 1 Oil Quantity Sys.1 |
| OIQ SDAC 1 029.1.073.00 QUART OIQ2 Eng 2 Oil Quantity Sys.1 |
| OIQ SDAC 2 029.2.073.11 |
| OIQ SDAC 2 029.2.073.00 |
| OIQH QT/HR OIQH1 Oil Consumption Prev.. |
| Flight Eng.1 |
| OIQH QT/HR OIQH2 Oil Consumption Prev.. |
| Flight Eng.2 |
| OIT FWC 1 026.1.316.01 DEG C OIT1 Eng 1 Oil Temperature |
| OIT FWC 1 026.1.316.10 DEG C OIT2 Eng 2 Oil Temperature |
| OIT FWC 2 026.2.316.01 |
| OIT FWC 2 026.2.316.10 |
| OPS1 S/W P/N 0OPS1P1 OPS P/N For ACU P.1 |
| Sys.1 |
| OPS1 S/W P/N 0OPS1P2 OPS P/N For ACU P.2 |
| Sys.1 |
| OPS1 S/W P/N 0OPS1P3 OPS P/N For ACU P.3 |
| Sys.1 |
| OPS2 S/W P/N 0OPS2P1 OPS P/N For ACU P.1 |
| Sys.2 |
| OPS2 S/W P/N 0OPS2P2 OPS P/N For ACU P.2 |
| Sys.2 |
| OPS2 S/W P/N 0OPS2P3 OPS P/N For ACU P.3 |
| Sys.2 |
| OPS3 S/W P/N 0OPS3P1 OPS P/N For ACU P.1 |
| Sys.3 |
| OPS3 S/W P/N 0OPS3P2 OPS P/N For ACU P.2 |
| Sys.3 |
| OPS3 S/W P/N 0OPS3P3 OPS P/N For ACU P.3 |
| Sys.3 |
| OTA APU 1 07A.1.247.01 DEG C OTA APU Oil Sump Temp |
| P125 EEC 1 07C.1.257.01 PSIA P1251 P12.5 (FAN Exit Pressure) |
| Sys. 1 |
| P125 EEC 2 07C.2.257.10 PSIA P1252 P12.5 (FAN Exit Pressure) |
| Sys. 2 |
| P2 EEC 1 07C.1.131.01 PSIA P21 P2 (FAN Inlet Pressure) |
| Sys. 1 |
| P2 EEC 2 07C.2.131.10 PSIA P22 P2 (FAN Inlet Pressure) |
| Sys. 2 |
| P25 ECU/ 07C.1.262.01 PSIA P251 P2.5 (LPC Exit Pressure) |
| EEC1 Sys. 1 |
| P25 ECU/ 07C.2.262.10 PSIA P252 P2.5 (LPC Exit Pressure) |
| EEC2 Sys. 2 |
| P2A APU 1 07A.1.112.01 BAR P2A Inlet Pressure |
| P3 ECU/ 07C.1.264.01 PSIA P31 PB Burner Pressure Sys.1 |
| EEC1 |
| P3 ECU/ 07C.2.264.10 PSIA P32 PB Burner Pressure Sys.2 |
| EEC2 |
| P49 EEC 1 07C.1.132.01 PSIA P491 LPT Exit Pressure Sys. 1 |
| P49 EEC 2 07C.2.132.10 PSIA P492 LPT Exit Pressure Sys. 2 |
| PBV PC/ 08E.1.112.11 % PBV1 Pack Bypass Valve |
| ACSC1 Position Sys. 1 |
| PBV PC/ 08E.2.112.00 % PBV2 Pack Bypass Valve |
| ACSC2 Position Sys. 2 |
| PD BMC 1 06F.1.142.01 PSI PDE2 Precooler Eng 2 Inlet |
| Press Sys. 1 |
| PD BMC 2 06F.2.142.10 |
| PD BMC 1 06F.1.143.01 PSI PDE1 Precooler Eng 1 Inlet |
| Press Sys. 1 |
| PD BMC 2 06F.2.143.10 |
| PDC PRESS 1 05C.1.144.01 PSI PDC Cabin Diff. Pressure |
| Sys. 1 |
| PDC PRESS 2 05C.2.144.10 |
| PF PC/ 08E.1.126.11 KG/SEC PFLKG Pack FLow Sys. 1 |
| ACSC1 |
| PF PC/ 08E.2.126.00 KG/SEC PFRKG Pack FLow Sys. 2 |
| ACSC2 |
| PFAD APU 1 07A.1.004.01 HEX PFAD Performance Adjustments |
| Sys. 1 |
| PH PHASE PHNUMPRT Flight Phase (DMU) |
| Sys. 1 (Print FORMAT) |
| PHA EVM 1 03D.1.226.01 DEG PHA1 N1 Phase Unbal BRG1 Or |
| TRF EN1 Sys. 1 |
| PHA EVM 1 03D.1.226.10 DEG PHA2 N1 Phase Unbal BRG1 Or |
| TRF EN2 Sys. 1 |
| PIPS1 PC/ 08E.1.361.11 PSIA PIPS1 PIPS For ACU |
| ACSC1 |
| PIPS2 PC/ 08E.2.361.00 PSIA PIPS2 PIPS For ACU |
| ACSC2 |
| PS DISCRETE PS1P Main Zone Control INOP |
| Sys. 2 Print |
| PS DISCRETE PS2P Main Zone Control INOP |
| Sys. 2 Print |
| PSB FWC 1 026.1.320.01 PSI PSB1 Eng 1 NO.4 Bearing |
| Pressure (IAE) |
| PSB FWC 1 026.1.320.10 PSI PSB2 Eng 2 NO.4 Bearing |
| Pressure (IAE) |
| PSB FWC 2 026.2.320.01 |
| PSB FWC 2 026.2.320.10 |
| PT APU 1 07A.1.166.01 BAR PT Bleed Air Pressure |
| PTCH IRS 1 004.1.324.01 DEG PTCH1 Pitch Angle Sys. 1 |
| PTCH IRS 2 004.2.324.10 |
| PTCR IRS 1 004.1.326.01 DEG/SEC QPTCR1 Body Axis Pitch Rate |
| (Load Report TRIG) |
| PTCR IRS 2 004.2.326.10 |
| QA QUAL # QA A/C Quality Number |
| Report Stability |
| QE QUAL # QE Eng Quality Number |
| Report Stability |
| RALR FT/SEC RALR0 Radio Altitude Rate |
| RALT DMC1 025.1.164.01 FT RALT1 Radio Height (R/A1) |
| Sys. 1 |
| RALT DMC1 025.1.164.10 FT RALT2 Radio Height (R/A1) |
| Sys. 2 |
| RALT DMC2 025.2.164.01 |
| RALT DMC2 025.2.164.10 |
| RI PC/ 08E.1.130.11 % RI1 Pack RAM Air Inlet |
| ACSC1 Position Sys. 1 |
| RI PC/ 08E.2.130.00 % RI2 Pack RAM Air Inlet |
| ACSC2 Position Sys. 2 |
| RO PC/ 08E.1.124.11 % RO1 Pack RAM Air Outlet Pos. |
| ACSC1 Sys. 1 |
| RO PC/ 08E.2.124.00 % RO2 Pack RAM Air Outlet Pos. |
| ACSC2 Sys. 2 |
| ROLL IRS 1 004.1.325.01 DEG ROLL Roll Angle Sys. 1 |
| ROLL IRS 2 004.2.325.10 |
| ROLR IRS 1 004.1.327.01 DEG/SEC QROLR1 Body Axis Roll Rate(Load |
| Report TRIG) |
| ROLR IRS 2 004.2.327.10 |
| RSP1 FCDC 1 06C.1.361.01 DEG RSP11 LH SPL 1 Position |
| RSP1 FCDC 2 06C.2.361.10 |
| RSP1 FCDC 1 06C.1.371.01 DEG RSP12 RH SPL 1 Position |
| RSP1 FCDC 2 06C.2.371.10 |
| RSP2 FCDC 1 06C.1.362.01 DEG RSP21 LH SPL 2 Position Sys. 1 |
| RSP2 FCDC 2 06C.2.362.10 |
| RSP2 FCDC 1 06C.1.372.01 DEG RSP22 RH SPL 2 Position Sys. 2 |
| RSP2 FCDC 2 06C.2.372.10 |
| RSP3 FCDC 1 06C.1.363.01 DEG RSP31 LH SPL 3 Position Sys. 1 |
| RSP3 FCDC 2 06C.2.363.10 |
| RSP3 FCDC 1 06C.1.373.01 DEG RSP32 RH SPL 3 Position Sys. 2 |
| RSP3 FCDC 2 06C.2.373.10 |
| RSP4 FCDC 1 06C.1.364.01 DEG RSP41 LH SPL 4 Position Sys. 1 |
| RSP4 FCDC 2 06C.2.364.10 |
| RSP4 FCDC 1 06C.1.374.01 DEG RSP42 RH SPL 4 Position Sys. 2 |
| RSP4 FCDC 2 06C.2.374.10 |
| RSP5 FCDC 1 06C.1.365.01 DEG RSP51 LH SPL 5 Position Sys. 1 |
| RSP5 FCDC 2 06C.2.365.10 |
| RSP5 FCDC 1 06C.1.375.01 DEG RSP52 RH SPL 5 Position Sys. 2 |
| RSP5 FCDC 2 06C.2.375.10 |
| RUDD SDAC 1 029.1.312.00 DEG RUDD Rudder Position Sys. 1 |
| RUDD SDAC 2 029.2.312.00 |
| RUDT FAC 1 00A.1.313.00 DEG RUDT Rudder Trim Sys. 1 |
| RUDT FAC 2 00A.2.313.00 |
| RV ZC/ 05D.2.060.10 DISCRETE ZDW1B202 Trim Air Press REG Valve |
| ACSC2 Sys. 2 |
| SAT ADC1 006.1.213.01 DEG C SAT Static Air Temperature |
| (BNR) |
| SAT ADC2 006.2.213.10 |
| SC1 SDAC 1 029.1.242.01 DEG C SC1C Selected Cockpit Compt |
| Temp Sys. 1 |
| SC1 SDAC 2 029.2.242.01 |
| SC2 SDAC 1 029.1.244.01 DEG C SC2C SEL FWD Cabine Compt |
| Temp Sys. 1 |
| SC2 SDAC 2 029.2.244.01 |
| SC3 SDAC 1 029.1.245.01 DEG C SC3C SEL AFT Cabine Compt |
| Temp Sys. 1 |
| SC3 SDAC 2 029.2.245.01 |
| SCC BSCU 1 06E.1.340.01 DEG NWSCO NWS Captain Order |
| SCC BSCU 2 06E.2.340.10 |
| SCFD BSCU 1 06E.1.341.01 DEG NWCFO NWS F/O Order |
| SCFD BSCU 2 06E.2.341.10 |
| SLAT DEG SLATLC Slat Actual Position |
| Sys. 1 |
| SLAT DEG SLATRC Slat Actual Position |
| Sys. 2 |
| SLP FAC 1 00A.1.226.00 DEG SLP1 Estimated Sideslip Sys.1 |
| SLP FAC 2 00A.2.226.00 DEG SLP2 Estimated Sideslip Sys.2 |
| SM EEC 1 07C.1.276.01 DISCRETE SW7B281 Autostart Mode Active |
| Sys. 1 |
| SM EEC 2 07C.2.276.10 DISCRETE SW7B282 Autostart Mode Active |
| Sys. 2 |
| STA SECONDS STA APU Start Time Sys. 1 |
| STAB FCDC 1 06C.1.315.01 DEG STAB Stabilizer Position #1 |
| Sys. 1 |
| STAB FCDC 2 06C.2.315.10 |
| SVA EEC 1 07C.1.325.01 % SVA1 SVA (Stator Vane |
| Actuator Feedback) Sys1 |
| SVA EEC 2 07C.2.325.10 % SVA2 SVA (Stator Vane |
| Actuator Feedback) Sys2 |
| T2 EEC 1 07C.1.130.01 DEG C T21 T2 (Inlet FAN Temp) |
| Sys. 1 |
| T2 EEC 2 07C.2.130.10 DEG C T22 T2 (Inlet FAN Temp) |
| Sys. 2 |
| T25 ECU/ 07C.1.263.01 DEG C T251 T2.5 (LPC Exit |
| EEC1 Temperature) Sys. 1 |
| T25 ECU/ 07C.2.263.10 DEG C T252 T2.5 (LPC Exit |
| EEC2 Temperature) Sys. 2 |
| T3 ECU/ 07C.1.265.01 DEG C T31 T3 (HPC Exit Temperature) |
| EEC1 Sys. 1 |
| T3 ECU/ 07C.2.265.10 DEG C T32 T3 (HPC Exit Temperature) |
| EEC2 Sys. 2 |
| TAT ADC 1 006.1.211.01 DEG C TAT Total Air Temperature |
| TAT ADC 2 006.2.211.10 |
| THDG IRS 1 004.1.044.01 DEG THDG1 True Heading 1 |
| THDG IRS 2 004.2.044.10 DEG THDG2 True Heading 2 |
| TLA ECU/ 07C.1.133.01 DEG TLA1 TLA (Throttle Resolver |
| EEC1 Angle) Sys. 1 |
| TLA ECU/ 07C.2.133.10 DEG TLA2 TLA (Throttle Resolver |
| EEC2 Angle) Sys. 2 |
| TN FWC 1 026.1.322.01 DEG C TN1 Eng 1 Nacelle |
| Temperature |
| TN FWC 1 026.1.322.10 DEG C TN2 Eng 2 Nacelle |
| Temperature |
| TN FWC 2 026.2.322.01 |
| TN FWC 2 026.2.322.10 |
| TP PC/ 08E.1.121.11 DEG C TP1 Pack Outlet Temperature |
| ACSC1 Sys. 1 |
| TP PC/ 08E.2.121.00 DEG C TP2 Pack Outlet Temperature |
| ACSC2 Sys. 2 |
| TPO BMC 1 06F.1.140.01 DEG C TPOE21 Precooler Eng 2 Outlet |
| Temp Sys. 1 |
| TPO BMC 2 06F.2.140.10 |
| TPO BMC 1 06F.1.141.01 DEG C TPOE11 Precooler Eng 1 Outlet |
| Temp Sys. 1 |
| TPO BMC 2 06F.2.141.10 |
| TRP EEC 1 07C.1.137.01 %DEPLOY TRP1 Thrust Reverser Position |
| Sys. 1 |
| TRP EEC 2 07C.2.137.10 %DEPLOY TRP2 Thrust Reverser Position |
| Sys. 2 |
| TW PC/ 08E.1.111.11 DEG C TW1 Pack Water Extr. |
| ACSC1 Temperature Sys. 1 |
| TW PC/ 08E.2.111.00 DEG C TW2 Pack Water Extr. |
| ACSC2 Temperature Sys. 2 |
| UTC HHMMSS UTC UTC For Alpha Callup |
| VA ZC/ 05D.2.220.10 % VA2 Cabin Temp REG VLV Pos |
| ACSC2 Group 3 Sys. 2 |
| VACC IRS 1 004.1.364.01 G VACC1 Vertical Acceleration |
| Sys. 1 |
| VACC IRS 2 004.2.364.10 G VACC2 Vertical Acceleration |
| Sys. 2 |
| VB1 EVM 1 03D.1.135.01 % VB11 N1 VIB Eng 1 BRG1 Or TRF |
| Sys. 1 |
| VB1 EVM 1 03D.1.135.10 % VB12 N1 VIB Eng 2 BRG1 Or TRF |
| Sys. 1 |
| VB2 EVM 1 03D.1.136.01 % VB21 N2 VIB Eng 1 BRG1 Or TRF |
| Sys. 1 |
| VB2 EVM 1 03D.1.136.10 % VB22 N2 VIB Eng 1 BRG1 Or TRF |
| Sys. 1 |
| VF ZC/ 05D.2.206.10 % VF2 CAB Temp REG VLV Pos |
| ACSC2 Group 1 Sys. 2 |
| VRTA SDAC 1 029.1.333.01 G VRTA1 Normal Acceleration |
| Sys. 1 |
| VRTA SDAC 2 029.2.333.01 |
| VW ZC/ 05D.2.207.10 % VW2 Cabin Temp REG VLV Pos |
| ACSC2 Group 2 Sys. 2 |
| WB APU 1 07A.1.123.01 KG/SEC WBKG Bleed Air FLOW |
| WD IRS 1 004.1.316.01 DEG WD1 Wind Direction - True |
| Sys. 1 |
| WD IRS 2 004.2.316.10 DEG WD2 Wind Direction - True |
| Sys. 2 |
| WFQ FQU 2 05A.2.257.10 KG WFQKG1 Fuel Quantity - LH Inner |
| Cell Sys. 2(KG) |
| WFQ FQU 2 05A.2.261.10 KG WFQKG2 Fuel Quantity - RH Inner |
| Cell Sys. 2(KG) |
| WS IRS 1 004.1.315.01 KTS WS1 Wind Speed Sys. 1 |
| WS IRS 2 004.2.315.10 KTS WS2 Wind Speed Sys. 2 |
| WS1 BSCU 1 06E.1.320.01 M/S Wheel 1 speed |
| WS1 BSCU 2 06E.2.320.10 M/S Wheel 1 speed |
| WS2 BSCU 1 06E.1.321.01 M/S Wheel 2 speed |
| WS2 BSCU 2 06E.2.321.10 M/S Wheel 2 speed |
| WS3 BSCU 1 06E.1.322.01 M/S Wheel 3 speed |
| WS3 BSCU 2 06E.2.322.10 M/S Wheel 3 speed |
| WS4 BSCU 1 06E.1.323.01 M/S Wheel 4 speed |
| WS4 BSCU 2 06E.2.323.10 M/S Wheel 4 speed |
| YAW IRS 1 004.1.330.01 DEG/SEC YAW Body Axis Yaw Rate Sys.1 |
| YAW IRS 2 004.2.330.10 |
| ZCB PRESS 1 05C.1.151.01 FT ZCB Cabin Altitude |
| ZCB PRESS 2 05C.2.151.10 |
| ZDW1 ZC/ 05D.2.060.10 HEX ZDW1 Zone Label 060 |
| ACSC2 |
| ZLD PRESS 1 05C.1.163.01 FT ZLD1 Landing Elevation Sys. 1 |
| ZLD PRESS 2 05C.2.163.10 FT ZLD2 Landing Elevation Sys. 2 |
NOTE: This Alpha Call-Up list is for CFM engines only.
| ------------------------------------------------------------------------------- |
| Alpha Source Eq/Sys/Lab SDI Unit Parameter Comment |
| Call Up /SDI |
| ------------------------------------------------------------------------------- |
| ACID ACID ACID Alpha Call Up |
| ACW1 HEX ACW1P1 ACW 1 Sys. 1 Print |
| ACW2 HEX ACW2P1 ACW 2 Sys. 1 Print |
| ACW3 HEX ACW3P1 Aileron Position Right |
| Sys. 1 |
| ACW4 HEX ACW4P1 ACW 4 Sys. 1 Print |
| ACYC CYCLES ACYC Start Cycles |
| ACYI APU 1 07A.1.133.01 CYCLES ACYI Start Cycles |
| ACYI APU 1 07A.1.136.01 CYCLES ACYI2 Start Cycles |
| ADIR1 ADIR1P/N 0ADIR1P1 ADIRU P/N For ACU P.1 |
| Sys.1 |
| ADIR1 ADIR1P/N 0ADIR1P2 ADIRU P/N For ACU P.2 |
| Sys.1 |
| ADIR1 ADIR1P/N 0ADIR1P3 ADIRU P/N For ACU P.3 |
| Sys.1 |
| ADIR2 ADIR2P/N 0ADIR2P1 ADIRU P/N For ACU P.1 |
| Sys.2 |
| ADIR2 ADIR2P/N 0ADIR2P2 ADIRU P/N For ACU P.2 |
| Sys.2 |
| ADIR2 ADIR2P/N 0ADIR2P3 ADIRU P/N For ACU P.3 |
| Sys.2 |
| ADIR3 ADIR3P/N 0ADIR3P1 ADIRU P/N For ACU P.1 |
| Sys.3 |
| ADIR3 ADIR3P/N 0ADIR3P2 ADIRU P/N For ACU P.2 |
| Sys.3 |
| ADIR3 ADIR3P/N 0ADIR3P3 ADIRU P/N For ACU P.3 |
| Sys.3 |
| AHRI APU 1 07A.1.132.01 HOURS AHRI Operating Hours |
| AHRI APU 1 07A.1.135.01 HOURS AHRI2 Operating Hours |
| (Label 132) |
| AHRS HOURS AHRS Operating Hours |
| AILL FCDC 1 06C.1.310.01 DEG AILL Aileron Position Left |
| Sys. 1 |
| AILL FCDC 2 06C.2.310.10 |
| AILR FCDC 1 06C.1.330.01 DEG AILR Aileron Position Right |
| Sys. 1 |
| AILR FCDC 2 06C.2.330.10 |
| ALT ADC 1 006.1.203.01 FT ALT Altitude(1013.25MB) |
| ALT ADC 2 006.2.203.10 |
| AOA ADC 1 006.1.241.01 DEG AOA1 Corrected Angle of |
| Attack Sys. 1 |
| AOA ADC 2 006.2.241.10 DEG AOA2 Corrected Angle of |
| Attack Sys. 2 |
| AP AP1 Auto Pilot Alpha Call |
| Up |
| AP AP2 Auto Pilot Alpha Call |
| Up |
| APU APU 1 07A.1.037.01 DISCRETE ADW1B111 APU Bleed Valve Open |
| ASN APU 1 07A.1.050.01 ASN APU Serial Numbers |
| Sys. 1 |
| BVP FWC 1 026.1.031.01 DISCRETE BVP1B261 Eng 1 Scavenge VLV |
| Open Sys. 1 |
| BVP FWC 1 026.1.031.10 DISCRETE BVP2B261 Eng 2 Scavenge VLV |
| Open Sys. 1 |
| BVP FWC 2 026.2.031.01 |
| BVP FWC 2 026.2.031.10 |
| CAS ADC 1 006.1.206.01 KTS CAS Computed Airspeed |
| CAS ADC 2 006.2.206.10 |
| CFPG G CFPG1 CFPG Sys. 1 |
| CFPG G CFPG2 CFPG Sys. 2 |
| CG FMC 1 002.1.077.00 %MAC CG Long Center of Gravity |
| CG FMC 2 002.2.077.00 |
| CIVV FT/MIN CIVV1 CIVV Sys. 1 |
| CIVV FT/MIN CIVV2 CIVV Sys. 2 |
| COT PC/ 08E.1.123.11 DEG C COT1 Pack Compr. Outlet |
| ACSC1 Temperature Sys. 1 |
| COT PC/ 08E.2.123.00 DEG C COT2 Pack Compr. Outlet |
| ACSC2 Temperature Sys. 2 |
| CPC DISCRETE CPC System In Control |
| DATE MMMDD DATE Date Alpha Callup |
| DIV DIVRGNCE DIV Parameter Divergency |
| Alpha Call Up Report |
| 09 |
| DT1A1 S/W P/N 0DT1A1P1 DT1 P/N For ACU P.1 |
| Sys. 1 |
| DT1A1 S/W P/N 0DT1A1P2 DT1 P/N For ACU P.2 |
| Sys. 1 |
| DT1A1 S/W P/N 0DT1A1P3 DT1 P/N For ACU P.3 |
| Sys. 1 |
| DT1A2 S/W P/N 0DT1A2P1 DT1 P/N For ACU P.1 |
| Sys. 2 |
| DT1A2 S/W P/N 0DT1A2P2 DT1 P/N For ACU P.2 |
| Sys. 2 |
| DT1A2 S/W P/N 0DT1A2P3 DT1 P/N For ACU P.3 |
| Sys. 2 |
| DT1A3 S/W P/N 0DT1A3P1 DT1 P/N For ACU P.1 |
| Sys. 3 |
| DT1A3 S/W P/N 0DT1A3P2 DT1 P/N For ACU P.2 |
| Sys. 3 |
| DT1A3 S/W P/N 0DT1A3P3 DT1 P/N For ACU P.3 |
| Sys. 3 |
| DT2A1 S/W P/N 0DT2A1P1 DT2 P/N For ACU P.1 |
| Sys. 1 |
| DT2A1 S/W P/N 0DT2A1P2 DT2 P/N For ACU P.2 |
| Sys. 1 |
| DT2A1 S/W P/N 0DT2A1P3 DT2 P/N For ACU P.3 |
| Sys. 1 |
| DT2A2 S/W P/N 0DT2A2P1 DT2 P/N For ACU P.1 |
| Sys. 2 |
| DT2A2 S/W P/N 0DT2A2P2 DT2 P/N For ACU P.2 |
| Sys. 2 |
| DT2A2 S/W P/N 0DT2A2P3 DT2 P/N For ACU P.3 |
| Sys. 2 |
| DT2A3 S/W P/N 0DT2A3P1 DT2 P/N For ACU P.1 |
| Sys. 3 |
| DT2A3 S/W P/N 0DT2A3P2 DT2 P/N For ACU P.2 |
| Sys. 3 |
| DT2A3 S/W P/N 0DT2A3P3 DT2 P/N For ACU P.3 |
| Sys. 3 |
| ECW1 HEX ECW1P1 Eng Control Word 1 Eng |
| 1 Sys.1 Print |
| ECW1 HEX ECW1P2 Eng Control Word 1 Eng |
| 2 Sys.2 Print |
| ECW2 HEX ECW2P1 Eng Control Word 2 Eng |
| 1 Sys.1 Print |
| ECW2 HEX ECW2P2 Eng Control Word 2 Eng |
| 2 Sys.2 Print |
| ECW5 HEX ECW5P1 Eng Control Word 5 Eng |
| 1 Sys.1 Print |
| ECW5 HEX ECW5P2 Eng Control Word 5 Eng |
| 2 Sys.2 Print |
| ECYC CYCLES ECYC1 Engine Cycles Engine |
| 1 System 1 |
| ECYC CYCLES ECYC2 Engine Cycles Engine |
| 2 System 1 |
| EGT ECU/ 07C.1.345.01 DEG C EGT1 EGT LPT Exit Temp |
| EEC1 Sys. 1 |
| EGT ECU/ 07C.2.345.10 DEG C EGT2 EGT LPT Exit Temp |
| EEC2 Sys. 2 |
| EGTA APU 1 07A.1.175.01 DEG C EGTA EGT(APU) |
| EGTK DEG C EGTK1 Corrected EGT |
| EGTK DEG C EGTK2 Corrected EGT |
| EGTM DEG C EGTM1 Max IAE EGT LPT Exit |
| Temp Sys. 1 |
| EGTM DEG C EGTM2 Max IAE EGT LPT Exit |
| Temp Sys. 2 |
| EGTP DEG C EGTP1 IAE EGT LPT Exit Temp |
| Sys. 1 Print |
| EGTP DEG C EGTP2 IAE EGT LPT Exit Temp |
| Sys. 2 Print |
| EHRS HOURS EHRS1P1 Flight Hours Engine 1 |
| Sys. 1 Print |
| EHRS HOURS EHRS2P1 Flight Hours Engine 2 |
| Sys. 1 Print |
| ELA1 ELAC1P/N 0ELA1P1 ELAC P/N For ACU P.1 |
| Sys.1 |
| ELA1 ELAC1P/N 0ELA1P2 ELAC P/N For ACU P.2 |
| Sys.1 |
| ELA2 ELAC2P/N 0ELA2P1 ELAC P/N For ACU P.1 |
| Sys.2 |
| ELA2 ELAC2P/N 0ELA2P2 ELAC P/N For ACU P.2 |
| Sys.2 |
| ELEV FCDC1 06C.1.314.01 DEG ELEV1 Elevator Position Left |
| Sys. 1 |
| ELEV FCDC2 06C.2.314.10 |
| ELEV FCDC1 06C.1.334.01 DEG ELEV2 Elevator Position |
| Right Sys. 1 |
| ELEV FCDC2 06C.2.334.10 |
| ERT ECU 1 07C.1.050.01 HOURS ERT1 Engine Running Time |
| ERT ECU 2 07C.2.050.10 HOURS ERT2 Engine Running Time |
| ESN SERIAL# ESNL Left Engine Serial |
| Number Alpha |
| ESN SERIAL# ESNR Right Engine Serial |
| Number Alpha |
| EVM EVM1 03D.1.035.01 HEX EVMBALL1 Engine Vibration |
| Status Word Eng. 1 |
| EVM EVM1 03D.1.035.10 HEX EVMBALL2 Engine Vibration |
| Status Word Eng. 2 |
| EXSWPN Extended Software |
| Partnumber |
| FCV PC/ 08E.1.062.11 DISCRETE PSW1111 FLow Control Valve |
| ACSC1 Status Close Sys. 1 |
| FCV PC/ 08E.2.062.00 DISCRETE PSW1112 FLow Control Valve |
| ACSC2 Status Close Sys. 2 |
| FD KG/L FDINT1 Fuel Density Left Tank |
| Internal Parameter |
| FD KG/L FDINT2 Fuel Density Right |
| Tank Internal Parameter |
| FF ECU/ 07C.1.244.01 KGPH FFKG1 Fuel Mass Flow Rate |
| EEC1 Sys. 1 (KG) |
| FF ECU/ 07C.2.244.10 KGPH FFKG2 Fuel Mass Flow Rate |
| EEC2 Sys. 2 (KG) |
| FFK KG/P/HR FFK1 Corrected FF |
| FFK KG/P/HR FFK2 Corrected FF |
| FLAP DEG FLAPLC FLAP Actual Position |
| Sys. 1(Left) |
| FLAP DEG FLAPRC FLAP Actual Position |
| Sys. 1(Right) |
| FLT FLT NUM FLT Flight Number For |
| Alpha Callup |
| FMV ECU 1 07C.1.347.01 % FMV1 Selected FMV Position |
| Sys. 1 |
| FMV ECU 2 07C.2.347.10 % FMV2 Selected FMV Position |
| Sys. 2 |
| FRTO CITYPAIR FRTO FRTO Alpha Call UP |
| FT FQU 2 05A.2.177.10 DEG C FT1 Fuel Temperature LH |
| Inner Cell Sys. 2 |
| FT FQU 2 05A.2.201.10 DEG C FT2 Fuel Temperature RH |
| Inner Cell Sys. 2 |
| GLA SDAC1 029.1.100.00 GLA APU Gen Load Sys. 1 |
| GLA SDAC2 029.2.100.00 |
| GLE SDAC1 029.1.077.01 % GLE1 Gen 1 Load Sys. 1 |
| GLE SDAC1 029.1.077.10 % GLE2 Gen 1 Load Sys. 2 |
| GLE SDAC2 029.2.077.01 |
| GLE SDAC2 029.2.077.10 |
| GLS DMC 1 025.1.174.01 DDM GLS1 ILS1 Glideslope |
| deviation Sys. 1 |
| GLS DMC 1 025.1.174.10 DDM GLS2 ILS1 Glideslope |
| deviation Sys. 2 |
| GLS DMC2 025.2.174.01 |
| GLS DMC2 025.2.174.10 |
| GS IRS 1 004.1.312.01 KTS GS1 IAE Ground Speed Sys.1 |
| GS IRS 2 004.2.312.10 KTS GS2 IAE Ground Speed Sys.2 |
| GW FMC 1 002.1.075.00 KG GWKG Gross Weight(KGS.) |
| GW FMC 2 002.2.075.00 |
| HPT ECU 1 07C.1.306.01 % HPT1 Selected HPTC Position |
| Sys. 1 |
| HPT ECU 2 07C.2.306.10 % HPT2 Selected HPTC Position |
| Sys. 2 |
| HUD1 HUD1SWPN 0HUD1P1 HUD P/N For ACU P.1 |
| Sys.1 |
| HUD1 HUD1SWPN 0HUD1P2 HUD P/N For ACU P.2 |
| Sys.1 |
| HUD1 HUD1SWPN 0HUD1P3 HUD P/N For ACU P.1 |
| Sys.1 |
| HUD2 HUD2SWPN 0HUD2P1 HUD P/N For ACU P.1 |
| Sys.2 |
| HUD2 HUD2SWPN 0HUD2P2 HUD P/N For ACU P.2 |
| Sys.2 |
| IGV APU 1 07A.1.130.01 DEG IGV IGV Position |
| IVV IRS 1 004.1.365.01 FT/MIN IVV01 Inertial Vertical |
| Speed Sys. 1 |
| IVV IRS 2 004.2.365.10 FT/MIN IVV02 Inertial Vertical |
| Speed Sys. 2 |
| LATA SDAC 1 029.1.332.01 G LATA1 Lateral Acceleration |
| Sys. 1 |
| LATA SDAC 2 029.2.332.01 |
| LATP IRS 1 004.1.310.NA DEG QLATP Present Position |
| Latitude (Variable) |
| LATP IRS 2 004.2.310.NA |
| LCDT APU 1 07A.1.074.01 DEG C LCDT Bleed Air Temp |
| LCIT APU 1 07A.1.110.01 DEG C LCIT Load Compressor Inlet |
| Temperature |
| LOC DMC 1 025.1.173.01 DDM LOC1 ILS1 Localizer |
| Deviation Sys. 1 |
| LOC DMC 1 025.1.173.10 DDM LOC2 ILS1 Localizer |
| Deviation Sys. 2 |
| LOC DMC 2 025.2.173.01 |
| LOC DMC 2 025.2.173.10 |
| LONA SDAC 1 029.1.331.01 G LONA1 Longitudinal |
| Acceleration Sys. 1 |
| LONA SDAC 2 029.2.331.01 |
| LONP IRS 1 004.1.311.NA DEG QLONP Present Position |
| Longitude (Variable) |
| LONP IRS 2 004.2.311.NA |
| LPT ECU 1 07C.1.307.01 % LPT1 Selected LPTC Position |
| Sys. 1 |
| LPT ECU 2 07C.2.307.10 % LPT2 Selected LPTC Position |
| Sys. 2 |
| MN ADC 1 006.1.205.01 MACH MN Mach |
| MN ADC 2 006.2.205.10 |
| N1 ECU 1 07C.1.346.01 %RPM N11 Selected N1 Sys. 1 |
| N1 ECU 2 07C.2.346.10 %RPM N12 Selected N1 Sys. 2 |
| N1C ECU 1 07C.1.341.01 %RPM N1C1 CFM N1 Command |
| Sys. 1 |
| N1C ECU 2 07C.2.341.10 %RPM N1C2 CFM N1 Command |
| Sys. 2 |
| N1K %RPM N1K1 Corrected N1 |
| N1K %RPM N1K2 Corrected N1 |
| N1MX ECU 1 07C.1.342.01 %RPM N1MX1 N1 Maximum Sys. 1 |
| N1MX ECU 2 07C.2.342.10 %RPM N1MX2 N1 Maximum Sys. 2 |
| N2 ECU/ 07C.1.344.01 %RPM N21 N2 Actual (High Rotor |
| EEC1 Speed) Sys. 1 |
| N2 ECU/ 07C.2.344.10 %RPM N22 N2 Actual (High Rotor |
| EEC2 Speed) Sys. 2 |
| N2K %RPM N2K1 Corrected N2 |
| N2K %RPM N2K2 Corrected N2 |
| NA APU 1 07A.1.176.01 %RPM NA RPM |
| NL DATA NL Number of Data Lines |
| In Report 19 |
| NPA %RPM NAEGTP1 NA At EGTP (RPM) |
| OF DISCRETE OF1 Oil And Fuel Filter |
| Clogged Alpha Call Up |
| OF DISCRETE OF2 Oil And Fuel Filter |
| Clogged Alpha Call Up |
| OIP FWC 1 026.1.317.01 PSI OIP1 Eng 1 Oil Pressure |
| OIP FWC 1 026.1.317.10 PSI OIP2 Eng 2 Oil Pressure |
| OIP FWC 2 026.2.317.01 |
| OIP FWC 2 026.2.317.10 |
| OIQ SDAC 1 029.1.073.11 QUART OIQ1 Eng 1 Oil Quantity |
| Sys. 1 |
| OIQ SDAC 1 029.1.073.00 QUART OIQ2 Eng 2 Oil Quantity |
| Sys. 1 |
| OIQ SDAC 2 029.2.073.11 |
| OIQ SDAC 2 029.2.073.00 |
| OIQH QT/HR OIQH1 Oil Consumption Prev.. |
| Flight Eng.1 |
| OIQH QT/HR OIQH2 Oil Consumption Prev.. |
| Flight Eng.2 |
| OIT FWC 1 026.1.316.01 DEG C OIT1 Eng 1 Oil Temperature |
| OIT FWC 1 026.1.316.10 DEG C OIT2 Eng 2 Oil Temperature |
| OIT FWC 2 026.2.316.01 |
| OIT FWC 2 026.2.316.10 |
| OPS1 S/W P/N 0OPS1P1 OPS P/N For ACU P.1 |
| Sys. 1 |
| OPS1 S/W P/N 0OPS1P2 OPS P/N For ACU P.2 |
| Sys. 1 |
| OPS1 S/W P/N 0OPS1P3 OPS P/N For ACU P.3 |
| Sys. 1 |
| OPS2 S/W P/N 0OPS2P1 OPS P/N For ACU P.1 |
| Sys.2 |
| OPS2 S/W P/N 0OPS2P2 OPS P/N For ACU P.2 |
| Sys.2 |
| OPS2 S/W P/N 0OPS2P3 OPS P/N For ACU P.3 |
| Sys.2 |
| OPS3 S/W P/N 0OPS3P1 OPS P/N For ACU P.1 |
| Sys.3 |
| OPS3 S/W P/N 0OPS3P2 OPS P/N For ACU P.2 |
| Sys.3 |
| OPS3 S/W P/N 0OPS3P3 OPS P/N For ACU P.3 |
| Sys.3 |
| OTA APU 1 07A.1.247.01 DEG C OTA APU Oil Sump Temp |
| P25 ECU/ 07C.1.262.01 PSIA P251 P2.5 (LPC Exit |
| EEC1 Pressure) Sys. 1 |
| P25 ECU/ 07C.2.262.10 PSIA P252 P2.5 (LPC Exit |
| EEC2 Pressure) Sys. 2 |
| P2A APU 1 07A.1.112.01 BAR P2A Inlet Pressure |
| P3 ECU/ 07C.1.264.01 PSIA P31 PB Burner Pressure |
| EEC1 Sys. 1 |
| P3 ECU/ 07C.2.264.10 PSIA P32 PB Burner Pressure |
| EEC2 Sys. 2 |
| PBV PC/ 08E.1.112.11 % PBV1 Pack Bypass Valve |
| ACSC1 Position Sys. 1 |
| PBV PC/ 08E.2.112.00 % PBV2 Pack Bypass Valve |
| ACSC2 Position Sys. 2 |
| PD BMC 1 06F.1.142.01 PSI PDE2 Precooler Eng 2 Inlet |
| Press Sys. 1 |
| PD BMC 2 06F.2.142.10 |
| PD BMC 1 06F.1.143.01 PSI PDE1 Precooler Eng 1 Inlet |
| Press Sys. 1 |
| PD BMC 2 06F.2.143.10 |
| PDC PRESS 1 05C.1.144.01 PSI PDC Cabin Diff. Pressure |
| Sys. 1 |
| PDC PRESS 2 05C.2.144.10 |
| PF PC/ 08E.1.126.11 KG/SEC PFLKG Pack FLow Sys. 1 |
| ACSC1 |
| PF PC/ 08E.2.126.00 KG/SEC PFRKG Pack FLow Sys. 2 |
| ACSC2 |
| PFAD APU 1 07A.1.004.01 HEX PFAD Performance |
| Adjustments Sys. 1 |
| PH PHASE PHNUMPRT Flight Phase (DMU) |
| Sys. 1 (Print FORMAT) |
| PHA EVM 1 03D.1.226.01 DEG PHA1 N1 Phase Unbal BRG1 Or |
| TRF EN1 Sys. 1 |
| PHA EVM 1 03D.1.226.10 DEG PHA2 N1 Phase Unbal BRG1 Or |
| TRF EN2 Sys. 1 |
| PHT EVM 1 03D.1.226.11 DEG PHT1 N1 Phase Unbal TRF EN1 |
| Sys. 1 |
| PHT EVM 1 03D.1.226.00 DEG PHT2 N1 Phase Unbal TRF EN2 |
| Sys. 1 |
| PO ECU 1 07C.1.114.01 PSIA PO1 Selected PO (Ambient |
| Pressure) Sys. 1 |
| PO ECU 2 07C.2.114.10 PSIA PO2 Selected PO (Ambient |
| Pressure) Sys. 2 |
| PS DISCRETE PS1P Main Zone Control INOP |
| Sys. 2 Print |
| PS DISCRETE PS2P Main Zone Control INOP |
| Sys. 2 Print |
| PS13 ECU 1 07C.1.127.01 PSIA PS131 PS13 Static Air |
| Pressure AT 1.3 Sys. 1 |
| PS13 ECU 2 07C.2.127.10 PSIA PS132 PS13 Static Air |
| Pressure AT 1.3 Sys. 2 |
| PSEL STATUS PSEL1 PSEL Alpha Call Up |
| PSEL STATUS PSEL2 PSEL Alpha Call Up |
| PT APU 1 07A.1.166.01 BAR PT Bleed Air Pressure |
| PT2 ECU 1 07C.1.131.01 PSIA PT21 PT2 (FAN Inlet |
| Pressure) Sys. 1 |
| PT2 ECU 2 07C.2.131.10 PSIA PT22 PT2 (FAN Inlet |
| Pressure) Sys. 2 |
| PTCH IRS 1 004.1.324.01 DEG PTCH1 Pitch Angle Sys. 1 |
| PTCH IRS 2 004.2.324.10 |
| PTCR IRS 1 004.1.326.01 DEG/SEC QPTCR1 Body Axis Pitch Rate |
| (Load Report TRIG) |
| PTCR IRS 2 004.2.326.10 |
| QA QUAL # QA A/C Quality Number |
| Report Stability |
| QE QUAL # QE Eng Quality Number |
| Report Stability |
| RALR FT/SEC RALR0 Radio Altitude Rate |
| RALT DMC1 025.1.164.01 FT RALT1 Radio Height (R/A1) |
| Sys. 1 |
| RALT DMC1 025.1.164.10 FT RALT2 Radio Height (R/A1) |
| Sys. 2 |
| RALT DMC2 025.2.164.01 |
| RALT DMC2 025.2.164.10 |
| RI PC/ 08E.1.130.11 % RI1 Pack RAM Air Inlet |
| ACSC1 Position Sys. 1 |
| RI PC/ 08E.2.130.00 % RI2 Pack RAM Air Inlet |
| ACSC2 Position Sys. 2 |
| RO PC/ 08E.1.124.11 % RO1 Pack RAM Air Outlet |
| ACSC1 Pos. Sys. 1 |
| RO PC/ 08E.2.124.00 % RO2 Pack RAM Air Outlet |
| ACSC2 Pos. Sys. 2 |
| ROLL IRS 1 004.1.325.01 DEG ROLL Roll Angle Sys. 1 |
| ROLL IRS 2 004.2.325.10 |
| ROLR IRS 1 004.1.327.01 DEG/SEC QROLR1 Body Axis Roll Rate |
| (Load Report TRIG) |
| ROLR IRS 2 004.2.327.10 |
| RSP1 FCDC 1 06C.1.361.01 DEG RSP11 LH SPL 1 Position |
| RSP1 FCDC 2 06C.2.361.10 |
| RSP1 FCDC 1 06C.1.371.01 DEG RSP12 RH SPL 1 Position |
| RSP1 FCDC 2 06C.2.371.10 |
| RSP2 FCDC 1 06C.1.362.01 DEG RSP21 LH SPL 2 Position |
| Sys. 1 |
| RSP2 FCDC 2 06C.1.362.10 |
| RSP2 FCDC 1 06C.1.372.01 DEG RSP22 RH SPL 2 Position |
| Sys. 2 |
| RSP2 FCDC 2 06C.2.372.10 |
| RSP3 FCDC 1 06C.1.363.01 DEG RSP31 LH SPL 3 Position |
| Sys. 1 |
| RSP3 FCDC 2 06C.1.363.10 |
| RSP3 FCDC 1 06C.1.373.01 DEG RSP32 RH SPL 3 Position |
| Sys. 2 |
| RSP3 FCDC 2 06C.1.373.10 |
| RSP4 FCDC 1 06C.1.364.01 DEG RSP41 LH SPL 4 Position |
| Sys. 1 |
| RSP4 FCDC 2 06C.2.364.10 |
| RSP4 FCDC 1 06C.1.374.01 DEG RSP42 RH SPL 4 Position |
| Sys. 2 |
| RSP4 FCDC 2 06C.2.374.10 |
| RSP5 FCDC 1 06C.1.365.01 DEG RSP51 LH SPL 5 Position |
| Sys. 1 |
| RSP5 FCDC 2 06C.2.365.10 |
| RSP5 FCDC 1 06C.1.375.01 DEG RSP52 RH SPL 5 Position |
| Sys. 2 |
| RSP5 FCDC 2 06C.2.375.10 |
| RUDD SDAC 1 029.1.312.00 DEG RUDD Rudder Position Sys. 1 |
| RUDD SDAC 2 029.2.312.00 |
| RUDT FAC 1 00A.1.313.00 DEG RUDT Rudder Trim Sys. 1 |
| RUDT FAC 2 00A.2.313.00 |
| RV ZC/ 05D.2.060.10 DISCRETE ZDW1B202 Trim Air Press REG |
| ACSC2 Valve Sys. 2 |
| SAT ADC1 006.1.213.01 DEG C SAT Static Air Temperature |
| (BNR) |
| SAT ADC2 006.2.213.10 |
| SC1 SDAC 1 029.1.242.01 DEG C SC1C Selected Cockpit Compt |
| Temp Sys. 1 |
| SC1 SDAC 2 029.2.242.01 |
| SC2 SDAC 1 029.1.244.01 DEG C SC2C SEL FWD Cabine Compt |
| Temp Sys. 1 |
| SC2 SDAC 2 029.2.244.01 |
| SC3 SDAC 1 029.1.245.01 DEG C SC3C SEL AFT Cabine Compt |
| Temp Sys. 1 |
| SC3 SDAC 2 029.2.245.01 |
| SCC BSCU 1 06E.1.340.01 DEG NWSCO NWS Captain Order |
| SCC BSCU 2 06E.2.340.10 |
| SCFD BSCU 1 06E.1.341.01 DEG NWCFO NWS F/O Order |
| SCFD BSCU 2 06E.2.341.10 |
| SLAT DEG SLATLC Slat Actual Position |
| Sys. 1 |
| SLAT DEG SLATRC Slat Actual Position |
| Sys. 2 |
| SLP FAC 1 00A.1.226.00 DEG SLP1 Estimated Sideslip |
| Sys. 1 |
| SLP FAC 2 00A.2.226.00 DEG SLP2 Estimated Sideslip |
| Sys. 2 |
| SSEL1 STATUS SSEL1A PSEL Alpha Call Up |
| SSEL1 STATUS SSEL1B PSEL Alpha Call Up |
| SSEL2 STATUS SSEL2A PSEL Alpha Call Up |
| SSEL2 STATUS SSEL2B PSEL Alpha Call Up |
| STA SECONDS STA APU Start Time |
| Sys. 1 Print |
| STAB FCDC 1 06C.1.315.01 DEG STAB Stabilizer Position |
| #1 Sys. 1 |
| STAB FCDC 2 06C.2.315.10 |
| T12 ECU 1 07C.1.130.01 DEG C T12A T12 (Inlet FAN Temp) |
| Sys. 1 |
| T12 ECU 2 07C.2.130.10 DEG C T12B T12 (Inlet FAN Temp) |
| Sys. 2 |
| T25 ECU/ 07C.1.263.01 DEG C T251 T2.5 (LPC Exit |
| EEC1 Temperature) Sys. 1 |
| T25 ECU/ 07C.2.263.10 DEG C T252 T2.5 (LPC Exit |
| EEC2 Temperature) Sys. 2 |
| T3 ECU/ 07C.1.265.01 DEG C T31 T3 (HPC Exit |
| EEC1 Temperature) Sys. 1 |
| T3 ECU/ 07C.2.265.10 DEG C T32 T3 (HPC Exit |
| EEC2 Temperature) Sys. 2 |
| T5 ECU 1 07C.1.260.01 DEG C T51 T5 Temperature At |
| Position 5 Sys. 1 |
| T5 ECU 2 07C.2.260.10 DEG C T52 T5 Temperature At |
| Position 5 Sys. 2 |
| TAT ADC 1 006.1.211.01 DEG C TAT Total Air Temperature |
| TAT ADC 2 006.2.211.10 |
| THDG IRS 1 004.1.044.01 DEG THDG1 True Heading 1 |
| THDG IRS 2 004.2.044.10 DEG THDG2 True Heading 2 |
| TLA ECU/ 07C.1.133.01 DEG TLA1 TLA (Throttle Resiolver |
| EEC1 Angle) Sys. 1 |
| TLA ECU/ 07C.2.133.10 DEG TLA2 TLA (Throttle Resiolver |
| EEC2 Angle) Sys. 2 |
| TN FWC 1 026.1.322.01 DEG C TN1 Eng 1 Nacelle |
| Temperature |
| TN FWC 1 026.1.322.10 DEG C TN2 Eng 2 Nacelle |
| Temperature |
| TN FWC 2 026.2.322.01 |
| TN FWC 2 026.2.322.10 |
| TP PC/ 08E.1.121.11 DEG C TP1 Pack Outlet |
| ACSC1 Temperature Sys. 1 |
| TP PC/ 08E.2.121.00 DEG C TP2 Pack Outlet |
| ACSC2 Temperature Sys. 2 |
| TPO BMC 1 06F.1.140.01 DEG C TPOE21 Precooler Eng 2 Outlet |
| Temp Sys. 1 |
| TPO BMC 2 06F.2.140.10 |
| TPO BMC 1 06F.1.141.01 DEG C TPOE11 Precooler Eng 1 Outlet |
| Temp Sys. 1 |
| TPO BMC 2 06F.2.141.10 |
| TR DISCRETE TR1 TR For Alpha Callup |
| TR DISCRETE TR2 TR For Alpha Callup |
| TW PC/ 08E.1.111.11 DEG C TW1 Pack Water Extr. |
| ACSC1 Temperature Sys. 1 |
| TW PC/ 08E.2.111.00 DEG C TW2 Pack Water Extr. |
| ACSC2 Temperature Sys. 2 |
| UTC HHMMSS UTC UTC For Alpha Callup |
| VA ZC/ 05D.2.220.10 % VA2 Cabine Temp REG VLV Pos |
| ACSC2 Group 3 Sys. 2 |
| VACC IRS 1 004.1.364.01 G VACC1 Vertical Acceleration |
| Sys. 1 |
| VACC IRS 2 004.2.364.10 G VACC2 Vertical Acceleration |
| Sys. 2 |
| VB1 EVM 1 03D.1.135.01 % VB11 N1 VIB Eng 1 BRG1 Or |
| TRF Sys. 1 |
| VB1 EVM 1 03D.1.135.10 % VB12 N1 VIB Eng 2 BRG1 Or |
| TRF Sys. 1 |
| VB2 EVM 1 03D.1.136.01 % VB21 N2 VIB Eng 1 BRG1 Or |
| TRF Sys. 1 |
| VB2 EVM 1 03D.1.136.10 % VB22 N2 VIB Eng 2 BRG1 Or |
| TRF Sys. 1 |
| VBV ECU 1 07C.1.071.01 DEG VBV1 Variable Bleed Valve |
| PSN Sys. 1 |
| VBV ECU 2 07C.2.071.10 DEG VBV2 Variable Bleed Valve |
| PSN Sys. 2 |
| VC EVM 1 03D.1.230.01 MILS VC1 FAN Pick Up N2 Track |
| Vibration Eng 1 |
| VC EVM 1 03D.1.230.10 MILS VC2 FAN Pick Up N2 Track |
| Vibration Eng 2 |
| VF ZC/ 05D.2.206.10 % VF2 CAB Temp REG VLV Pos |
| ACSC2 Group 1 Sys. 2 |
| VH EVM 1 03D.1.230.11 IPS VH1 TRF Pick Up N2 Track |
| Vibration Eng 1 |
| VH EVM 1 03D.1.230.00 IPS VH2 TRF Pick Up N2 Track |
| Vibration Eng 2 |
| VL EVM 1 03D.1.227.11 MILS VL1 TRF Pick Up N1 Track |
| Vibration Eng 1 |
| VL EVM 1 03D.1.227.00 MILS VL2 TRF Pick Up N1 Track |
| Vibration Eng 2 |
| VN EVM 1 03D.1.227.01 MILS VN1 FAN Pick Up N1 Track |
| Vibration Eng 1 |
| VN EVM 1 03D.1.227.10 MILS VN2 FAN Pick Up N1 Track |
| Vibration Eng 2 |
| VRTA SDAC 1 029.1.333.01 G VRTA1 Normal Acceleration |
| Sys. 1 |
| VRTA SDAC 2 029.2.333.01 |
| VSV ECU 1 07C.1.072.01 DEG VSV1 Selected Variable |
| Stator Vane PSN Sys. 1 |
| VSV ECU 2 07C.2.072.10 DEG VSV2 Selected Variable |
| Stator Vane PSN Sys. 2 |
| VW ZC/ 05D.2.207.10 % VW2 Cabine Temp REG VLV |
| ACSC2 Pos Group 2 Sys. 2 |
| WB APU 1 07A.1.123.01 KG/SEC WBKG Bleed Air FLOW |
| WD IRS 1 004.1.316.01 DEG WD1 Wind Driection - True |
| Sys. 1 |
| WD IRS 2 004.2.316.10 DEG WD2 Wind Driection - True |
| Sys. 2 |
| WFQ FQU 2 05A.2.257.10 KG WFQKG1 Fuel Quantity - LH |
| Inner Cell Sys. 2(KG) |
| WFQ FQU 2 05A.2.261.10 KG WFQKG2 Fuel Quantity - RH |
| Inner Cell Sys. 2(KG) |
| WS IRS 1 004.1.315.01 KTS WS1 Wind Speed Sys. 1 |
| WS IRS 2 004.2.315.10 KTS WS2 Wind Speed Sys. 2 |
| WS1 BSCU 1 06E.1.320.01 M/S Wheel 1 speed |
| WS1 BSCU 2 06E.2.320.10 M/S Wheel 1 speed |
| WS2 BSCU 1 06E.1.321.01 M/S Wheel 2 speed |
| WS2 BSCU 2 06E.2.321.10 M/S Wheel 2 speed |
| WS3 BSCU 1 06E.1.322.01 M/S Wheel 3 speed |
| WS3 BSCU 2 06E.2.322.10 M/S Wheel 3 speed |
| WS4 BSCU 1 06E.1.323.01 M/S Wheel 4 speed |
| WS4 BSCU 2 06E.2.323.10 M/S Wheel 4 speed |
| YAW IRS 1 004.1.330.01 DEG/SEC YAW Body Axis Yaw |
| Rate Sys. 1 |
| YAW IRS 2 004.2.330.10 |
| ZCB PRESS 1 05C.1.151.01 FT ZCB Cabin Altitude |
| ZCB PRESS 2 05C.2.151.10 |
| ZDW1 ZC/ 05D.2.060.10 HEX ZDW1 Zone Label 060 |
| ACSC2 |
NOTE: This Alpha Call-Up list is for CFM engines only.
| ------------------------------------------------------------------------------- |
| Alpha Source Eq/Sys/Lab Unit Parameter Comment |
| Call Up /SDI |
| ------------------------------------------------------------------------------- |
| ACTYP ACTYPE A/C TYPE (DMU computed) |
| ACW1 ACW1 APU control word #1 |
| (DMU computed) |
| ACW2 ACW2 APU control word #2 |
| (DMU computed) |
| ACW3 ACW3 APU control word #3 |
| (DMU computed) |
| ACW4 ACW4 APU control word #4 |
| (DMU computed) |
| ACYC CYCLES ACYC APU cycles (DMU |
| computed) |
| ACYI APU1 07A.1.133.01 CYCLES ACYI APU start cycles |
| ACYI APU1 07A.1.136.01 CYCLES ACYI APU start cycles |
| ADIR1 ADIR1_PN_P1 ADIRU hardware P/N (DMU |
| computed from ADC1 bus) |
| ADIR1 ADIR1_PN_P2 |
| ADIR1 ADIR1_PN_P3 |
| ADIR2 ADIR2_PN_P1 ADIRU hardware P/N (DMU |
| computed from ADC2 bus) |
| ADIR2 ADIR2_PN_P2 |
| ADIR2 ADIR2_PN_P3 |
| ADIR3 ADIR3_PN_P1 ADIRU hardware P/N (DMU |
| computed from ADC3 bus) |
| ADIR3 ADIR3_PN_P2 |
| ADIR3 ADIR3_PN_P3 |
| ADW1 APU1 07A.1.037.01 APUDSW1 APU:Discrete status |
| word #1 |
| AHRI APU1 07A.1.132.01 H AHRI APU operating hours |
| AHRI APU1 07A.1.135.01 H AHRI APU operating hours |
| AHRS H AHRS APU hours |
| (DMU computed) |
| AIL FCDC1 06C.1.310.01 DEG AIL_1 Aileron position left |
| AIL FCDC1 06C.1.330.01 DEG AIL_2 Aileron position right |
| AILL FCDC1 06C.1.310.01 DEG AIL_1 Aileron position left |
| AILL FCDC2 06C.2.310.10 DEG AIL_1 Aileron position left |
| AILR FCDC1 06C.1.330.01 DEG AIL_2 Aileron position right |
| AILR FCDC2 06C.2.330.10 DEG AIL_2 Aileron position right |
| ALT ADC1 006.1.203.01 FEET ALT Altitude (1013.25mb) |
| switched parameter |
| ALT ADC2 006.2.203.10 FEET ALT Altitude (1013.25mb) |
| switched parameter |
| ALT3 FWC1 026.1.203.11 FEET ALT3 Altitude 3 (1013.25 ha) |
| ALTR FGC1 001.1.365.00 FT/MIN ALTRATE Altitude rate (VZBI) |
| ALTR FGC2 001.2.365.00 FT/MIN ALTRATE Altitude rate (VZBI) |
| AMW1 APU1 07A.1.353.01 APUMW1 APU: Maintenance |
| word #1 |
| AMW2 APU1 07A.1.351.01 APUMW2 APU: Maintenance |
| word #2 |
| AMW3 APU1 07A.1.352.01 APUMW3 APU: Maintenance |
| word #3 |
| AOA ADC1 006.1.241.01 DEG AOA_1 Corrected angle of |
| attack system #1 |
| AOA ADC2 006.2.241.10 DEG AOA_2 Corrected angle of |
| attack system #2 |
| AOA3 FWC1 026.1.241.11 DEG AOA3 Corrected angle of |
| attack 3 |
| AP AP_1 Auto pilot status (AP) |
| left |
| AP AP_2 Auto pilot status (AP) |
| right |
| APLAT AP_LAT_1 A/P lateral mode left |
| APLAT AP_LAT_2 A/P lateral mode right |
| APLON AP_LON_1 A/P longitudinal mode |
| left |
| APLON AP_LON_2 A/P longitudinal mode |
| right |
| APU APU1 07A.1.037.01 APU_BLDV APU Bleed Valve - |
| _OPF Bit 11 |
| ASN APU1 07A.1.050.01 ASN APU serial number |
| BP1 BSCU1 06E.1.300.01 BAR BP1 Brake 1 pressure |
| BP1 BSCU2 06E.2.300.10 BAR BP1 Brake 1 pressure |
| BP2 BSCU1 06E.1.301.01 BAR BP2 Brake 2 pressure |
| BP2 BSCU2 06E.2.301.10 BAR BP2 Brake 2 pressure |
| BP3 BSCU1 06E.1.302.01 BAR BP3 Brake 3 pressure |
| BP3 BSCU2 06E.2.302.10 BAR BP3 Brake 3 pressure |
| BP4 BSCU1 06E.1.303.01 BAR BP4 Brake 4 pressure |
| BP4 BSCU2 06E.2.303.10 BAR BP4 Brake 4 pressure |
| BT1 BSCU1 06E.1.114.01 DEGC BT1 Brake 1 temperature |
| BT1 BSCU2 06E.2.114.10 DEGC BT1 Brake 1 temperature |
| BT2 BSCU1 06E.1.115.01 DEGC BT2 Brake 2 temperature |
| BT2 BSCU2 06E.2.115.10 DEGC BT2 Brake 2 temperature |
| BT3 BSCU1 06E.1.116.01 DEGC BT3 Brake 3 temperature |
| BT3 BSCU2 06E.2.116.10 DEGC BT3 Brake 3 temperature |
| BT4 BSCU1 06E.1.117.01 DEGC BT4 Brake 4 temperature |
| BT4 BSCU2 06E.2.117.10 DEGC BT4 Brake 4 temperature |
| BVP FWC1 026.1.031.01 BVP_OP_1 Scavenge valve open |
| engine #1 |
| BVP FWC1 026.1.031.10 BVP_OP_2 Scavenge valve open |
| engine #2 |
| CAS ADC 1 006.1.206.01 KTS CAS Computed air speed |
| (switched parameter) |
| CAS ADC 2 006.2.206.10 KTS CAS Computed air speed |
| (switched parameter) |
| CAS3 FWC1 026.1.206.11 KTS CAS3 Computed air speed 3 |
| CFPG D_CFPG_1 Calculated flight path |
| acceleration sys.#1 |
| (DMU computed) |
| CFPG D_CFPG_2 Calculated flight path |
| acceleration sys.#2 |
| (DMU computed) |
| CG FMC 1 002.1.077.00 %MAC CG Long Center of gravity |
| (switched parameter) |
| CG FMC 2 002.2.077.00 %MAC CG Long Center of gravity |
| (switched parameter) |
| CIVV D_CIVV_1 Calculated inertial |
| vertical speed system |
| #1 (DMU computed) |
| CIVV D_CIVV_2 Calculated inertial |
| vertical speed system |
| #2 (DMU computed) |
| CNT DMU RCOUNT Report count |
| CPC DISCRETE CPC System In Control |
| COT PC/ 08E.1.123.11 DEGC COT_1 Pack Compr. Outlet |
| ACSC1 Temperature LH |
| COT PC/ 08E.2.123.00 DEGC COT_2 Pack Compr. Outlet |
| ACSC2 Temperature RH |
| CSV1 BSCU1 06E.1.310.01 MA CSV1 Current SNV1 |
| CSV1 BSCU2 06E.2.310.10 MA CSV1 Current SNV1 |
| CSV2 BSCU1 06E.1.311.01 MA CSV2 Current SNV2 |
| CSV2 BSCU2 06E.2.311.10 MA CSV2 Current SNV2 |
| CSV3 BSCU1 06E.1.312.01 MA CSV3 Current SNV3 |
| CSV3 BSCU2 06E.2.312.10 MA CSV3 Current SNV3 |
| CSV4 BSCU1 06E.1.313.01 MA CSV4 Current SNV4 |
| CSV4 BSCU2 06E.2.313.10 MA CSV4 Current SNV4 |
| DA IRS1 004.1.321.01 DEG DRIFT Drift angle |
| DA IRS2 004.2.321.10 DEG DRIFT Drift angle |
| DATE FDIU1 017.1.260.00 DATE GMT Date |
| DISI1 DISIDMU_DSW1 DMU input discrete word |
| #1 |
| DMEF DMC1 025.1.035.01 MHZ DME1_FREQ DME 1 frequency |
| DMEF DMC1 025.1.035.10 MHZ DME2_FREQ DME 2 frequency |
| DSW1 BSCU1 06E.1.270.01 BSCUDSW1 BSCU discrete status |
| word #1 |
| DSW1 BSCU2 06E.2.270.10 BSCUDSW1 BSCU discrete status |
| word #1 |
| DSW2 BSCU1 06E.1.026.01 BSCUDSW2 BSCU discrete status |
| word #2 |
| DSW2 BSCU2 06E.2.026.10 BSCUDSW2 BSCU discrete status |
| word #2 |
| DSW3 BSCU1 06E.1.027.01 BSCUDSW3 BSCU discrete status |
| word #3 |
| DSW3 BSCU2 06E.2.027.10 BSCUDSW3 BSCU discrete status |
| word #3 |
| DT1A1 DT1A1_P1 Static source error |
| correction (DMU |
| computed from ADC1 bus) |
| DT1A1 DT1A1_P2 |
| DT1A1 DT1A1_P3 |
| DT1A2 DT1A2_P1 Static source error |
| correction (DMU |
| computed from ADC2 bus) |
| DT1A2 DT1A2_P2 |
| DT1A2 DT1A2_P3 |
| DT1A3 DT1A3_P1 Static source error |
| correction (DMU |
| computed from ADC3 bus) |
| DT1A3 DT1A3_P2 |
| DT1A3 DT1A3_P3 |
| DT2A1 DT2A1_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC1 bus) |
| DT2A1 DT2A1_P2 |
| DT2A1 DT2A1_P3 |
| DT2A2 DT2A2_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC2 bus) |
| DT2A2 DT2A2_P2 |
| DT2A2 DT2A2_P3 |
| DT2A3 DT2A3_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC3 bus) |
| DT2A3 DT2A3_P2 |
| DT2A3 DT2A3_P3 |
| ECW1 D_ECUCW1_1 CFM Engine #1 control |
| word #1 |
| ECW1 D_ECUCW1_2 CFM Engine #2 control |
| word #1 |
| ECW2 D_ECUCW2_1 CFM Engine #1 control |
| word #2 |
| ECW2 D_ECUCW2_2 CFM Engine #2 control |
| word #2 |
| ECW5 D_ECUCW5_1 CFM Engine #1 control |
| word #5 |
| ECW5 D_ECUCW5_2 CFM Engine #2 control |
| word #5 |
| ECYC ECYC_1 Engine #1 cycles (DMU |
| computed) |
| ECYC ECYC_2 Engine #2 cycles (DMU |
| computed) |
| EGT EEC/ECU1 07C.1.345.01 DEGC EGT_1 EGT LPT exit temp |
| engine #1 |
| EGT EEC/ECU2 07C.2.345.10 DEGC EGT_2 EGT LPT exit temp |
| engine #2 |
| EGTA APU1 07A.1.175.01 DEGC APU_EGT APU EGT |
| EGTF DEGC EGT_1_F EGT LPT exit temp |
| engine #1: Filtered |
| parameter |
| EGTF DEGC EGT_2_F EGT LPT exit temp |
| engine #2: Filtered |
| parameter |
| EGTK DMU EGTK_1 EGT corrected left (DMU |
| computed) |
| EGTK DMU EGTK_2 EGT corrected right |
| (DMU computed) |
| EGTP DEGC APU_EGT_PEAK APU EGT PEAK during APU |
| start |
| EGTR DEG DEGTREF_5 Delta egt reference |
| value in climb |
| EGTR DEG DEGTREF_6 Delta egt reference |
| value in cruise |
| EHRS DMU HOURS EHRS_1 Engine #1 hours (DMU |
| computed) |
| EHRS DMU HOURS EHRS_2 Engine #2 hours (DMU |
| computed) |
| ELA1 ELAC1_PN_P1 ELAC 1 software P/N |
| ELAC1_PN_P2 (DMU computed from |
| data transmitted of |
| FCDC bus) |
| ELA1 ELAC1_PN_P3 |
| ELA2 ELAC2_PN_P1 ELAC 2 software P/N |
| ELAC2_PN_P2 (DMU computed from |
| data transmitted of |
| FCDC bus) |
| ELA2 ELAC2_PN_P3 |
| ELEV FCDC1 06C.1.314.01 DEG ELEV_1 Elevator position left |
| ELEV FCDC1 06C.1.334.01 DEG ELEV_2 Elevator position right |
| ENGFA FDIU1 017.1.304.00 ENGFAMILY A/C type engine |
| ENTYP ENGTYPE Engine type (DMU |
| computed) |
| ERT ECU1 07C.1.050.01 H ERT_1 Engine #1 running time |
| ERT ECU2 07C.2.050.10 H ERT_2 Engine #2 running time |
| ESN ESN_1 Engine #1 serial number |
| (DMU computed) |
| ESN ESN_2 Engine #2 serial number |
| (DMU computed) |
| ESN1 EEC/ECU1 07C.1.047.01 ESN_MSD_1 Engine serial number |
| (First half) engine #1 |
| ESN1 EEC/ECU1 07C.1.046.01 ESN_LSD_1 Engine serial number |
| (Last half) engine #1 |
| ESN2 EEC/ECU2 07C.2.047.10 ESN_MSD_2 Engine serial number |
| (First half) engine #2 |
| ESN2 EEC/ECU2 07C.2.046.10 ESN_LSD_2 Engine serial number |
| (Last half) engine #2 |
| ESWPN DMU EXSWPN1 Extended Software Part |
| Number (EXSWPN) for |
| Vendor and Engine Type |
| ESWPN DMU EXSWPN2 Extended Software Part |
| Number (EXSWPN) for |
| System SW PN |
| ESWPN DMU EXSWPN3 Extended Software Part |
| Number (EXSWPN) for |
| Database version and |
| revision |
| EVM EVM1 03D.1.035.01 EVMDW1_1 EVM discrete word #1 |
| engine #1 |
| EVM EVM1 03D.1.035.10 EVMDW1_2 EVM discrete word #1 |
| engine #2 |
| F318 SFCC1 01B.1.137.01 DEG FLAP_1_A318 FLAP actual position |
| left for A318 A/C |
| F318 SFCC1 01B.1.137.10 DEG FLAP_1_A318 FLAP actual position |
| left for A318 A/C |
| F319 SFCC1 01B.1.137.01 DEG FLAP_1_A319 FLAP actual position |
| left for A319 A/C |
| F319 SFCC2 01B.2.137.10 DEG FLAP_2_A319 FLAP actual position |
| right for A319 A/C |
| F320 SFCC1 01B.1.137.01 DEG FLAP_1_A320 FLAP actual position |
| left for A320 A/C |
| F320 SFCC2 01B.2.137.10 DEG FLAP_2_A320 FLAP actual position |
| right A320 A/C |
| F321 SFCC1 01B.1.137.01 DEG FLAP_1_A321 FLAP actual position |
| left for A321 A/C |
| F321 SFCC2 01B.2.137.10 DEG FLAP_2_A321 FLAP actual position |
| right A321 A/C |
| FD FQIC 05A.2.272.10 Kg/l FD_L Fuel density left wing |
| tank (DMU computed) |
| FD FQIC 05A.2.272.10 Kg/l FD_R Fuel density right wing |
| tank (DMU computed) |
| FDC FD_C Fuel density center |
| wing tank |
| (DMU computed) |
| FDL FD_L Fuel density left wing |
| tank (DMU computed) |
| FDR FD_R Fuel density right wing |
| tank (DMU computed) |
| FDRAW FQU2 05A.2.272.10 FUEL_D Fuel density |
| FF EEC/ECU1 07C.1.244.01 PPH/KG FF_1 Fuel mass flow rate |
| engine #1 |
| FF EEC/ECU2 07C.2.244.10 PPH/KG FF_2 Fuel mass flow rate |
| engine #2 |
| FFK DMU PPH FFK_1 Fuel flow corrected |
| engine #1 |
| FFK DMU PPH FFK_2 Fuel flow corrected |
| engine #2 |
| FLAP SFCC1 01B.1.137.01 DEG FLAP_1 FLAP actual position |
| left |
| FLAP SFCC1 01B.2.137.10 DEG FLAP_2 FLAP actual position |
| right |
| FLAPW DEG FLAP FLAP actual position |
| switched |
| FLCNT FLCNT Flight counter (DMU |
| computed) |
| FLNUM FLINUM Flight number (DMU |
| computed) |
| FM FLIMOD_DISP Flight phase to display |
| (DMU computed) |
| FMB FLIMOD_BROAD Flight phase |
| broadcasted to ACARS |
| (DMU computed) |
| FMF FWC1 026.1.126.01 FM_FWC Flight phases |
| FMF FWC2 026.2.126.01 FM_FWC Flight phases |
| FMGD1 FGC1 001.1.274.00 FMGCDSW1 FMGC discrete status |
| word #1 |
| FMGD1 FGC2 001.2.274.00 FMGCDSW1 FMGC discrete status |
| word #1 |
| FMGD2 FGC1 001.1.275.00 FMGCDSW2 FMGC discrete status |
| word #2 |
| FMGD2 FGC2 001.2.275.00 FMGCDSW2 FMGC discrete status |
| word #2 |
| FMGD4 FGC1 001.1.146.00 FMGCDSW4 FMGC discrete status |
| word #4 |
| FMGD4 FGC2 001.2.146.00 FMGCDSW4 FMGC discrete status |
| word #4 |
| FMI FLIMOD_INT Internal flight phase |
| (DMU computed) |
| FMV ECU1 07C.1.347.01 FMV_1 Selected FMV position |
| engine #1 |
| FMV ECU2 07C.2.347.10 FMV_2 Selected FMV position |
| engine #2 |
| FPA IRS1 004.1.322.01 DEG FPA Flight path angle |
| FPA IRS2 004.2.322.10 DEG FPA Flight path angle |
| FPAC IRS1 004.1.323.01 G FPAC Flight path |
| acceleration |
| FPAC IRS2 004.2.323.10 G FPAC Flight path |
| acceleration |
| FPPU SFCC1 01B.1.137.01 DEG FLAP_RAW FLAP actual position |
| (switched parameter) |
| FPPU SFCC2 01B.2.137.10 DEG FLAP_RAW FLAP actual position |
| (switched parameter) |
| FROM ORIGIN Departure (DMU |
| computed) |
| FRTO FMGC1 001.1.040.DD FROM(11,12, Identification of |
| 13) CITY PAIR |
| FRTO FMGC2 001.2.040.DD FROM(21,22, Identification of |
| 23) CITY PAIR |
| FRTO FMGC1 001.1.041.DD FROM(14,15, Identification of |
| 16) CITY PAIR |
| FRTO FMGC2 001.2.041.DD FROM(24,25, Identification of |
| 26) CITY PAIR |
| FRTO FMGC1 001.1.042.DD FROM(17,18, Identification of |
| 19) CITY PAIR |
| FRTO FMGC2 001.2.042.DD FROM(27,28, Identification of |
| 29) CITY PAIR |
| FT FQIC 05A.2.177.10 DEGC FT_1 Fuel temperature engine |
| #1 |
| FT FQIC 05A.2.201.10 DEGC FT_2 Fuel temperature engine |
| #2 |
| GLA SDAC1 029.1.100.00 % GLA APU generator load |
| GLA SDAC2 029.2.100.00 % GLA APU generator load |
| GLE SDAC1 029.1.077.01 % GLE_1 Generator load engine |
| #1 |
| GLE SDAC2 029.2.077.01 % GLE_1 Generator load engine |
| #2 |
| GLE SDAC1 029.1.077.10 % GLE_2 Engine Generator Load |
| GLE SDAC2 029.2.077.10 % GLE_2 Engine Generator Load |
| GLS DMC1 025.1.174.01 DDM GLS1 ILS1 glideslope |
| deviation |
| GLS DMC1 025.1.174.10 DDM GLS2 ILS2 glideslope |
| deviation |
| GS IRS1 004.1.312.01 KTS GS Ground speed |
| GS IRS2 004.2.312.10 KTS GS Ground speed |
| GW FMC1 002.1.075.00 10Kg GW Actual Gross Weight |
| GW FMC2 002.2.075.00 10Kg GW Actual Gross Weight |
| GWFK FAC1 00A.1.074.00 KG GWFK Gross weight FAC (kg) |
| GWFK FAC2 00A.2.074.00 KG GWFK Gross weight FAC (kg) |
| GWFL FAC1 00A.1.074.00 LBS GWFL Gross weight FAC (lbs) |
| GWFL FAC2 00A.2.074.00 LBS GWFL Gross weight FAC (lbs) |
| HPT ECU1 07C.1.306.01 % HPT_1 Selected HPTC position |
| engine #1 |
| HPT ECU2 07C.2.306.10 % HPT_2 Selected HPTC position |
| engine #2 |
| HPTC ECU1 07C.1.063.01 % HPTC_1 HPTC demand #1 |
| HPTC ECU2 07C.2.063.10 % HPTC_2 HPTC demand #2 |
| HUD1 HUD1_PN_P1 HUDC1 Software P/N (DMU |
| computed from HUDC bus) |
| HUD1 HUD1_PN_P2 |
| HUD1 HUD1_PN_P3 |
| HUD2 HUD2_PN_P1 HUDC2 Software P/N (DMU |
| computed from HUDC bus) |
| HUD2 HUD2_PN_P2 |
| HUD2 HUD2_PN_P3 |
| IALT IRS1 004.1.361.NA FEET IALT Inertial altitude |
| IALT IRS2 004.2.361.NA FEET IALT Inertial altitude |
| IGV APU1 07A.1.130.01 DEG IGV APU IGV position |
| ILS DMC1 025.1.033.01 MHZ ILS1_FREQ ILS 1 frequency |
| ILS DMC1 025.1.033.10 MHZ ILS2_FREQ ILS 2 frequency |
| IVV IRS1 004.1.365.01 FT/MIN IVV Initial vertical speed |
| IVV IRS2 004.2.365.10 FT/MIN IVV Initial vertical speed |
| K K_R09 K value for divergence |
| (EGT or TN) computing |
| LATA SDAC1 029.1.332.01 G LATACC Lateral acceleration |
| LATA SDAC2 029.2.332.01 G LATACC Lateral acceleration |
| LATG IRS1 004.1.332.01 G LATG Body lateral |
| acceleration |
| LATG IRS2 004.2.332.10 G LATG Body lateral |
| acceleration |
| LATP IRS1 004.1.310.NA DEG LATP_1 Present position |
| latitude system 1 |
| LATP IRS2 004.2.310.NA DEG LATP_2 Present position |
| latitude system 2 |
| LCDT APU1 07A.1.074.01 DEGC LCDT APU Bleed air |
| temperature |
| LCIT APU1 07A.1.110.01 DEGC APU_LCIT APU Load compressor |
| inlet temperature |
| LGDW LGCIU1 06D.1.021.01 LGCIUDSW2 LGCIU discrete word #2 |
| LGDW LGCIU2 06D.2.021.10 LGCIUDSW2 LGCIU discrete word #2 |
| LOC DMC1 025.1.173.01 DDM LOC1 ILS1 localizer |
| deviation |
| LOC DMC1 025.1.173.10 DDM LOC2 ILS2 localizer |
| deviation |
| LONA SDAC1 029.1.331.01 G LONGACC Longitudinal |
| acceleration |
| LONA SDAC2 029.2.331.01 G LONGACC Longitudinal |
| acceleration |
| LONG IRS1 004.1.331.01 G LONG Body longitudinal |
| acceleration |
| LONG IRS2 004.2.331.10 G LONG Body longitudinal |
| acceleration |
| LONP IRS1 004.1.311.NA DEG LONG_1 Present position |
| longitude system 1 |
| LONP IRS2 004.2.311.NA DEG LONG_2 Present position |
| longitude system 2 |
| LOPP BSCU1 06E.1.331.01 DEG BRAKE_LPA Left brake pedal angle |
| LOPP BSCU2 06E.2.330.10 DEG BRAKE_LPA Left brake pedal |
| angle |
| LPT ECU1 07C.1.307.01 % LPT_1 Selected LPTC position |
| engine #1 |
| LPT ECU2 07C.2.307.10 % LPT_2 Selected LPTC position |
| engine #2 |
| MFDI FDIU1 017.1.350.00 FDIUMW FDIU maintenance word |
| MH IRS1 004.1.320.01 DEG MH Magnetic heading |
| MH IRS2 004.2.320.10 DEG MH Magnetic heading |
| MN ADC1 006.1.205.01 MACH MACH Mach (switched |
| parameter) |
| MN ADC2 006.2.205.10 MACH MACH Mach (switched |
| parameter) |
| MN3 FWC1 026.1.205.11 MACH MACH3 Mach 3 |
| MN3 FWC2 026.2.205.11 MACH MACH3 Mach 3 |
| MW1 EEC/ 07C.1.350.01 EECMW1_1 EEC/ECU Maintenance |
| ECU1 data word #1 engine #1 |
| MW1 EEC/ECU2 ECUMW1_1 |
| MW1 EEC/ 07C.2.350.10 EECMW1_2 EEC/ECU Maintenance |
| ECU1 data word #1 engine #2 |
| MW1 EEC/ECU2 ECUMW1_2 |
| MW2 EEC/ 07C.1.351.01 EECMW2_1 EEC/ECU Maintenance |
| ECU1 data word #2 engine #1 |
| MW2 EEC/ECU2 ECUMW2_1 |
| MW2 EEC/ 07C.2.351.10 EECMW2_2 EEC/ECU Maintenance |
| ECU1 data word #2 engine #2 |
| MW2 EEC/ECU2 ECUMW2_2 |
| MW3 EEC/ 07C.1.352.01 EECMW3_1 EEC/ECU Maintenance |
| ECU1 data word #3 engine #1 |
| MW3 EEC/ECU2 ECUMW3_1 |
| MW3 EEC/ 07C.2.352.10 EECMW3_2 EEC/ECU Maintenance |
| ECU1 data word #3 engine #2 |
| MW3 EEC/ECU2 ECUMW3_2 |
| MW4 EEC/ 07C.1.353.01 EECMW4_1 EEC/ECU Maintenance |
| ECU1 data word #4 engine #1 |
| MW4 EEC/ECU2 ECUMW4_1 |
| MW4 EEC/ 07C.2.353.10 EECMW4_2 EEC/ECU Maintenance |
| ECU1 data word #4 engine #2 |
| MW4 EEC/ECU2 ECUMW4_2 |
| MW5 EEC/ 07C.1.354.01 EECMW5_1 EEC/ECU Maintenance |
| ECU1 data word #5 engine #1 |
| MW5 EEC/ECU2 ECUMW5_2 |
| MW5 EEC/ 07C.2.354.10 EECMW5_2 EEC/ECU Maintenance |
| ECU1 data word #5 engine #2 |
| MW5 EEC/ECU2 ECUMW5_2 |
| N1 EEC/ 07C.1.331.01 %RPM N1U_1 Selected Unbiased N1 |
| ECU1 engine #1 |
| N1 EEC/ 07C.2.331.10 %RPM N1U_2 Selected Unbiased N1 |
| ECU2 engine #2 |
| N1C ECU1 07C.1.341.01 %RPM N1C_1 N1 command engine #1 |
| N1C ECU2 07C.2.341.10 %RPM N1C_2 N1 command engine #2 |
| N1K DMU N1K_1 N1 corrected left |
| (DMU computed) |
| N1K DMU N1K_2 N1 corrected right |
| (DMU computed) |
| N1L EEC/ 07C.1.337.01 %RPM N1L_1 N1 limit engine #1 |
| ECU1 |
| N1L EEC/ 07C.2.337.10 %RPM N1L_2 N1 limit engine #2 |
| ECU2 |
| N1MX ECU1 07C.1.342.01 %RPM N1MX_1 N1 maximum engine #1 |
| N1MX ECU2 07C.2.342.10 %RPM N1MX_2 N1 maximum engine #2 |
| N1R %RPM N1_1_RATE N1 left rate |
| N1R %RPM N1_2_RATE N1 right rate |
| N2 EEC/ 07C.1.344.01 %RPM N2_1 N2 Actual (high rotor |
| ECU1 speed) engine #1 |
| (Fmt:5.1) |
| N2 EEC/ 07C.2.344.10 %RPM N2_2 N2 Actual (high rotor |
| ECU2 speed) engine #2 |
| (Fmt:5.1) |
| N2F %RPM N2_1_F N2 Actual (high rotor |
| speed) engine #1: |
| Filtered parameter |
| N2F %RPM N2_2_F N2 Actual (high rotor |
| speed) engine #2: |
| Filtered parameter |
| N2K N2K_1 N2 corrected left (DMU |
| computed) |
| N2K N2K_2 N2 corrected right (DMU |
| computed) |
| NA APU1 07A.1.176.01 %RPM APU_RPM APU RPM |
| NAI ZC/ NAI_OP_1 Nacelle anti-ice engine |
| ACSC2 05D.2.061.10 #1 open |
| NAI ZC/ NAI_OP_2 Nacelle anti-ice engine |
| ACSC2 05D.2.061.10 #2 open |
| NPA %RPM APU_RPM_PEAK APU RPM at APU EGT peak |
| during APU start |
| NRA BSCU1 06E.1.334.01 DEG NWSANG NWS angle |
| NRA BSCU2 06E.2.334.10 DEG NWSANG NWS angle |
| NSVC BSCU1 06E.1.335.01 MA NSVC Current servo valve NWS |
| NSVC BSCU2 06E.2.335.10 MA NSVC Current servo valve NWS |
| NWSA BSCU1 06E.1.334.01 DEG NWSANG NWS angle |
| NWSA BSCU2 06E.2.334.10 DEG NWSANG NWS angle |
| OIP FWC1 026.1.317.01 PSI OIP_1 OIL pressure engine #1 |
| OIP FWC1 026.1.317.10 PSI OIP_2 OIL pressure engine #2 |
| OIQ FWC1 026.1.073.01 QUART OIQ_1 OIL quantity engine #1 |
| OIQ FWC1 026.1.073.10 QUART OIQ_2 OIL quantity engine #2 |
| OIQH OIQH_1 OIL consumption from |
| the previous flight |
| engine #1 |
| OIQH OIQH_2 OIL consumption from |
| the previous flight |
| engine #2 |
| OIT FWC1 026.1.316.01 DEGC OIT_1 OIL temperature engine |
| #1 |
| OIT FWC2 026.2.316.01 DEGC OIT_1 OIL temperature engine |
| #1 |
| OIT FWC1 026.1.316.10 DEGC OIT_2 OIL temperature engine |
| #2 |
| OIT FWC2 026.2.316.10 DEGC OIT_2 OIL temperature engine |
| #2 |
| OPS1 OPS1_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC1 bus) |
| OPS1 OPS1_SN_P2 |
| OPS1 OPS1_SN_P3 |
| OPS2 OPS2_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC2 bus) |
| OPS2 OPS2_SN_P2 |
| OPS2 OPS2_SN_P3 |
| OPS3 OPS3_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC3 bus) |
| OPS3 OPS3_SN_P2 |
| OPS3 OPS3_SN_P3 |
| OTA APU1 07A.1.247.01 DEGC OTA APU OIL sum temperature |
| OVP PRESS1 05C.1.153.01 % OVP1 Outflow valve position |
| OVP PRESS2 05C.2.153.10 % OVP2 Outflow valve position |
| P2 EEC/ 07C.1.131.01 PSIA P2_1 P2 (FAN inlet pressure) |
| ECU1 engine #1 |
| P2 EEC/ 07C.2.131.10 PSIA P2_2 P2 (FAN inlet pressure) |
| ECU2 engine #2 |
| P25 EEC/ 07C.1.262.01 PSIA P25_1 P2.5(Low Pres Comp exit |
| ECU1 pressure) engine #1 |
| (alternative parameter) |
| P25 EEC/ 07C.2.262.10 PSIA P25_2 P2.5(Low Pres Comp exit |
| ECU2 pressure) engine #2 |
| (alternative parameter) |
| P3 EEC/ 07C.1.264.01 PSIA PB_1 Pb burner pressure |
| ECU1 engine #1 |
| P3 EEC/ 07C.2.264.10 PSIA PB_2 Pb burner pressure |
| ECU2 engine #2 |
| PB EEC/ 07C.1.264.01 PSIA PB_1 Pb burner pressure |
| ECU1 engine #1 |
| PB EEC/ 07C.2.264.10 PSIA PB_2 Pb burner pressure |
| ECU2 engine #2 |
| PBV PC/ 08E.1.112.11 % PBV_1 Pack bypass valve |
| ACSC1 position system #1 |
| PBV PC/ 08E.2.112.00 % PBV_2 Pack bypass valve |
| ACSC2 position system #2 |
| PCSW PRESS1 05C.1.057.01 PCSW Press control bus: |
| Status + Fault info |
| PCSW PRESS2 05C.2.057.10 PCSW Press control bus: |
| Status + Fault info |
| PD BMC1 06F.1.143.01 PSI PD_1 Precooler inlet |
| pressure |
| PD BMC2 06F.2.143.10 PSI PD_1 Precooler inlet |
| pressure |
| PD BMC1 06F.1.142.01 PSI PD_2 Precooler inlet |
| pressure |
| PD BMC2 06F.2.142.10 PSI PD_2 Precooler inlet |
| pressure |
| PDC PRESS1 05C.1.144.01 PSI PDC Cabin differential |
| pressure |
| PDC PRESS2 05C.2.144.10 PSI PDC Cabin differential |
| pressure |
| PF PC/ 08E.1.126.11 KG/S PF_1 Pack flow system #1 |
| ACSC1 |
| PF PC/ 08E.2.126.00 KG/S PF_2 Pack flow system #2 |
| ACSC2 |
| PFAD APU1 07A.1.004.01 PFAD APU: Performance |
| adjustments |
| PH FDIMU FLIMOD_DISP Flight phase to display |
| (DMU computed) |
| PHA EVM1 03D.1.226.01 DEG PHA_1 N1 phase unbalance brg1 |
| engine #1 |
| PHA EVM1 03D.1.226.10 DEG PHA_2 N1 phase unbalance brg1 |
| engine #2 |
| PHA EIU1 07B.1.224.XX DEG PHA.1 FAN pick up phase angle |
| PHA EIU2 07B.2.224.XX DEG PHA.2 FAN pick up phase angle |
| PHT EVM1 03D.1.226.11 DEG PHT_1 N1 phase unbalance TRF |
| engine #1 |
| PHT EVM1 03D.1.226.00 DEG PHT_2 N1 phase unbalance TRF |
| engine #2 |
| PS13 ECU1 07C.1.127.01 PSIA PS13_1 PS13 (FAN exit |
| pressure) engine #1 |
| PS13 ECU2 07C.2.127.10 PSIA PS13_2 PS13 (FAN exit |
| pressure) engine #2 |
| PSB FWC1 026.1.320.01 PSIA PSB_1 No. 4 bearing |
| pressure engine #1 |
| PSB FWC1 026.1.320.10 PSIA PSB_2 No. 4 bearing pressure |
| engine #2 |
| PSEL PSEL_1 Status of different |
| FADEC sensor eng1 |
| PSEL PSEL_2 Status of different |
| FADEC sensor eng2 |
| PSW1 PC/ 08E.1.062.11 PC062DW_1 Discrete data word |
| ACSC1 (Label 062) of pack |
| control bus system #1 |
| PSW1 PC/ 08E.2.062.00 PC062DW_2 Discrete data word |
| ACSC2 (Label 062) of pack |
| control bus system #2 |
| PT APU1 07A.1.166.01 BAR PT Bleed air pressure |
| PT2 ECU1 07C.1.131.01 PSIA P2_1 PT2 (FAN inlet |
| pressure) engine #1 |
| PT2 ECU2 07C.2.131.10 PSIA P2_2 PT2 (FAN inlet |
| pressure) engine #2 |
| PTCH IRS1 004.1.324.01 DEG PITCH Pitch angle |
| PTCH IRS2 004.2.324.10 DEG PITCH Pitch angle |
| PTCR IRS1 004.1.326.01 DEG/S PTCR Body axis pitch rate |
| PTCR IRS2 004.2.326.10 DEG/S PTCR Body axis pitch rate |
| RAC ECU1 07C.1.055.01 % RAC_1 Rotor active clearance |
| control position engine |
| #1 |
| RAC ECU2 07C.2.055.10 % RAC_2 Rotor active clearance |
| control position engine |
| #2 |
| RALR RALR_R15 Radio altitude rate |
| RALT DMC1 025.1.164.01 FEET RALT1 Radio Altitude |
| RALT DMC1 025.1.164.10 FEET RALT1 Radio Altitude |
| RALT DMC2 025.2.164.01 FEET RALT2 Radio Altitude |
| RALT DMC2 025.2.164.10 FEET RALT2 Radio Altitude |
| RI PC/ 08E.1.130.11 % RI_1 Pack ram inlet position |
| ACSC1 LH |
| RI PC/ 08E.2.130.00 % RI_2 Pack ram inlet position |
| ACSC2 RH |
| RO PC/ 08E.1.124.11 % RO_1 Pack ram outlet |
| ACSC1 position LH |
| RO PC/ 08E.2.124.00 % RO_2 Pack ram outlet |
| ACSC2 position RH |
| ROLL IRS1 004.1.325.01 DEG ROLL.1 ROLL angle |
| ROLL IRS2 004.2.325.10 DEG ROLL.1 ROLL angle |
| ROLR IRS1 004.1.327.01 DEG/S ROLR Body axis roll rate |
| ROLR IRS2 004.2.327.10 DEG/S ROLR Body axis roll rate |
| ROPP BSCU1 06E.1.330.01 DEG BRAKE_RPA Right brake pedal angle |
| ROPP BSCU2 06E.2.330.10 DEG BRAKE_RPA Right brake pedal angle |
| RSCC BSCU1 06E.1.332.01 KTS REFSPDCC Reference speed command |
| channel |
| RSCC BSCU2 06E.2.332.10 KTS REFSPDCC Reference speed command |
| channel |
| RSP2 FCDC1 06C.1.362.01 DEG RSP2_1 LH spoiler #2 position |
| RSP2 FCDC2 06C.2.362.10 DEG RSP2_1 LH spoiler #2 position |
| RSP2 FCDC1 06C.1.372.01 DEG RSP2_2 RH spoiler #2 position |
| RSP2 FCDC2 06C.2.372.10 DEG RSP2_2 RH spoiler #2 position |
| RSP3 FCDC1 06C.1.363.01 DEG RSP3_1 LH spoiler #3 position |
| RSP3 FCDC2 06C.2.363.10 DEG RSP3_1 LH spoiler #3 position |
| RSP3 FCDC1 06C.1.373.01 DEG RSP3_2 RH spoiler #3 position |
| RSP3 FCDC2 06C.2.373.10 DEG RSP3_2 RH spoiler #3 position |
| RSP4 FCDC1 06C.1.364.01 DEG RSP4_1 LH spoiler #4 position |
| RSP4 FCDC1 06C.2.364.10 DEG RSP4_1 LH spoiler #4 position |
| RSP4 FCDC1 06C.1.374.01 DEG RSP4_2 RH spoiler #4 position |
| RSP4 FCDC2 06C.2.374.10 DEG RSP4_2 RH spoiler #4 position |
| RSP5 FCDC1 06C.1.365.01 DEG RSP5_1 LH spoiler #5 position |
| RSP5 FCDC2 06C.2.365.10 DEG RSP5_1 LH spoiler #5 position |
| RSP5 FCDC1 06C.1.375.01 DEG RSP5_2 RH spoiler #5 position |
| RSP5 FCDC2 06C.2.375.10 DEG RSP5_2 RH spoiler #5 position |
| RUDD SDAC1 029.1.312.00 DEG RUDD.1 Rudder position |
| RUDD SDAC2 029.2.312.00 DEG RUDD.2 Rudder position |
| RUDT FAC1 00A.1.313.00 DEG RUDT.1 Rudder Trim Position |
| RUDT FAC2 00A.2.313.00 DEG RUDT.2 Rudder Trim Position |
| SAT ADC1 006.1.213.01 DEGC SAT.1 Static air temperature |
| (BNR) |
| SAT ADC2 006.2.213.10 DEGC SAT.2 Static air temperature |
| (BNR) |
| SC1 SDAC1 029.1.242.01 DEGC/F SC1 Sel aft cab compt temp |
| SC1 SDAC2 029.2.242.01 DEGC/F SC1 Sel aft cab compt temp |
| SC2 SDAC1 029.1.244.01 DEGC/F SC2 Sel fwd cab compt temp |
| SC2 SDAC2 029.2.244.01 DEGC/F SC2 Sel fwd cab compt temp |
| SC3 SDAC1 029.1.245.01 DEGC/F SC3 Sel aft cab compt temp |
| SC3 SDAC2 029.2.245.01 DEGC/F SC3 Sel aft cab compt temp |
| SCC BSCU1 06E.1.340.01 DEG STEERCC Steering command |
| captain |
| SCC BSCU2 06E.2.340.10 DEG STEERCC Steering command |
| captain |
| SCFD BSCU1 06E.1.341.01 DEG STEERCFO Steering command F/O |
| SCFD BSCU2 06E.2.341.10 DEG STEERCFO Steering command F/O |
| SDS1 SDAC1 029.1.001.01 SDACSDS1 SDAC discrete status |
| word #1 |
| SDS1 SDAC2 029.2.001.01 SDACSDS2 SDAC discrete status |
| word #2 |
| SDS2 SDAC1 029.1.001.10 SDACSDS2 SDAC discrete status |
| word #2 |
| SDS2 SDAC2 029.2.001.10 SDACSDS2 SDAC discrete status |
| word #2 |
| SLAT SFCC1 01B.1.127.01 DEG SLAT_1 SLAT actual position |
| system #1 |
| SLAT SFCC2 01B.2.127.10 DEG SLAT_2 SLAT actual position |
| system #2 |
| SLP FAC1 00A.1.226.00 DEG SLP_1 Estimd sideslip (side |
| slip angle) syst.#1 |
| SLP FAC2 00A.2.226.00 DEG SLP_2 Estimd sideslip (side |
| slip angle) syst.#2 |
| SM ECU1 07C.1.273.01 SM_ACT_ON_1 Autostart mode active |
| engine #1 |
| SM ECU2 07C.2.273.10 SM_ACT_ON_2 Autostart mode active |
| engine #2 |
| SSEL1 SSEL1_1 Status of different |
| FADEC sensor: part 1 |
| SSEL1 SSEL1_2 Status of different |
| FADEC sensor: part 1 |
| SSEL2 SSEL2_1 Status of different |
| FADEC sensor: part 2 |
| SSEL2 SSEL2_2 Status of different |
| FADEC sensor: part 2 |
| SSEL3 SSEL3_1 Status of different |
| FADEC sensor: part 3 |
| SSEL3 SSEL3_2 Status of different |
| FADEC sensor: part 3 |
| SSEL4 SSEL4_1 Status of different |
| FADEC sensor: part 4 |
| SSEL4 SSEL4_2 Status of different |
| FADEC sensor: part 4 |
| STA SEC STA APU start time |
| STA01 STAB_R01 Stability status for |
| report 01 monitoring |
| STA02 STAB_R02 Stability status for |
| report 02 monitoring |
| STAB FCDC1 06C.1.315.01 DEG STAB.1 Stabilizer position #1 |
| STAB FCDC2 06C.2.315.10 DEG STAB.2 Stabilizer position #2 |
| STVC FWC1 026.1.032.01 SV_STV_CL_1 Scavenge valve stuck |
| closed engine #1 |
| STVC FWC2 026.2.032.01 SV_STV_CL_1 Scavenge valve stuck |
| closed engine #1 |
| STVC FWC1 026.1.032.10 SV_STV_CL_2 Scavenge valve stuck |
| closed engine #2 |
| STVC FWC2 026.2.032.10 SV_STV_CL_2 Scavenge valve stuck |
| closed engine #2 |
| STVO FWC1 026.1.032.01 SV_STV_OP_1 Scavenge valve stuck |
| open engine #1 |
| STVO FWC2 026.2.032.01 SV_STV_OP_1 Scavenge valve stuck |
| open engine #1 |
| STVO FWC1 026.1.032.10 SV_STV_OP_2 Scavenge valve stuck |
| open engine #2 |
| STVO FWC2 026.2.032.10 SV_STV_OP_2 Scavenge valve stuck |
| open engine #2 |
| SV EEC/ 07C.1.270.01 SV_OP_1 Starter air valve open |
| ECU1 (local switch) engine |
| #1 |
| SV EEC/ 07C.2.270.10 SV_OP_2 Starter air valve open |
| ECU2 (local switch) engine |
| #2 |
| SW1 ECU1 07C.1.270.01 ECUDSW1_1 ECU Discrete status |
| word #1 engine #1 |
| SW1 ECU2 07C.2.270.10 ECUDSW1_2 ECU Discrete status |
| word #1 engine #2 |
| SW2 ECU1 07C.1.272.01 ECUDSW2_1 ECU Discrete status |
| word #2 engine #1 |
| SW2 ECU2 07C.2.272.10 ECUDSW2_2 ECU Discrete status |
| word #2 engine #2 |
| SW3 ECU1 07C.1.273.01 ECUDSW3_1 ECU Discrete status |
| word #3 engine #1 |
| SW3 ECU2 07C.2.273.10 ECUDSW3_2 ECU Discrete status |
| word #3 engine #2 |
| SW4 ECU1 07C.1.274.01 ECUDSW4_1 ECU Discrete status |
| word #4 engine #1 |
| SW4 ECU2 07C.2.274.10 ECUDSW4_2 ECU Discrete status |
| word #4 engine #2 |
| SW5 ECU1 07C.1.275.01 ECUDSW5_1 ECU Discrete status |
| word #5 engine #1 |
| SW5 ECU2 07C.2.275.10 ECUDSW5_2 ECU Discrete status |
| word #5 engine #2 |
| T12 ECU1 07C.1.130.01 DEGC T12_1 T12 (Fan inlet |
| temperature) engine #1 |
| T25 EEC/ 07C.1.263.01 DEGC T25_1 T2.5 (Low Pressure |
| ECU1 Compressor exit |
| temperature) engine #1 |
| T25 EEC/ 07C.2.263.10 DEGC T25_2 T2.5 (Low Pressure |
| ECU2 Compressure exit |
| temperature) engine #2 |
| T3 EEC/ 07C.1.265.01 DEGC T3_1 T3 (High Pressure |
| ECU1 Compressor exit |
| temperature) engine #1 |
| T3 EEC/ 07C.2.265.10 DEGC T3_2 T3 (High Pressure |
| ECU2 Compressor exit |
| temperature) engine #2 |
| T5 ECU1 07C.1.260.01 DEGC T5_1 T5 (Low pressure |
| turbine-exit |
| temperature) engine #1 |
| T5 ECU2 07C.2.260.10 DEGC T5_2 T5 (Low pressure |
| turbine-exit |
| temperature) engine #2 |
| TAIL1 ACTAIL1 A/C ident word #1 (DMU |
| computed) |
| TAIL2 ACTAIL2 A/C ident word #2 (DMU |
| computed) |
| TAT ADC1 006.1.211.01 DEGC TAT_1 Total air temperature |
| (BNR) (switched |
| parameter) |
| TAT ADC2 006.2.211.10 DEGC TAT_2 Total air temperature |
| (BNR) (switched |
| parameter) |
| THDG IRS1 004.1.044.01 DEG THDG_1 TRUE HEADING system #1 |
| THDG IRS2 004.2.044.10 DEG THDG_2 TRUE HEADING system #2 |
| TLA ECU1 07C.1.133.01 DEG TLA_1 Selected TLA (Throttle |
| resolver angle) |
| engine #1 |
| TLA ECU2 07C.2.133.10 DEG TLA_2 Selected TLA (Throttle |
| resolver angle) |
| engine #2 |
| TN FWC1 026.1.322.01 DEGC TN_1 Nacelle temperature |
| engine #1 |
| TN FWC2 026.2.322.01 DEGC TN_1 Nacelle temperature |
| engine #2 |
| TN FWC1 026.1.322.10 DEGC TN_2 NACELLE TEMPERATURE |
| TN FWC2 026.2.322.10 DEGC TN_2 NACELLE TEMPERATURE |
| TNR DEG DTNREF_5 Delta TN reference |
| value in climb |
| TNR DEG DTNREF_6 Delta TN reference |
| value in cruise |
| TO DESTINATION Destination (DMU |
| COMPUTED) |
| TP PC/ 08E.1.121.11 DEGC TP_1 Pack outlet temperature |
| ACSC1 LH |
| TP PC/ 08E.2.121.00 DEGC TP_2 Pack outlet temperature |
| ACSC2 RH |
| TPO BMC1 06F.1.141.01 DEGC TPO_1 Precooler eng #1 outlet |
| temperature |
| TPO BMC2 06F.2.141.10 DEGC TPO_1 Precooler eng #1 outlet |
| temperature |
| TPO BMC1 06F.1.140.01 DEGC TPO_2 Precooler eng #2 outlet |
| temperature |
| TPO BMC2 06F.2.140.10 DEGC TPO_2 Precooler eng #2 outlet |
| temperature |
| TR ECU1 07C.1.273.01 TR_1 4 T/R Doors (stowed and |
| locked + deployed) |
| engine #1 |
| TR ECU2 07C.2.273.10 TR_2 4 T/R Doors (stowed and |
| locked + deployed) |
| engine #2 |
| TW PC/ 08E.1.111.11 DEGC TW_1 Pack water extr. |
| ACSC1 temperature LH |
| TW PC/ 08E.2.111.00 DEGC TW_2 Pack water extr. |
| ACSC2 temperature RH |
| UTC FDIU1 017.1.150.00 UTC UTC (Universal time |
| coordinated BNR) |
| V3 FAC1 00A.1.263.00 KTS V3 V3 (min. speed flaps |
| retr.) |
| V3 FAC2 00A.2.263.00 KTS V3 V3 (min. speed flaps |
| retr.) |
| V4 FAC1 00A.1.264.00 KTS V4 V4 (min. speed slats |
| retr.) |
| V4 FAC2 00A.2.264.00 KTS V4 V4 (min. speed slats |
| retr.) |
| VA ZC/ 05D.2.220.10 % VA CAB temp reg vlv pos |
| ACSC2 group 3 |
| VACC IRS1 004.1.364.01 G VACC Vertical acceleration |
| VACC IRS2 004.2.364.10 G VACC Vertical acceleration |
| VB1 EVM1 03D.1.135.01 % VB1_1 N1 vibration eng #1 |
| VB1 EVM1 03D.1.135.10 % VB1_2 N1 vibration eng #2 |
| VB2 EVM1 03D.1.136.01 UNITS VB2_1 N2 vibration eng #1 |
| VB2 EVM1 03D.1.136.10 UNITS VB2_2 N2 vibration eng #2 |
| VBV ECU1 07C.1.071.01 DEG VBV_1 Selected VBV position |
| (Variable bleed valve) |
| engine #1 |
| VBV ECU2 07C.2.071.10 DEG VBV_2 Selected VBV position |
| (Variable bleed valve) |
| engine #2 |
| VC EVM1 03D.1.230.01 IPS VC_1 Displace unbalance TRF |
| (LPT) eng1 |
| VC EVM1 03D.1.230.10 IPS VC_2 Displace unbalance TRF |
| (LPT) eng2 |
| VF ZC/ 05D.2.206.10 % VF CAB temp reg vlv pos |
| ACSC2 group 1 |
| VH EVM1 03D.1.230.11 IPS VH_1 N2 veloc unbalance BRG1 |
| (HPC) engine #1 |
| VH EVM1 03D.1.230.00 IPS VH_2 N2 veloc unbalance BRG1 |
| (HPC) engine #2 |
| VL EVM1 03D.1.227.01 MILS VL_1 TRF pick up N1 track |
| vibration eng 1 |
| VL EVM1 03D.1.227.10 MILS VL_1 TRF pick up N1 track |
| vibration eng 2 |
| VLS FAC1 00A.1.245.00 KTS VLS VLS (min airspeed) |
| VLS FAC2 00A.2.245.00 KTS VLS VLS (min airspeed) |
| VMAN FAC1 00A.1.265.00 KTS VMAN V man (maneuvering |
| speed) |
| VMAN FAC2 00A.2.265.00 KTS VMAN V man (maneuvering |
| speed) |
| VMAX FAC1 00A.1.207.00 KTS VMAX V max (max allowed |
| speed) |
| VMAX FAC2 00A.2.207.00 KTS VMAX V max (max allowed |
| speed) |
| VN EVM1 03D.1.227.01 MILS VN_1 Displace unbalance BRG1 |
| ENG1 |
| VN EVM1 03D.1.227.10 MILS VN_2 Displace unbalance BRG1 |
| ENG2 |
| VORF DMC1 025.1.034.01 MHZ VOR1_FREQ VOR 1 frequency |
| VORF DMC2 025.2.034.10 MHZ VOR2_FREQ VOR 2 frequency |
| VRTA SDAC1 029.1.333.01 G VRTACC Normal acceleration |
| VRTA SDAC2 029.2.333.10 G VRTACC Normal acceleration |
| VRTG IRS1 004.1.333.01 G VRTG Body normal |
| acceleration |
| VRTG IRS2 004.2.333.10 G VRTG Body normal |
| acceleration |
| VSCB PRESS1 05C.1.150.01 FT/MIN VSCB Cabin v/s |
| VSCB PRESS2 05C.2.150.02 FT/MIN VSCB Cabin v/s |
| VSV ECU1 07C.1.260.01 DEG VSV_1 Selected VSV position |
| (Variable stator vanes) |
| engine #1 |
| VSV ECU2 07C.2.260.10 DEG VSV_2 Selected VSV position |
| (Variable stator vanes) |
| engine #2 |
| VW ZC/ 05D.2.207.10 % VW CAB temp reg vlv pos |
| ACSC2 group 2 |
| WAI SDAC1 029.1.001.11 WAI_VLV_CL_1 LH wing anti ice valve |
| closed system #1 |
| WAI SDAC1 029.1.001.00 WAI_VLV_CL_2 RH wing anti ice valve |
| closed system #2 |
| WARN FWC1 026.1.126.00 FWC126DSW1 FWC Discrete status |
| word |
| WARN FWC2 026.2.126.00 FWC126DSW1 FWC Discrete status |
| word |
| WB APU1 07A.1.123.01 KG/S WB APU bleed air flow |
| WD IRS1 004.1.316.01 DEG WD_1 WIND DIRECTION true |
| system #1 |
| WD IRS2 004.2.316.10 DEG WD_2 WIND DIRECTION true |
| system #2 |
| WEFA1 MP14E WEFA interlock discrete |
| 1 |
| WEFA2 TP14H WEFA interlock discrete |
| 2 |
| WEFA3 MP14G WEFA interlock discrete |
| 2 |
| WFQ FQIC 05A.2.257.10 KG/LBS WFQ_1 Fuel quantity LH inner |
| cell system #1 |
| WFQ FQIC 05A.2.261.10 KG/LBS WFQ_2 Fuel quantity LH inner |
| cell system #2 |
| WS IRS1 004.1.315.01 KTS WS_1 WIND SPEED system #1 |
| WS IRS2 004.2.315.10 KTS WS_2 WIND SPEED system #2 |
| WS1 BSCU1 06E.1.320.01 M/S WS1 Wheel 1 speed |
| WS1 BSCU2 06E.2.320.10 M/S WS1 Wheel 1 speed |
| WS2 BSCU1 06E.1.321.01 M/S WS2 Wheel 2 speed |
| WS2 BSCU2 06E.2.321.10 M/S WS2 Wheel 2 speed |
| WS3 BSCU1 06E.1.322.01 M/S WS3 Wheel 3 speed |
| WS3 BSCU2 06E.2.322.10 M/S WS3 Wheel 3 speed |
| WS4 BSCU1 06E.1.323.01 M/S WS4 Wheel 4 speed |
| WS4 BSCU2 06E.2.323.10 M/S WS4 Wheel 4 speed |
| YAW IRS1 004.1.330.01 DEG/S YAW Body axis YAW rate |
| YAW IRS2 004.2.330.10 DEG/S YAW Body axis YAW rate |
| ZCACI ZC/ 05D.2.060.10 ZC_ACSC_STS ZC and PACK/ACSC |
| ACSC2 selection status |
| ZCACO ZC_ACSC_CNF ZC and PACK/ACSC |
| configuration selected |
| ZCB PRESS1 05C.1.151.01 FEET ZCB Cabin altitude |
| ZCB PRESS2 05C.2.151.10 FEET ZCB Cabin altitude |
| ZDW1 ZC/ 05D.2.060.10 ZC060DW Discrete data word |
| ACSC2 (Label 060) Zone |
| Controller bus2 |
| ZLD PRESS1 05C.1.163.01 FEET ZLD Landing elevation |
| ZLD PRESS2 05C.2.163.10 FEET ZLD Landing elevation |
NOTE: This Alpha Call-Up list is for PW engines only.
| ------------------------------------------------------------------------------- |
| Alpha Source Parameter Unit Parameter Comment |
| Call-Up number |
| -------------------------------------------------------------------------------- |
| ABDS EIU1 07B.1.276.XX DISCRETE ABDS.1 Aborted Start detected |
| ABDS EIU2 07B.2.276.XX DISCRETE ABDS.2 Aborted Start detected |
| ACCT EIU1 07B.1.163.XX mA ACCT.1 ACC Valve Torque motor |
| current |
| ACCT EIU2 07B.2.163.XX mA ACCT.2 ACC Valve Torque motor |
| current |
| ACID FDIU 017.1.301.00 ACID(1 TO 3) Aircraft Identification |
| (Tail Number) |
| ACID FDIU 014.1.302.00 ACID(4 TO 6) Aircraft Identification |
| (Tail Number) |
| ACID FDIU 014.1.303.00 CID(7 TO 9) Aircraft Identification |
| (Tail Number) |
| ACTYP ACTYPE A/C Type (DMU computed) |
| ACW1 ACW1 APU control word #1 |
| (DMU computed) |
| ACW2 ACW2 APU control word #2 |
| (DMU computed) |
| ACW3 ACW3 APU control word #3 |
| (DMU computed) |
| ACW4 ACW4 APU control word #4 |
| (DMU computed) |
| ACYC CYCLES ACYC APU cycles |
| (DMU computed) |
| ACYI APU1 07A.1.133.01 CYCLES ACYI APU start cycles |
| ACYI APU1 07A.1.136.01 CYCLES ACYI APU start cycles |
| ADIR1 ADIR1_PN_P1 ADIRU hardware P/N |
| (DMU computed from |
| ADC1 bus) |
| ADIR1 ADIR1_PN_P2 |
| ADIR1 ADIR1_PN_P3 |
| ADIR2 ADIR2_PN_P1 ADIRU hardware P/N |
| (DMU computed from |
| ADC2 bus) |
| ADIR2 ADIR2_PN_P2 |
| ADIR2 ADIR2_PN_P3 |
| ADIR3 ADIR3_PN_P1 ADIRU hardware P/N |
| (DMU computed from |
| ADC3 bus) |
| ADIR3 ADIR3_PN_P2 |
| ADIR3 ADIR3_PN_P3 |
| ADW1 APU1 07A.1.037.01 APUDSW1 APU:Discrete status |
| word #1 |
| AHRI APU1 07A.1.132.01 H AHRI APU operating hours |
| AHRI APUI 071.1.135.01 H AHRI APU operating hours |
| AHRS H AHRS APU hours (DMU |
| computed) |
| AIL FCDC1 06C.1.310.01 DEG AIL_1 Aileron position left |
| AIL FCDC1 06C.1.330.01 DEG AIL_2 Aileron position right |
| AILL FCDC1 06C.1.310.01 DEG AIL_1 Aileron position left |
| AILL FCDC2 06C.1.310.10 DEG AIL_1 Aileron position left |
| AILR FCDC1 06C.1.330.01 DEG AIL_2 Aileron position right |
| AILR FCDC2 06C.2.330.10 DEG AIL_2 Aileron position right |
| ALT ADC1 006.1.203.01 FEET ALT Altitude (1013.25mb) |
| (switched parameter) |
| ALT ADC2 006.2.203.10 FEET ALT Altitude (1013.25mb) |
| (switched parameter) |
| ALT3 FWC 026.1.203.11 FEET ALT3 Altitude 3 (1013.25ha) |
| ALTR FGC1 001.1.365.00 FT/MIN ALTRATE Altitude rate (VZBI) |
| ALTR FGC2 001.2.365.00 FT/MIN ALTRATE Altitude rate (VZBI) |
| AMW1 APU1 07A.1.353.01 APUMW1 APU: Maintenance |
| word #1 |
| AMW2 APU1 07A.1.351.01 APUMW2 APU: Maintenance |
| word #2 |
| AMW3 APU1 07A.1.352.01 APUMW3 APU: Maintenance |
| word #3 |
| AOA ADC1 006.1.241.01 DEG AOA_1 Corrected angle of |
| attack system #1 |
| AOA ACD2 006.2.241.10 DEG AOA_2 Corrected angle of |
| attack system #2 |
| AOA3 FWC1 026.1.241.11 DEG AOA3 Corrected angle of |
| attack 3 |
| AOC EIU1 07B.1.332.XX % AOC.1 The engine Air Oil |
| Collar valve feedback |
| AOC EIU2 07B.2.332.XX % AOC.2 The engine Air Oil |
| Collar valve feedback |
| AOCOC EIU1 07B.1.040.XX % AOCOC.1 Engine Air cooler |
| actuator open command |
| AOCOC EIU2 07B.1.040.XX % AOCOC.2 Engine Air cooler |
| actuator open command |
| AP AP_1 Auto pilot status (AP) |
| left |
| AP AP_2 Auto pilot status (AP) |
| right |
| APLAT AP_LAT_1 A/P lateral mode left |
| APLAT AP_LAT_2 A/P lateral mode right |
| APLCT APU1 07A.1.110.01 DEGC APU_LCIT APU Load compressor |
| inlet temperature |
| APLON AP_LON_1 A/P longitudinal mode |
| left |
| APLON AP_LON_2 A/P longitudinal mode |
| right |
| APMW1 APU1 07A.1.353.01 APUMW1 APU: Maintenance |
| word #1 |
| APMW1 APU1 07A.1.351.01 APUMW2 APU: Maintenance |
| word #2 |
| APMW1 APU1 07A.1.352.01 APUMW3 APU: Maintenance |
| word #3 |
| APRPM APU1 07A.1.176.01 %RPM APU_RPM APU RPM BNR LINEAR(A*X) |
| APU APU1 07A.1.037.01 APU_BLDV_OPF APU Bleed Valve-Bit 11 |
| ASN APU1 07A.1.050.01 ASN APU serial number |
| B25 EIU1 07B.1.323.XX % B25.1 Stage 2.5 bleed valve |
| actuator percent open |
| command - 100%=1.94 in |
| B25 EIU2 07B.2.323.XX % B25.2 Stage 2.5 bleed valve |
| actuator percent open |
| command - 100%=1.94 in |
| BAF EIU1 07B.1.335.XX % BAF.1 The engine 2.5 position |
| bleed Actuator Feedback |
| BAF EIU2 07B.2.335.XX % BAF.2 The engine 2.5 position |
| bleed Actuator Feedback |
| BBF EIU1 07B.1.236.XX IPS BBF.1 Broad Band Vibration |
| Front |
| BBF EIU2 07B.2.236.XX IPS BBF.2 Broad Band Vibration |
| Front |
| BBR EIU1 07B.1.237.XX IPS BBR.1 Broad Band Vibration |
| Rear |
| BBR EIU2 07B.2.237.XX IPS BBR.2 Broad Band Vibration |
| Rear |
| BBV EIU1 07B.1.235.XX IPS BBR.2 Broadband Vibration |
| BBV EIU2 07B.2.235.XX IPS BBV.2 Broadband Vibration |
| BCV APU1 07A.1.131.01 % BCV Bleed Control Valve |
| Position |
| BLOPF APU1 07A.1.037.01 APU_BLDV_OPF APU Bleed valve open |
| (filtered) |
| BP1 BSCU1 06E.1.300.01 BAR BP1 Brake 1 pressure |
| BP1 BSCU2 06E.2.300.10 BAR BP1 Brake 1 pressure |
| BP2 BSCU1 06E.1.301.01 BAR BP2 Brake 2 pressure |
| BP2 BSCU2 06E.1.301.10 BAR BP2 Brake 2 pressure |
| BP3 BSCU1 06E.1.302.01 BAR BP3 Brake 3 pressure |
| BP3 BSCU2 06E.1.302.10 BAR BP3 Brake 3 pressure |
| BP4 BSCU1 06E.1.303.01 BAR BP4 Brake 4 pressure |
| BP4 BSCU2 06E.1.303.10 BAR BP4 Brake 4 pressure |
| BT1 BSCU1 06E.1.114.01 DEG C BT1 Brake 1 temperature |
| BT1 BSCU2 06E.2.114.10 DEG C BT1 Brake 1 temperature |
| BT2 BSCU1 06E.1.115.01 DEG C BT2 Brake 2 temperature |
| BT2 BSCU2 06E.2.115.10 DEG C BT2 Brake 2 temperature |
| BT3 BSCU1 06E.1.116.01 DEG C BT3 Brake 3 temperature |
| BT3 BSCU2 06E.2.116.10 DEG C BT3 Brake 3 temperature |
| BT4 BSCU1 06E.1.117.01 DEG C BT4 Brake 4 temperature |
| BT4 BSCU2 06E.2.117.10 DEG C BT4 Brake 4 temperature |
| BTMC EIU1 07B.1.162.XX mA BTMC.1 2.5 BldAct Torque |
| motor current |
| BTMC EIU2 07B.2.162.XX mA BTMC.2 2.5 BldAct Torque |
| motor current |
| BVP FWC1 026.1.031.01 BVP_OP_1 Scavenge valve open |
| engine #1 |
| BVP FWC1 026.1.031.10 BVP_OP_2 Scavenge valve open |
| engine #2 |
| CAS ADC1 006.1.206.01 KTS CAS Computed air speed |
| (switched parameter) |
| CAS ADC2 006.1.206.10 KTS CAS Computed air speed |
| (switched parameter) |
| CAS3 FWC1 026.1.206.11 KTS CAS3 Computed air speed 3 |
| CC EIU1 07B.1.270.XX DISCRETE CC.1 Channel in Control |
| CC EIU1 07B.2.270.XX DISCRETE CC.2 Channel in Control |
| CFPG D_CFPG_1 Calculated flight |
| path acceleration |
| system #1 (DMU Computed) |
| CFPG D_CFPG_2 Calculated flight |
| path acceleration |
| system #2 (DMU Computed) |
| CG FMC1 002.1.077.00 %MAC CG Long center of gravity |
| (switched computed) |
| CG FMC2 002.2.077.00 %MAC CG Long center of gravity |
| (switched computed) |
| CIVV D_CIVV_1 Calculated inertial |
| vertical speed system |
| #2 (DMU Computed) |
| CIVV D_CIVV_2 Calculated inertial |
| vertical speed system |
| #2 (DMU Computed) |
| CNT DMU RCOUNT Report count |
| CPC DISCRETE CPC System in Control |
| COT PC/ACSC1 08E.1.123.11 DEG C COT_1 Pack compr. outlet |
| temperature LH |
| COT PC/ACSC2 08E.2.123.11 DEG C COT_1 Pack compr. outlet |
| temperature RH |
| CSV1 BSCU1 06E.1.310.01 MA CSV1 Current SNV1 |
| CSV1 BSCU2 06E.2.310.10 MA CSV1 Current SNV1 |
| CSV2 BSCU1 06E.1.311.01 MA CSV2 Current SNV2 |
| CSV2 BSCU2 06E.2.311.10 MA CSV2 Current SNV2 |
| CSV3 BSCU1 06E.1.312.01 MA CSV3 Current SNV3 |
| CSV3 BSCU2 06E.2.312.10 MA CSV3 Current SNV3 |
| CSV4 BSCU1 06E.1.313.01 MA CSV4 Current SNV4 |
| CSV4 BSCU2 06E.2.313.10 MA CSV4 Current SNV4 |
| DA IRS1 004.1.321.01 DEG DRIFT Drift angle |
| DA IRS2 004.2.321.10 DEG DRIFT Drift angle |
| DATE FDIU1 017.1.260.00 DATE GMT date |
| DBFL EIU1 07B.1.370.XX Ferrous DBFL.1 Debris Rate Non- |
| Particles Ferrous-Long term |
| DBFL EIU2 07B.2.370.XX Ferrous DBFL.2 Debris Rate Non- |
| Particles Ferrous-Long-term |
| DBFS EIU1 07B.1.371.XX Ferrous DBFS.1 Debris Rate Ferrous |
| Particles Short-term |
| DBFS EIU2 07B.2.371.XX Ferrous DBFS.2 Debris Rate Ferrous |
| Particles Short-term |
| DBNFL EIU1 07B.1.372.XX Ferrous DBNFL.1 Debris Rate Non- |
| Particles Ferrous-Long-term |
| DBNFL EIU2 07B.2.372.XX Ferrous DBNFL.2 Debris Rate Non- |
| Particles Ferrous-Long-term |
| DBNFS EIU1 07B.1.374.XX Ferrous DBNFS.1 Debris Rate Ferrous |
| Particles Short-term |
| DBNFS EIU2 07B.2.374.XX Ferrous DBNFS.2 Debris Rate Ferrous |
| Particles Short-term |
| DFLM Ferrous Debris Rate Ferrous |
| Particles Long-term(Max) |
| DFSM Ferrous Debris Rate Ferrous |
| Particles Short-term (Max) |
| DMEF DMC1 025.1.035.01 MHZ DME1_FREQ DME 1 frequency |
| DMEF DMC1 025.1.035.10 MHZ DME2_FREQ DME 2 frequency |
| DNFLM Ferrous Debris Rate Ferrous |
| Particles Long-term (Max) |
| DNFSM Ferrous Debris Rate Ferrous |
| Particles Short-term (Max) |
| DPA APU1 07A.1.165.01 PSID DPA Delta Pressure for |
| APIC APUs |
| DPH EIU1 07B.1.227.XX IPS DPH.1 Displacement Unbalance |
| for PHMU |
| DPH EIU2 07B.2.227.XX IPS DPH.2 Displacement Unbalance |
| for PHMU |
| DSW1 BSCU1 06E.1.270.01 BSCUDSW1 BSCU discrete status |
| word #1 |
| DSW1 BSCU2 06E.2.270.10 BSCUDSW1 BSCU discrete status |
| word #1 |
| DSW2 BSCU1 06E.1.026.01 BSCUDSW2 BSCU discrete status |
| word #2 |
| DSW2 BSCU2 06E.2.026.10 BSCUDSW2 BSCU discrete status |
| word #2 |
| DSW3 BSCU1 06E.1.027.01 BSCUDSW3 BSCU discrete status |
| word #3 |
| DSW3 BSCU2 06E.2.027.10 BSCUDSW3 BSCU discrete status |
| word #3 |
| DT1A1 DT1A1_P1 Static source error |
| correction (DMU |
| computed from ADC1 bus) |
| DT1A1 DT1A1_P2 |
| DT1A1 DT1A1_P3 |
| DT1A2 DT1A2_P1 Static source error |
| correction (DMU |
| computed from ADC2 bus) |
| DT1A2 DT1A2_P2 |
| DT1A2 DT1A2_P3 |
| DT1A3 DT1A3_P1 Static source error |
| correction (DMU |
| computed from ADC3 bus) |
| DT1A3 DT1A3_P2 |
| DT1A3 DT1A3_P3 |
| DT2A1 DT2A1_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC1 bus) |
| DT2A1 DT2A1_P2 |
| DT2A1 DT2A1_P3 |
| DT2A2 DT2A2_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC1 bus) |
| DT2A2 DT2A2_P2 |
| DT2A2 DT2A2_P3 |
| DT2A2 DT2A2_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC2 bus) |
| DT2A2 DT2A2_P2 |
| DT2A2 DT2A2_P3 |
| DT2A3 DT2A3_P1 Magnetic Variable Table |
| (DMU computed from |
| ADC3 bus) |
| DT2A3 DT2A3_P2 |
| DT2A3 DT2A3_P3 |
| EAMI EIU1 07B.1.066.xx DISCRETE EAM.1 Engine Above Min Idle |
| EAMI EIU2 07B.2.066.xx DISCRETE EAM.2 Engine Above Min Idle |
| ECYC ECYC_1 Engine #1 cycles |
| (DMU computed) |
| ECYC ECYC_2 Engine #2 cycles |
| (DMU computed) |
| EGT EIU1 07B.1.345.XX DEG C EGT.1 Selected Cockpit Exhaust |
| Gas Temperature from the |
| engine (Station 5) |
| EGT EIU2 07B.2.345.XX DEG C EGT.2 Selected Cockpit Exhaust |
| Gas Temperature from the |
| engine (Station 5) |
| EGTA APU1 07A.1.175.01 DEG C APU_EGT APU EGT |
| EGTB EIU1 07B.1.321.XX DEG C EGTB.1 Selected unshunted |
| turbine Gas total |
| Temperature |
| EGTB EIU2 07B.2.321.XX DEG C EGTB.2 Selected unshunted |
| turbine Gas total |
| Temperature |
| EGTF DEG C EGT_1_F EGT LPT exit temp |
| engine #1: Filtered |
| parameter |
| EGTF DEG C EGT_2_F EGT LPT exit temp |
| engine #2: Filtered |
| parameter |
| EGTK DMU EGTK_1 EGT corrected left |
| (DMU computed) |
| EGTK DMU EGTK_2 EGT corrected left |
| (DMU computed) |
| EGTP DEG C APU_EGT_PEAK APU EGT PEAK during |
| APU start |
| EGTR DEG DEGTREF_5 Delta egt reference |
| value in climb |
| EGTRD EIU1 07B.1.120.XX DISCRETE EGTRD.1 EGT Redline exceeded |
| EGTRD EIU2 07B.2.120.XX DISCRETE EGTRD.2 EGT Redline exceeded |
| EHRS DMU HOURS EHRS_1 Engine #1 hours |
| (DMU computed) |
| EHRS DMU HOURS EHRS_2 Engine #2 hours |
| (DMU computed) |
| ELA1 ELAC1_PN_P1, ELAC 1 software P/N |
| ELAC1_PN_P2 (DMU computed from data |
| transmitted of FCDC bus) |
| ELA1 ELAC1_PN_P3 |
| ELA2 ELAC2_PN_P1, ELAC 2 software P/N |
| ELAC2_PN_P2 (DMU computed from data |
| transmitted of FCDC bus) |
| ELA2 ELAC2_PN_P3 |
| ELEL FCDC1 06C.1.314.01 DEG ELEV.1.1 Elevator position Left |
| ELEL FCDC2 06C.2.314.10 DEG ELEV.1.2 Elevator position Left |
| ELER FCDC1 06C.1.334.01 DEG ELEV.2.1 Elevator position Right |
| ELER FCDC2 06C.1.334.10 DEG ELEV.2.2 Elevator position Right |
| ELEV FCDC1 06C.1.314.01 DEG ELEV_1 Elevator position Left |
| ELEV FCDC1 06C.1.334.01 DEG ELEV_2 Elevator position Left |
| ENGFL EIU1 07B.1.276.XX DISCRETE ENGFL.1 Engine fail detected |
| ENGFL EIU2 07B.2.276.XX DISCRETE ENGFL.2 Engine fail detected |
| ENGFA FDIU1 017.1.304.00 ENGFAMILY A/C type engine |
| ENGRG EIU1 07B.1.270.XX ENGRG.1 Engine running |
| ENGRG EIU2 07B.2.270.XX ENGRG.1 Engine running |
| ENTYP ENGTYPE Engine type |
| (DMU computed) |
| EOPT EIU1 07B.1.161.XX HOURS EOPT.1 Engine Operating Time |
| EOPT EIU2 07B.2.161.XX HOURS EOPT.2 Engine Operating Time |
| ERUS FWC 026.1.031.01 DISCRETE ERUS.1.1.14 Engine 1 master Lever |
| Selected On |
| ERUS FWC 026.2.031.01 DISCRETE ERUS.2.1.14 Engine 1 master Lever |
| Selected On |
| ERUS FWC 026.1.031.10 DISCRETE ERUS.1.2.14 Engine 2 master Lever |
| Selected On |
| ERUS FWC 026.2.031.10 DISCRETE ERUS.2.2.14 Engine 2 master Lever |
| Selected On |
| ESN EIU1 07B.1.046.XX ESN1.1 ENGINE SERIAL NUMBER |
| ESN EIU1 07B.2.047.XX ESN1.2 ENGINE SERIAL NUMBER |
| ESN EIU2 07B.1.046.XX ESN2.1 ENGINE SERIAL NUMBER |
| ESN EIU2 07B.2.047.XX ESN2.2 ENGINE SERIAL NUMBER |
| ESWPN EXSWPN1 Extended Software Part |
| Number (EXSWPN) for |
| Vendor and Engine Type |
| ESWPN EXSWPN2 Extended Software Part |
| Number (EXSWPN) for |
| Vendor and Engine Type |
| ESWPN EXSWPN3 Extended Software Part |
| Number (EXSWPN) for |
| Vendor and Engine Type |
| ESWPN FDIMU Extended Software |
| Part number |
| F320 SFCC1 01B.1.137.01 DEG FLAP_1_A320 FLAP actual position |
| left for A320 A/C |
| F320 SFCC2 01B.2.137.10 DEG FLAP_2_A320 FLAP actual position |
| right for A320 A/C |
| FD FQIC 05A.2.272.10 Kg/l FL_L Fuel density left wing |
| tank (DMU computed) |
| FD FQIC 05A.2.272.10 Kg/l FL_R Fuel density right wing |
| tank (DMU computed) |
| FDC FD_C Fuel density center |
| wing tank (DMU computed) |
| FDL FD_L Fuel density left wing |
| tank (DMU computed) |
| FDP EIU1 07B.1.311.XX PSIG FDP.1 Engine Fuel Delta |
| Pressure |
| FDP EIU2 07B.2.311.XX PSIG FDP.2 Engine Fuel Delta |
| Pressure |
| FDR FD_R Fuel density right wing |
| tank (DMU computed) |
| FDRAW FQU2 05A.2.272.10 FUEL_D Fuel density |
| FEDET EIU1 07B.1.071.XX Ferrous FEDET.1 Cumulative number of |
| Particles ferrous particles |
| detected |
| FEDET EIU2 07B.2.071.XX Ferrous FEDET.2 Cumulative number of |
| Particles ferrous particles |
| detected |
| FF EIU1 07B.1.244.XX PPH FF.1 Engine Fuel Flow |
| FF EIU2 07B.2.244.XX PPH FF.2 Engine Fuel Flow |
| FFAN EIU1 07B.1.173.XX IPS FFAN.1 Front Vibe Sensor FAN |
| SO1 |
| FFAN EIU2 07B.2.173.XX IPS FFAN.2 Front Vibe Sensor FAN |
| SO1 |
| FFK DMU PPH FFK_1 Fuel flow corrected |
| engine #1 |
| FFK DMU PPH FFK_2 Fuel flow corrected |
| engine #2 |
| FFR EIU1 07B.1.347.XX PPH FFR.1 Fuel Metering Valve |
| Position Feedback |
| FFR EIU1 07B.2.347.XX PPH FFR.2 Fuel Metering Valve |
| Position Feedback |
| FLAP SFFC1 01B.1.137.01 DEG FLAP_1 FLAP actual position |
| left |
| FLAP SFFC2 01B.2.137.01 DEG FLAP_2 FLAP actual position |
| right |
| FLAPW DEG FLAP FLAP actual position |
| switched |
| FLCNT FLCNT Flight counter |
| (DMU computed) |
| FLNUM FLINUM Flight number (DMU |
| (DMU computed) |
| FLOT EIU1 07B.1.276.XX DISCRETE FLOT.1 Flame out detected |
| FLOT EIU2 07B.2.276.XX DISCRETE FLOT.2 Flame out detected |
| FLT FMGC1 001.1.233.00 FLT(11,12) A/C identification |
| tail number |
| FLT FMGC2 001.2.233.00 FLT(21,22) A/C identification |
| tail number |
| FLT FMGC1 001.1.234.00 FLT(13,14) A/C identification |
| tail number |
| FLT FMGC2 001.2.234.00 FLT(23,24) A/C identification |
| tail number |
| FLT FMGC1 001.1.235.00 FLT(15,16) A/C identification |
| tail number |
| FLT FMGC2 001.2.235.00 FLT(25,26) A/C identification |
| tail number |
| FLT FMGC1 001.1.236.00 FLT(17,18) A/C identification |
| tail number |
| FLT FMGC2 001.2.236.00 FLT(27,28) A/C identification |
| tail number |
| FM FLIMOD_DISP Flight phase to |
| display (DMU computed) |
| FMB FLIMOD_BROAD Flight phase broad |
| casted to ACARS (DMU |
| computed) |
| FMF FWC1 026.1.126.01 FM_FWC Flight phases |
| FMF FWC1 026.2.126.01 FM_FWC Flight phases |
| FMFF FM_FWC_F Flight phases filtered |
| FMGD1 FGC1 001.1.274.00 FMGCDSW1 FMGC discrete status |
| word #1 |
| FMGD1 FGC2 001.2.275.00 FMGCDSW2 FMGC discrete status |
| word #2 |
| FMGD2 FGC1 001.1.275.00 FMGCDSW2 FMGC discrete status |
| word #2 |
| FMGD2 FGC2 001.2.275.00 FMGCDSW2 FMGC discrete status |
| word #2 |
| FMGD4 FGC1 001.1.146.00 FMGCDSW4 FMGC discrete status |
| word #4 |
| FMGD4 FGC2 001.2.146.00 FMGCDSW4 FMGC discrete status |
| word #4 |
| FMI FLIMOD_INT Internal flight phase |
| (DMU computed) |
| FMVC EIU1 07B.1.334.XX PPH FMVC.1 Fuel Metering Valve |
| command |
| FMVC EIU2 07B.2.334.XX PPH FMVC.2 Fuel Metering Valve |
| command |
| FMVT EIU1 07B.1.164.XX mA FMVT.1 FMV Torque motor |
| current feedback |
| FMVT EIU2 07B.2.164.XX mA FMVT.2 FMV Torque motor |
| current feedback |
| FO SDAC1 029.1.004.01 DISCRETE FO.1.18 Fuel pump active |
| (RH & LH) |
| FO SDAC2 029.2.004.10 DISCRETE FO.2.18 Fuel pump active |
| (RH & LH) |
| FOC EIU1 07B.1.212.XX % FOC.1 FOC Position Feedback |
| FOC EIU2 07B.2.212.XX % FOC.2 FOC Position Feedback |
| FOCB EIU1 07B.1.357.XX PSIA FOCB.1 FOC bypass indication |
| FOCB EIU2 07B.2.357.XX PSIA FOCB.2 FOC bypass indication |
| FOCVP EIU1 07B.1.251.XX % FOCVP.1 Fuel oil cooler |
| bypass valve position |
| FOCVP EIU2 07B.2.251.XX % FOCVP.2 Fuel oil cooler |
| bypass valve position |
| FPA IRS1 004.1.322.01 DEG FPA Flight path angle |
| FPA IRS2 004.2.322.10 DEG FPA Flight path angle |
| FPAC IRS1 004.1.323.01 G FPAC Flight path |
| acceleration |
| FPAC IRS2 004.2.323.10 G FPAC Flight path |
| acceleration |
| FPPU SFCC1 01B.1.137.01 DEG FLAP_RAW Flap actual position |
| (switched parameter) |
| FPPU SFCC2 01B.2.137.10 DEG FLAP_RAW Flap actual position |
| (switched parameter) |
| FROM ORIGIN Departure (DMU computed) |
| FRTO FMGC 1 001.1.040.DD FROM(11,12,13) Identification of CITY |
| PAIR |
| FRTO FMGC 2 001.2.040.DD FROM(21,22,23) Identification of CITY |
| PAIR |
| FRTO FMGC 1 001.1.041.DD FROM(14,15,16) Identification of CITY |
| PAIR |
| FRTO FMGC 2 001.2.041.DD FROM(24,25,26) Identification of CITY |
| PAIR |
| FRTO FMGC 1 001.1.042.DD FROM(17,18,19) Identification of CITY |
| PAIR |
| FRTO FMGC 2 001.2.042.DD FROM(27,28,29) Identification of CITY |
| PAIR |
| FT FQIC 05A.2.177.10 DEG C SE01.1.14 Fuel temperature |
| engine #1 |
| FT FQIC 05A.2.201.10 DEG C PSE01.1.14 Fuel temperature |
| engine #2 |
| FTBA EUI1 07B.1.055.XX A FTBA.1 Fan Trim Balance |
| Solution angle |
| FTBA EUI2 07B.2.055.XX A FTBA.2 Fan Trim Balance |
| Solution angle |
| FTBM EUI1 07B.1.054.XX A FTBM.1 Fan Trim Balance |
| Solution Magnitude |
| FTBM EUI2 07B.2.054.XX A FTBM.2 Fan Trim Balance |
| Solution Magnitude |
| FTO FGC1 001.1.272.00 A FTO_1 Flex T/O selected #1 |
| FTO FGC2 001.2.272.00 A FTO_2 Flex T/O selected #2 |
| FVD EIU1 07B.1.056.XX IPS FVD.1 Front Vibe Sensor |
| Deoiler schaft SO1 |
| FVD EIU2 07B.2.056.XX IPS FVD.2 Front Vibe Sensor |
| Deoiler schaft SO1 |
| FVL EIU1 07B.1.057.XX IPS FVL.1 Front Vibe Sensor |
| Layschaft SO1 |
| FVL EIU2 07B.2.057.XX IPS FVL.2 Front Vibe Sensor |
| Layschaft SO1 |
| FVL EIU1 07B.1.061.XX IPS FVMF.1 Front Vibe Sensor |
| Main Fuel Pump SO1 |
| FVL EIU2 07B.2.061.XX IPS FVMF.2 Front Vibe Sensor |
| Main Fuel Pump SO1 |
| FVMO EIU1 07B.1.062.XX IPS FVMO.1 Front Vive Sensor |
| Main Oil Pump SO1 |
| FVM0 EIU2 07B.2.062.XX IPS FVMO.2 Front Vive Sensor |
| Main Oil Pump SO1 |
| FVN1 EIU1 07B.1.171.XX IPS FVN1.1 Front Vibe Sensor |
| N1 SO1 |
| FVN1 EIU2 07B.1.171.XX IPS FVN1.2 Front Vibe Sensor |
| N1 SO1 |
| FVN2 EIU1 07B.1.172.XX IPS FVN1.1 Front Vibe Sensor |
| N1 SO1 |
| FVN2 EIU2 07B.1.172.XX IPS FVN1.2 Front Vibe Sensor |
| N1 SO1 |
| FVO EIU1 07B.1.145.XX DISCRETE FVO.1 Front valve Open |
| FVO EIU2 07B.2.145.XX DISCRETE FVO.2 Front valve Open |
| FVP EIU1 07B.1.145.XX IPS FVP.1 Front Vibe PMA schaft |
| SO1 |
| FVP EIU1 07B.1.145.XX IPS FVP.2 Front Vibe PMA schaft |
| SO1 |
| FVT EIU1 07B.1.063.XX IPS FVT.1 Front Vibe Sensor Tower |
| schaft SO1 |
| FVT EIU2 07B.2.063.XX IPS FVT.2 Front Vibe Sensor Tower |
| schaft SO1 |
| GLA SDAC1 029.1.100.00 % GLA APU generator load |
| GLA SDAC2 029.2.100.00 % GLA APU generator load |
| GLE SDAC1 029.1.077.01 % GLE_1 Generator load |
| engine #1 |
| GLE SDAC2 029.2.077.01 % GLE_1 Generator load |
| engine #2 |
| GLE SDAC1 029.1.077.10 % GLE_2 Engine Generator load |
| GLE SDAC2 029.2.077.10 % GLE_2 Engine Generator load |
| GLS DMC1 025.1.174.01 DDM GLS1 ILS1 glideslope |
| deviation |
| GLS DMC1 025.1.174.10 DDM GLS2 ILS2 glideslope |
| deviation |
| GS IRS1 004.1.312.01 KTS GS Ground speed |
| GS IRS2 004.2.312.10 KTS GS Ground speed |
| GSF GS_F Ground speed (filtered) |
| GW FMC1 002.1.075.00 10Kg GW Actual Gross Weight |
| GW FMC2 002.2.075.00 10Kg GW Actual Gross Weight |
| GWFK FAC1 00A.1.074.00 KG GWFK Gross weight FAC (kg) |
| GWFK FAC2 00A.2.074.00 KG GWFK Gross weight FAC (kg) |
| GWFK FAC1 00A.1.074.00 LBS GWFK Gross weight FAC (lbs) |
| GWFK FAC2 00A.2.074.00 LBS GWFK Gross weight FAC (lbs) |
| HUD1 HUD1_PN_P1 HUDC1 Software P/N |
| (DMU computed from |
| HUDC bus) |
| HUD1 HUD1_PN_P2 |
| HUD1 HUD1_PN_P3 |
| HUD2 HUD2_PN_P1 HUDC1 Software P/N |
| (DMU computed from |
| HUDC bus) |
| HUD2 HUD2_PN_P2 |
| HUD2 HUD2_PN_P3 |
| HUNG EIU1 07B.1.276.XX DISCRETE HUNG.1 HPC SVA Torque motor |
| current |
| HUNG EIU2 07B.2.276.XX DISCRETE HUNG.2 HPC SVA Torque motor |
| current |
| IALT IRS1 004.1.361.NA FEET IALT Inertial altitude |
| IALT IRS2 004.2.361.NA FEET IALT Inertial altitude |
| IGC1 EIU1 07B.1.315.XX DISCRETE IGC1.1 Ignition 1 Commanded |
| IGC1 EIU2 07B.2.315.XX DISCRETE IGC1.2 Ignition 1 Commanded |
| IGC2 EIU1 07B.1.315.XX DISCRETE IGC2.1 Ignition 2 Commanded |
| IGC2 EIU2 07B.2.315.XX DISCRETE IGC2.2 Ignition 2 Commanded |
| IGV APU1 07A.1.130.01 DEG IGV APU IGV position |
| ILS DMC1 025.1.033.01 MHZ ILS1_FREQ ILS1 frequency |
| ILS DMC1 025.1.033.10 MHZ ILS2_FREQ ILS2 frequency |
| IVV IRS1 004.1.365.01 FT/MIN IVV Initial vertical speed |
| IVV IRS2 004.2.365.10 FT/MIN IVV Initial vertical speed |
| JOIP EIU1 07B.1.125.XX PSIA JOIP.1 Journal Oil Pressure |
| JOIP EIU2 07B.2.125.XX PSIA JOIP.2 Journal Oil Pressure |
| LATA SDAC1 029.1.332.01 G LATACC Lateral acceleration |
| LATA SDAC2 029.2.332.01 G LATACC Lateral acceleration |
| LATG IRS1 004.1.332.01 G LATG Body lateral |
| acceleration |
| LATG IRS2 004.2.332.10 G LATG Body lateral |
| acceleration |
| LATP IRS1 004.1.310.NA DEG LATP_1 Present position |
| latitude system 1 |
| LATP IRS2 004.2.310.NA DEG LATP_2 Present position |
| latitude system 2 |
| LCDT APU1 07A.1.074.01 DEG C LCDT APU Bleed temperature |
| LCIT APU1 07A.1.110.01 DEG C APU_LCIT APU Load compressor |
| inlet temperature |
| LGDW LGCIU1 06D.1.021.01 LGCIUDSW2 LGCIU discrete word #2 |
| LGDW LGCIU2 06D.2.021.10 LGCIUDSW2 LGCIU discrete word #2 |
| LOC DMC1 025.1.173.01 DDM LOC1 ILS1 localizer deviation |
| LOC DMC1 025.1.173.10 DDM LOC2 ILS2 localizer deviation |
| LONA SDAC1 029.1.331.01 G LONGACC Longitudinal |
| acceleration |
| LONA SDAC2 029.2.331.01 G LONGACC Longitudinal |
| acceleration |
| LONG IRS1 004.1.331.01 G LONG Body longitudinal |
| acceleration |
| LONGP IRS1 004.1.311.DD DEG LONP.1 Longitude Position |
| LONGP IRS2 004.2.311.DD DEG LONP.2 Longitude Position |
| LONP IRS1 004.1.311.NA DEG LONP_1 Present position |
| longitude system 1 |
| LONP IRS2 004.2.311.NA DEG LONP_2 Present position |
| longitude system 1 |
| LOPP BSCU1 06E.1.331.01 DEG BRAKE_LPA Left brake pedal angle |
| LOPP BSCU2 06E.2.331.10 DEG BRAKE_LPA Left brake pedal angle |
| LPBT EIU1 07B.1.101.XX DEG C LPBT.1 Buffer Air Temp |
| LPBT EIU2 07B.2.101.XX DEG C LPBT.2 Buffer Air Temp |
| LPCSP EIU1 07B.1.257.XX % LPCSP.1 LPC SVA position |
| percent open command |
| LPCSP EIU2 07B.2.257.XX % LPCSP.2 LPC SVA position |
| percent open command |
| LPCSV EIU1 07B.1.260.XX % LPCSV.1 LPC SVA position |
| percent open feedback |
| LPCSV EIU2 07B.2.260.XX % LPCSV.2 LPC SVA position |
| percent open feedback |
| LPCTC EIU1 07B.1.202.XX mA LPCTC.1 LPC SVA Torque motor |
| current |
| LPCTC EIU2 07B.2.202.XX mA LPCTC.2 LPC SVA Torque motor |
| current |
| LPT EIU1 07C.1.040.XX % AOCOC.1 LPT Trim Balance |
| Solution angle |
| LPT EIU2 07C.2.040.XX % AOCOC.2 LPT Trim Balance |
| Solution angle |
| LPTM EIU1 07C.1.324.XX OZ- LPTM.1 LPT Trim Balance |
| INCHES Solution Magnitude |
| LPTM EIU2 07C.2.324.XX OZ- LPTM.2 LPT Trim Balance |
| INCHES Solution Magnitude |
| LTLD EIU1 07B.1.210.XX % LTLD.1 Left Thrust Reverser |
| Transcowl opposite |
| channel LVDT Position |
| LTLD EIU2 07B.2.210.XX % LTLD.2 Left Thrust Reverser |
| Transcowl opposite |
| channel LVDT Position |
| LTRD EIU1 07B.1.142.XX % LTRD.1 Left Thrust Reverser |
| Door local RVDT Position |
| LTRD EIU2 07B.2.142.XX % LTRD.2 Left Thrust Reverser |
| Door local RVDT Position |
| LUD EIU1 07B.1.315.XX DISCRETE LUD.1 LightUp detected |
| LUD EIU2 07B.2.315.XX DISCRETE LUD.2 LightUp detected |
| MCT EIU1 07B.1.134.XX DISCRETE MCT.1 TLA at MCT |
| (33,33 <= TLA <= 36,67) |
| MCT EIU2 07B.2.134.XX DISCRETE MCT.2 TLA at MCT |
| (33,33<=TLA<=36,67) |
| MFDI FDIU1 017.1.350.00 FDIUMW FDIU maintenance word |
| MH IRS1 004.1.320.01 DEG MH Magnetic heading |
| MH IRS2 004.2.320.10 DEG MH Magnetic heading |
| MN ADC1 006.1.205.01 MACH MACH Mach (switched |
| parameter) |
| MN ADC2 006.2.205.10 MACH MACH Mach (switched |
| parameter) |
| MN3 FWC1 026.1.205.11 MACH MACH Mach 3 |
| MN3 FWC2 026.2.205.11 MACH MACH3 Mach 3 |
| MNE EIU1 07B.1.205.XX mm MNE.1 Mach Number from Engine |
| MNE EIU2 07B.2.205.XX mm MNE.2 Mach Number from Engine |
| MSWOF SDAC1 029.1.002.11 APU_MSW_OF_F APU master switch P/B |
| OFF - filtered |
| N1 EIU1 07B.1.331.XX %RPM N1.1 The engine low pressure |
| module speed, N1 Unbiased |
| N1 EIU2 07B.2.331.XX %RPM N1.2 The engine low pressure |
| module speed, N1 Unbiased |
| N1A EIU1 07B.1.346.XX %RPM N1A.1 The engine low pressure |
| module speed, Selected |
| (indicated) N1 actual |
| N1A EIU2 07B.2.346.XX %RPM N1A.2 The engine low pressure |
| module speed, Selected |
| (indicated) N1 actual |
| N1C2 EIU1 07B.1.340.XX % N1C2.1 N1 corrected |
| N1C2 EIU2 07B.2.340.XX % N1C2.2 N1 corrected |
| N1COM EIU1 07B.1.341.XX %RPM N1COM.1 The engine low pressure |
| module speed, N1 command |
| N1COM EIU2 07B.2.341.XX %RPM N1COM.2 The engine low pressure |
| pressure module speed, |
| N1 command |
| N1K DMU N1K_1 N1 corrected left |
| (DMU computed) |
| N1K DMU N1K_2 N1 corrected right |
| (DMU computed) |
| N1LIM EIU1 07B.1.337.XX %RPM N1LIM.1 The engine low pressure |
| module speed, N1 Trust |
| setting Limit for FMGC |
| N1LIM EIU2 07B.2.337.XX %RPM N1LIM.2 The engine low pressure |
| module speed, N1 Trust |
| setting Limit for FMGC |
| N1MAX EIU1 07B.1.342.XX %RPM N1MAX.1 The engine low pressure |
| module speed, N1 Maximum |
| allowed for Flight Deck |
| N1MAX EIU2 07B.2.342.XX %RPM N1MAX.2 The engine low pressure |
| module speed, N1 Maximum |
| allowed for Flight Deck |
| N1MSA %RPM Max N1 Speed Achieved |
| N1P FDIMU %RPM N1PK_1 N1P corrected left |
| (DMU computed) |
| N1P FDIMU %RPM N1PK_2 N1P corrected left |
| (DMU computed) |
| N1RED EIU1 07B.1.120.XX DISCRETE N1RED.1 N1 Redline exceeded |
| N1RED EIU2 07B.2.120.XX DISCRETE N1RED.2 N1 Redline exceeded |
| N1VIB EIU1 07B.1.035.XX DISCRETE N1VIB.1 N1 Vibration Warning |
| N1VIB EIU2 07B.2.035.XX DISCRETE N1VIB.2 N1 Vibration Warning |
| N2A EIU1 07B.1.344.XX %RPM N2A.1 The engine high pressure |
| module speed,Selected |
| (indicated) N2 actual |
| N2A EIU2 07B.2.344.XX %RPM N2A.2 The engine high pressure |
| module speed,Selected |
| (indicated) N2 actual |
| N2C5 EIU1 07B.1.336.XX %RPM N2C5.1 The engine high pressure |
| module speed, N2 |
| corrected for station 2.5 |
| N2C5 EIU2 07B.2.336.XX %RPM N2C5.2 The engine high pressure |
| module speed, N2 |
| corrected for station 2.5 |
| N2K N2K_1 N2 corrected left |
| (DMU computed) |
| N2K N2K_2 N2 corrected right |
| (DMU computed) |
| N2P FDIMU %RPM N2PK_1 N2P corrected left |
| (DMU computed) |
| N2P FDIMU %RPM N2PK_2 N2P corrected right |
| (DMU computed) |
| N2RED EIU1 07B.1.120.XX DISCRETE N2RED.1 N2 Redline exceeded |
| N2RED EIU2 07B.2.120.XX DISCRETE N2RED.2 N2 Redline exceeded |
| N2VIB EIU1 07B.1.035.XX DISCRETE N2VIB.1 N1 Vibration Warning |
| N2VIB EIU2 07B.2.035.XX DISCRETE N2VIB.2 N1 Vibration Warning |
| NA APU1 07A.1.176.01 %RPM APU_RPM APU RPM |
| NAI EIU1 07B.1.105.XX.18 NAI_OP_1 Nacelle anti-ice |
| engine #1 open |
| NAI EIU2 07B.2.105.XX.18 NAI_OP_2 Nacelle anti-ice |
| engine #2 open |
| NAIDP EIU1 07B.1.107.XX PSI NAIDP.1 NAI DwnSTR Valve Pres |
| NAIDP EIU2 07B.2.107.XX PSI NAIDP.2 NAI DwnSTR Valve Pres |
| NAIT EIU1 07B.1.220.XX DEG C NAIT.1 NAI Temperature |
| NAIT EIU2 07B.2.220.XX DEG C NAIT.2 NAI Temperature |
| NAIUP EIU1 07B.1.106.XX PSI NAIUP.1 NAI UpStr Valve Pres |
| NAIUP EIU2 07B.2.106.XX PSI NAIUP.2 NAI UpStr Valve Pres |
| NAIV EIU1 07B.1.105.XX DISCRETE NAI.1 Nacelle Anti Ice Closed |
| NAIV EIU2 07B.2.105.XX DISCRETE NAI.2 Nacelle Anti Ice Closed |
| NEDET EIU1 07B.1.072.XX Ferrous NEDET.1 Cumulative number of |
| Particles nonferrous particles |
| detected |
| NEDET EIU2 07B.2.072.XX Ferrous NEDET.2 Cumulative number of |
| Particles nonferrous particles |
| detected |
| NF EIU1 07B.1.326.XX % NF.1 Fan speed |
| NF EIU2 07B.2.326.XX % NF.2 Fan speed |
| NOLS EIU1 07B.1.276.XX DISCRETE NOLS.1 No Light during start |
| detected |
| NOLS EIU2 07B.2.276.XX DISCRETE NOLS.2 No Light during start |
| detected |
| NPA %RPM APU_RPM_PEAK APU RPM at APU EGT peak |
| during APU start |
| NRA BSCU1 06E.1.334.01 DEG NWSANG NWS angle |
| NRA BSCU2 06E.2.334.10 DEG NWSANG NWS angle |
| NSA EIU1 07B.1.307.XX % NSA.1 Starter turbine Airspeed |
| NSA EIU2 07B.2.307.XX % NSA.2 Starter turbine Airspeed |
| NSVC BSCU1 06E.1.335.01 MA NSVC Curent servo valve NWS |
| NSVC BSCU2 06E.2.335.10 MA NSVC Curent servo valve NWS |
| NWSA BSCU1 06E.1.334.01 DEG NWSANG NWS angle |
| NWSA BSCU2 06E.2.334.10 DEG NWSANG NWS angle |
| OAT EIU1 07B.1.367.XX DEG OAT.1 Outside Air temperature |
| OAT EIU2 07B.2.367.XX DEG OAT.2 Outside Air temperature |
| ODL EIU1 07B.1.124.XX DISCRETE ODL.1 Oil Debris above limit |
| ODL EIU2 07B.2.124.XX DISCRETE ODL.2 Oil Debris above limit |
| ODM0F EIU1 07B.1.041.XX Ferrous ODM0F.1 ODM BIN 0 Ferrous Counts |
| Particles |
| ODM0F EIU2 07B.2.041.XX Ferrous ODM0F.2 ODM BIN 0 Ferrous Counts |
| Particles |
| ODM1F EIU1 07B.1.042.XX Ferrous ODM1F.1 ODM BIN 1 Ferrous Counts |
| Particles |
| ODM1F EIU2 07B.2.042.XX Ferrous ODM1F.2 ODM BIN 1 Ferrous Counts |
| Particles |
| ODM2F EIU1 07B.1.043.XX Ferrous ODM2F.1 ODM BIN 2 Ferrous Counts |
| Particles |
| ODM2F EIU2 07B.2.043.XX Ferrous ODM2F.2 ODM BIN 2 Ferrous Counts |
| Particles |
| ODM3F EIU1 07B.1.044.XX Ferrous ODM3F.1 ODM BIN 3 Ferrous Counts |
| Particles |
| ODM3F EIU2 07B.2.044.XX Ferrous ODM3F.2 ODM BIN 3 Ferrous Counts |
| Particles |
| ODM4F EIU1 07B.1.045.XX Ferrous ODM4F.1 ODM BIN 4 Ferrous Counts |
| Particles |
| ODM4F EIU2 07B.2.045.XX Ferrous ODM4F.2 ODM BIN 4 Ferrous Counts |
| Particles |
| ODM5F EIU1 07B.1.050.XX Ferrous ODM5F.1 ODM BIN 5 Ferrous Counts |
| Particles |
| ODM5F EIU2 07B.2.050.XX Ferrous ODM5F.2 ODM BIN 5 Ferrous Counts |
| Particles |
| ODM6F EIU1 07B.1.051.XX Ferrous ODM6F.1 ODM BIN 6 Ferrous Counts |
| Particles |
| ODM6F EIU2 07B.2.051.XX Ferrous ODM6F.2 ODM BIN 6 Ferrous Counts |
| Particles |
| ODM7F EIU1 07B.1.052.XX Ferrous ODM7F.1 ODM BIN 7 Ferrous Counts |
| Particles |
| ODM7F EIU2 07B.2.052.XX Ferrous ODM7F.2 ODM BIN 7 Ferrous Counts |
| Particles |
| ODP EIU1 07B.1.312.XX PSIG ODP.1 Engine Oil Filter delta |
| pressure |
| ODP EIU2 07B.2.312.XX PSIG ODP.2 Engine Oil Filter delta |
| pressure |
| OIF SDAC1 029.1.001.01 OIL_FT_CL_1 OIL filter clogged |
| engine #1 |
| OIF SDAC2 029.2.001.10 OIL_FT_CL_2 OIL filter clogged |
| engine #2 |
| OILLO EIU1 07B.1.157.XX DISCRETE OILLO.1 Oil Level below Limit |
| OILLO EIU2 07B.2.157.XX DISCRETE OILLO.2 Oil Level below Limit |
| OIP EIU1 07B.1.317.XX PSID OIP.1 Engine Oil Pressure |
| OIP EIU2 07B.2.317.XX PSID OIP.2 Engine Oil Pressure |
| OIQ EIU 07B.1.073.XX QTS OIQ.1 Engine Oil Quantity |
| OIQ EIU 07B.2.073.XX QTS OIQ.2 Engine Oil Quantity |
| OIQH OIQH_1 OIL consumption from |
| the previous flight |
| engine |1 |
| OIQH OIQH_2 OIL consumption from |
| the previous flight |
| engine |2 |
| OIT EIU1 07B.1.316.XX DEG C OIT.1 Engine Oil Temperature |
| OIT EIU2 07B.2.316.XX DEG C OIT.2 Engine Oil Temperature |
| OPLOW EIU1 07B.1.273.XX DISCRETE OPLOW.1 Oil Pressure below Low |
| limit |
| OPLOW EIU2 07B.2.273.XX DISCRETE OPLOW.2 Oil Pressure below Low |
| limit |
| OPRED EIU1 07B.1.120.XX DISCRETE OPRED.1 Oil Pressure below Red |
| limit |
| OPRED EIU2 07B.2.120.XX DISCRETE OPRED.2 Oil Pressure below Red |
| limit |
| OPS1 OPS1_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC1 bus) |
| OPS1 OPS1_SN_P2 |
| OPS1 OPS1_SN_P3 |
| OPS2 OPS2_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC2 bus) |
| OPS2 OPS2_SN_P2 |
| OPS2 OPS2_SN_P3 |
| OPS3 OPS3_SN_P1 ADIRU Operational |
| Software P/N (DMU |
| computed from data on |
| ADC3 bus) |
| OPS3 OPS3_SN_P2 |
| OPS3 OPS3_SN_P3 |
| OTA APU1 07A.1.247.01 DEG C OTA APU Oil sum temperature |
| OTRED EIU1 07B.1.333.XX DISCRETE OTRED.1 Oil Temperature Red |
| Limit exceeded |
| OTRED EIU2 07B.2.333.XX DISCRETE OTRED.2 Oil Temperature Red |
| Limit exceeded |
| OVP PRESS1 05C.1.153.01 % OVP1 Outflow valve position |
| OVP PRESS2 05C.2.153.10 % OVP2 Outflow valve position |
| P2 EIU1 07B.1.242.XX PSI P2.1 Selected total air |
| pressure from the gas |
| path (Station 2) for |
| control laws |
| P2 EIU2 07B.2.242.XX PSI P2.2 Selected total air |
| pressure from the gas |
| path (Station 2) for |
| control laws |
| P25 EIU1 07B.1.262.XX PSIA P25.1 The total air pressure |
| from the engine gas |
| path (Station 2.5) |
| P25 EIU2 07B.2.262.XX PSIA P25.2 The total air pressure |
| from the engine gas |
| path (Station 2.5) |
| P2A APU1 07A.1.112.01 BAR P2A APU inlet pressure |
| P2E EIU1 07B.1.131.XX PSI P2E.1 Selected Inlet Total |
| Pressure |
| P2E EIU2 07B.2.131.XX PSI P2E.2 Selected Inlet Total |
| Pressure |
| P5 EIU1 07B.1.132.XX PSIA P5.1 Selected Engine sensed |
| turbine exhaust total |
| pressure |
| P5 EIU2 07B.2.132.XX PSIA P5.2 Selected Engine sensed |
| turbine exhaust total |
| pressure |
| PAMB EIU1 07B.1.114.XX PSIA PAMB.1 The Ambient Air Pressure |
| from the engine (under |
| nacelle fan cowl) |
| PAMB EIU2 07B.2.114.XX PSIA PAMB.2 The Ambient Air Pressure |
| from the engine (under |
| nacelle fan cowl) |
| PB EIU1 07B.1.264.XX PSIA PB.1 The Selected Burner |
| Pressure from the engine |
| gas path |
| PB EIU2 07B.2.264.XX PSIA PB.2 The Selected Burner |
| Pressure from the engine |
| gas path |
| PBV PC/ACSC1 08E.1.112.11 % PBV_1 Pack bypass valve |
| position system #1 |
| PBV PC/ACSC2 08E.2.112.00 % PBV_2 Pack bypass valve |
| position system #2 |
| PCSW PRESS1 05C.1.057.01 PCSW Press control bus: |
| Status + Fault info |
| PCSW PRESS2 05C.2.057.10 PCSW Press control bus: |
| Status + Fault info |
| PD BMC1 06F.1.143.01 PSI PD_1 Precooler inlet pressure |
| PD BMC2 06F.2.143.10 PSI PD_1 Precooler inlet pressure |
| PD BMC1 06F.1.142.01 PSI PD_2 Precooler inlet pressure |
| PD BMC2 06F.2.142.10 PSI PD_2 Precooler inlet pressure |
| PDC PRESS1 05C.1.144.01 PSI PDC Cabin differential |
| pressure |
| PDC PRESS2 05C.2.144.10 PSI PDC Cabin differential |
| pressure |
| PF PC/ACSC1 08E.1.126.11 KG/S PF_1 Pack flow system #1 |
| PF PC/ACSC2 08E.2.126.00 KG/S PF_2 Pack flow system #2 |
| PFAD APU1 07A.1.004.01 PFAD APU: Performance |
| adjustments |
| PH FDIMU FLIMOD_DISP Flight phase to |
| display (DMU computed) |
| PHM EIU1 07B.1.224.XX PHM.1 Phase unbalance from |
| PHMU |
| PHM EIU2 07B.2.224.XX PHM.2 Phase unbalance from |
| PHMU |
| PS14 EIU1 07B.1.116.XX PSIA PS14.1 FEGV (Fan Exit Guide |
| Vane) static pressure |
| PS14 EIU2 07B.2.116.XX PSIA PS14.2 FEGV (Fan Exit Guide |
| Vane) static pressure |
| PSW1 PC/ACSC1 08E.1.062.11 PC062DW_1 Discrete data word |
| (Label 062) of pack |
| PSW1 PC/ACSC2 08E.2.062.00 PC062DW_0 Discrete data word |
| (Label 062) of pack |
| PT APU1 07A.1.166.01 BAR PT Bleed air pressure |
| PTCH IRS1 004.1.324.01 DEG PITCH Pitch Angle |
| PTCH IRS2 004.2.324.10 DEG PITCH Pitch Angle |
| PTCR IRS1 004.1.326.01 DEG/S PTCR Body axis pitch rate |
| PTCR IRS2 004.2.326.01 DEG/S PTCR Body axis pitch rate |
| PTMC EIU1 07B.1.111.XX mA PTMC.1 Protection Torque Motor |
| Current |
| PTMC EIU2 07B.2.111.XX mA PTMC.2 Protection Torque Motor |
| Current |
| RALT DMC1 025.1.164.01 FEET RALT1 Radio Altitude |
| RALT DMC1 025.1.164.10 FEET RALT1 Radio Altitude |
| RALT DMC2 025.2.164.01 FEET RALT2 Radio Altitude |
| RALT DMC2 025.2.164.10 FEET RALT2 Radio Altitude |
| REVL EIU1 07B.1.127.XX % REVL.1 Left T/R cowl percent |
| deployed position |
| REVL EIU2 07B.2.127.XX % REVL.2 Left T/R cowl percent |
| deployed position |
| REVR EIU1 07B.1.126.XX % REVL.1 Right T/R cowl percent |
| deployed position |
| REVR EIU2 07B.2.126.XX % REVL.2 Right T/R cowl percent |
| deployed position |
| RFAN EIU1 07B.1.176.XX % RFAN.1 Rear Vibe Sensor FAN S01 |
| RFAN EIU2 07B.2.176.XX % RFAN.2 Rear Vibe Sensor FAN S01 |
| RI PC/ACSC1 08E.1.130.11 % RI_1 Pack ram inlet position |
| LH |
| RI PC/ACSC2 08E.2.130.00 % RI_2 Pack ram inlet position |
| RLH |
| RO PC/ACSC1 08E.1.124.11 % RO_1 Pack ram inlet position |
| LH |
| RO PC/ACSC2 08E.2.124.00 % RO_2 Pack ram inlet position |
| RLH |
| ROLL IRS1 004.1.325.01 DEG ROLL.1 ROLL angle |
| ROLL IRS2 004.2.325.10 DEG ROLL.2 ROLL angle |
| ROLR IRS1 004.1.327.01 DEG ROLR Body axis roll rate |
| ROLR IRS2 004.2.327.10 DEG ROLR Body axis roll rate |
| ROPP BSCU1 06E.1.330.01 DEG BRAKE_RPA Right brake pedal angle |
| ROPP BSCU2 06E.2.330.10 DEG BRAKE_RPA Right brake pedal angle |
| RSCC BSCU1 06E.1.332.01 KTS REFSPDCC Reference speed command |
| channel |
| RSCC BSCU2 06E.2.332.10 KTS REFSPDCC Reference speed command |
| channel |
| RSP2 FCDC1 06C.1.362.01 DEG RSP2_1 LH spoiler #2 Position |
| RSP2 FCDC2 06C.2.362.10 DEG RSP2_1 LH spoiler #2 Position |
| RSP2 FCDC1 06C.1.372.01 DEG RSP2_2 RH spoiler #2 Position |
| RSP2 FCDC2 06C.2.372.10 DEG RSP2_2 RH spoiler #2 Position |
| RSP3 FCDC1 06C.1.363.01 DEG RSP3_1 LH spoiler #3 Position |
| RSP3 FCDC2 06C.2.363.10 DEG RSP3_1 LH spoiler #3 Position |
| RSP3 FCDC1 06C.1.373.01 DEG RSP3_2 RH spoiler #3 Position |
| RSP3 FCDC2 06C.2.373.10 DEG RSP3_2 RH spoiler #3 Position |
| RSP4 FCDC1 06C.1.364.01 DEG RSP4_1 LH spoiler #4 Position |
| RSP4 FCDC2 06C.2.364.10 DEG RSP4_1 LH spoiler #4 Position |
| RSP4 FCDC1 06C.1.374.01 DEG RSP4_2 LH spoiler #4 Position |
| RSP4 FCDC2 06C.2.374.10 DEG RSP4_2 LH spoiler #4 Position |
| RSP5 FCDC1 06C.1.365.01 DEG RSP5_1 LH spoiler #5 Position |
| RSP5 FCDC2 06C.2.365.10 DEG RSP5_1 LH spoiler #5 Position |
| RSP5 FCDC1 06C.1.375.01 DEG RSP5_2 LH spoiler #5 Position |
| RSP5 FCDC2 06C.2.375.10 DEG RSP5_2 LH spoiler #5 Position |
| RTRC EIU1 07B.1.123.XX % RTRC.1 Right Thrust Reverser |
| Door opposite channel |
| RVDT Position |
| RTRC EIU2 07B.2.123.XX % RTRC.2 Right Thrust Reverser |
| Door opposite channel |
| RVDT Position |
| RTRD EIU1 07B.1.204.XX % RTRD.1 Right Thrust Reverser |
| Door local RVDT Position |
| RTRD EIU2 07B.2.204.XX % RTRD.2 Right Thrust Reverser |
| Door local RVDT Position |
| RUDD SDAC1 029.1.312.00 DEG RUDD.1 Rudder position |
| RUDD SDAC2 029.2.312.00 DEG RUDD.2 Rudder position |
| RUDT FAC1 00A.1.313.00 DEG RUDT.1 Rudder Trim Position |
| RUDT FAC2 00A.2.313.00 DEG RUDT.2 Rudder Trim Position |
| RVN1 EIU1 07B.1.174.XX % RVN1.1 Rear Vibe Sensor N1 SO1 |
| RVN1 EIU2 07B.2.174.XX % RVN1.2 Rear Vibe Sensor N1 SO1 |
| RVN2 EIU1 07B.1.175.XX % RVN2.1 Rear Vibe Sensor N2 SO1 |
| RVN2 EIU2 07B.2.175.XX % RVN2.2 Rear Vibe Sensor N2 SO1 |
| SAT ADC1 06B.1.213.01 DEG C SAT.1 Static air temperature |
| (BNR) |
| SAT ADC2 06B.2.213.10 DEG C SAT.2 Static air temperature |
| (BNR) |
| SAVO EIU1 07B.1.270.XX DISCRETE SAVO.1 Starter Air Valve |
| Solenoid Commanded Open |
| SAVO EIU2 07B.2.270.XX DISCRETE SAVO.2 Starter Air Valve |
| Solenoid Commanded Open |
| SAVRQ EIU1 07B.1.271.XX DISCRETE SAVRQ.1 Starter Air Valve |
| Solenoid Commanded On |
| SAVRQ EIU2 07B.2.271.XX DISCRETE SAVRQ.2 Starter Air Valve |
| Solenoid Commanded On |
| SC1 SDAC1 029.1.242.01 DEG C/F SC1 Sel aft cab comp temp |
| SC1 SDAC2 029.2.242.01 DEG C/F SC1 Sel aft cab comp temp |
| SC2 SDAC1 029.1.244.01 DEG C/F SC2 Sel aft cab comp temp |
| SC2 SDAC2 029.2.244.01 DEG C/F SC2 Sel aft cab comp temp |
| SC3 SDAC1 029.1.245.01 DEG C/F SC3 Sel aft cab comp temp |
| SC3 SDAC2 029.2.245.01 DEG C/F SC3 Sel aft cab comp temp |
| SCC BSCU1 06E.1.340.01 DEG STEERCC Sterring command captain |
| SCC BSCU2 06E.2.340.10 DEG STEERCC Sterring command captain |
| SCFD BSCU1 06E.1.341.01 DEG STEERCFO Sterring command F/O |
| SCFD BSCU2 06E.2.341.10 DEG STEERCFO Sterring command F/O |
| SCV APU1 07A.1.134.01 DEG SCV Surge Control Valve |
| Position |
| SDAUT APU1 07A.1.037.01 APU_SD_AUT_F APU automatic shut |
| down - filtered |
| SDEXT APU1 07A.1.037.01 APU_SD_EXT_F Emergency (external) |
| S/D - filtered |
| STRON APU1 07A.1.037.01 APU_STR_ON_F APU start in progress |
| - filtered |
| SDS1 SDAC1 029.1.001.01 SDACSDS1 SDAC discrete status |
| word #1 |
| SDS1 SDAC2 029.2.001.10 SDACSDS2 SDAC discrete status |
| word #2 |
| SDS2 SDAC1 029.1.001.10 SDACSDS2 SDAC discrete status |
| word #2 |
| SDS2 SDAC2 029.2.001.10 SDACSDS2 SDAC discrete status |
| word #2 |
| SHPTP EIU1 07B.1.153.XX PSIA/SEC SHPTP.1 Synthesized HPT Pressure |
| SHPTP EIU2 07B.2.153.XX PSIA/SEC SHPTP.2 Synthesized HPT Pressure |
| SIP EIU1 07B.1.315.XX DISCRETE SIP.1 Start In Progress |
| SIP EIU2 07B.2.315.XX DISCRETE SIP.2 Start In Progress |
| SLAT SFCC1 00B.1.127.01 DEG SLAT_1 SLAT actual position |
| system #1 |
| SLAT SFCC2 00B.2.127.10 DEG SLAT_2 SLAT actual position |
| system #2 |
| SLP FAC1 00A.1.226.00 DEG SLP_1 Estimd sideslip |
| (side slip angle) |
| syst.#1 |
| SLP FAC2 00A.2.226.00 DEG SLP_2 Estimd sideslip |
| (side slip angle) |
| syst.#2 |
| SLPTP EIU1 07B.1.154.XX PSIA/SEC SLPTP.1 Synthesized LPT Presure |
| SLPTP EIU2 07B.2.154.XX PSIA/SEC SLPTP.2 Synthesized LPT Presure |
| STA SEC STA APU start time |
| STAB FCDC1 06C.1.315.01 DEG STAB.1 Stabilizer position #1 |
| STAB FCDC2 06C.2.315.01 DEG STAB.2 Stabilizer position #2 |
| STALL EIU1 07B.1.145.XX DISCRETE STALL.1 Engine surge (Stall) |
| detected |
| STALL EIU2 07B.2.145.XX DISCRETE STALL.2 Engine surge (Stall) |
| detected |
| STVC FWC1 026.1.032.01 SV_STV_CL_1 Scavenge valve stuck |
| closed engine #1 |
| STVC FWC2 026.2.032.01 SV_STV_CL_1 Scavenge valve stuck |
| closed engine #1 |
| STVC FWC1 026.1.032.10 SV_STV_CL_2 Scavenge valve stuck |
| closed engine #2 |
| STVC FWC2 026.2.032.10 SV_STV_CL_2 Scavenge valve stuck |
| closed engine #2 |
| STVO FWC1 026.1.032.10 SV_STV_OP_1 Scavenge valve stuck |
| closed engine #1 |
| STVO FWC2 026.2.032.10 SV_STV_OP_1 Scavenge valve stuck |
| closed engine #1 |
| STVO FWC1 026.1.032.10 SV_STV_OP_2 Scavenge valve stuck |
| closed engine #2 |
| STVO FWC2 026.2.032.10 SV_STV_OP_2 Scavenge valve stuck |
| closed engine #2 |
| STW01 EIU1 07B.1.270.XX DISCRETE EEC ARINC WORD #15 |
| STW01 EIU2 07B.2.270.XX DISCRETE EEC ARINC WORD #15 |
| STW02 EIU1 07B.1.271.XX DISCRETE EEC ARINC WORD #16 |
| STW02 EIU2 07B.2.271.XX DISCRETE EEC ARINC WORD #16 |
| STW03 EIU1 07B.1.272.XX DISCRETE EEC ARINC WORD #17 |
| STW03 EIU2 07B.2.272.XX DISCRETE EEC ARINC WORD #17 |
| STW04 EIU1 07B.1.273.XX DISCRETE EEC ARINC WORD #18 |
| STW04 EIU2 07B.2.273.XX DISCRETE EEC ARINC WORD #18 |
| STW05 EIU1 07B.1.274.XX DISCRETE EEC ARINC WORD #19 |
| STW05 EIU2 07B.2.274.XX DISCRETE EEC ARINC WORD #19 |
| STW06 EIU1 07B.1.275.XX DISCRETE EEC ARINC WORD #20 |
| STW06 EIU2 07B.2.275.XX DISCRETE EEC ARINC WORD #20 |
| STW07 EIU1 07B.1.276.XX DISCRETE EEC ARINC WORD #21 |
| STW07 EIU2 07B.2.276.XX DISCRETE EEC ARINC WORD #21 |
| STW08 EIU1 07B.1.145.XX DISCRETE EEC ARINC WORD #08 |
| STW08 EIU2 07B.2.145.XX DISCRETE EEC ARINC WORD #08 |
| STW09 EIU1 07B.1.146.XX DISCRETE EEC ARINC WORD #09 |
| STW09 EIU2 07B.2.146.XX DISCRETE EEC ARINC WORD #09 |
| STW10 EIU1 07B.1.066.XX DISCRETE EEC ARINC WORD #02 |
| STW10 EIU2 07B.2.066.XX DISCRETE EEC ARINC WORD #02 |
| STW11 EIU1 07B.1.147.XX DISCRETE EEC ARINC WORD #10 |
| STW11 EIU2 07B.2.147.XX DISCRETE EEC ARINC WORD #10 |
| STW12 EIU1 07B.1.277.XX DISCRETE EEC ARINC WORD #22 |
| STW12 EIU2 07B.2.277.XX DISCRETE EEC ARINC WORD #22 |
| STW13 EIU1 07B.1.037.XX DISCRETE EEC ARINC WORD #29 |
| STW13 EIU2 07B.2.037.XX DISCRETE EEC ARINC WORD #29 |
| STW14 EIU1 07B.1.105.XX DISCRETE EEC ARINC WORD #03 |
| STW14 EIU2 07B.2.105.XX DISCRETE EEC ARINC WORD #03 |
| STW15 EIU1 07B.1.110.XX DISCRETE EEC ARINC WORD #39 |
| STW15 EIU2 07B.2.110.XX DISCRETE EEC ARINC WORD #39 |
| STW16 EIU1 07B.1.120.XX DISCRETE EEC ARINC WORD #04 |
| STW16 EIU2 07B.2.120.XX DISCRETE EEC ARINC WORD #04 |
| STW17 EIU1 07B.1.124.XX DISCRETE EEC ARINC WORD #05 |
| STW17 EIU2 07B.2.124.XX DISCRETE EEC ARINC WORD #05 |
| STW18 EIU1 07B.1.155.XX DISCRETE EEC ARINC WORD #11 |
| STW18 EIU2 07B.2.155.XX DISCRETE EEC ARINC WORD #11 |
| STW19 EIU1 07B.1.156.XX DISCRETE EEC ARINC WORD #12 |
| STW19 EIU2 07B.2.156.XX DISCRETE EEC ARINC WORD #12 |
| STW22 EIU1 07B.1.170.XX DISCRETE EEC ARINC WORD #41 |
| STW22 EIU2 07B.2.170.XX DISCRETE EEC ARINC WORD #41 |
| STW23 EIU1 07B.1.215.XX DISCRETE EEC ARINC WORD #14 |
| STW23 EIU2 07B.2.215.XX DISCRETE EEC ARINC WORD #14 |
| STW24 EIU1 07B.1.216.XX DISCRETE EEC ARINC WORD #42 |
| STW24 EIU2 07B.2.216.XX DISCRETE EEC ARINC WORD #42 |
| STW25 EIU1 07B.1.217.XX DISCRETE EEC ARINC WORD #46 |
| STW25 EIU2 07B.2.217.XX DISCRETE EEC ARINC WORD #46 |
| STW26 EIU1 07B.2.225.XX DISCRETE EEC ARINC WORD #44 |
| STW26 EIU2 07B.1.225.XX DISCRETE EEC ARINC WORD #44 |
| STW27 EIU1 07B.2.315.XX DISCRETE EEC ARINC WORD #23 |
| STW27 EIU2 07B.1.315.XX DISCRETE EEC ARINC WORD #23 |
| STW28 EIU1 07B.2.333.XX DISCRETE EEC ARINC WORD #24 |
| STW28 EIU2 07B.1.333.XX DISCRETE EEC ARINC WORD #24 |
| STW29 EIU1 07B.2.053.XX DISCRETE EEC ARINC WORD #25 |
| STW29 EIU2 07B.1.053.XX DISCRETE EEC ARINC WORD #25 |
| STW30 EIU1 07B.2.117.XX DISCRETE EEC ARINC WORD #26 |
| STW30 EIU2 07B.2.117.XX DISCRETE EEC ARINC WORD #26 |
| STW31 EIU1 07B.1.241.XX DISCRETE EEC ARINC WORD #27 |
| STW31 EIU2 07B.2.241.XX DISCRETE EEC ARINC WORD #27 |
| STW32 EIU1 07B.1.366.XX DISCRETE EEC ARINC WORD #28 |
| STW32 EIU2 07B.2.366.XX DISCRETE EEC ARINC WORD #28 |
| STW33 EIU1 07B.1.362.XX DISCRETE EEC ARINC WORD #34 |
| STW33 EIU2 07B.2.362.XX DISCRETE EEC ARINC WORD #34 |
| STW34 EIU1 07B.1.035.XX DISCRETE EEC ARINC WORD #01 |
| STW34 EIU2 07B.2.035.XX DISCRETE EEC ARINC WORD #01 |
| STW35 EIU1 07B.1.134.XX DISCRETE EEC ARINC WORD #06 |
| STW35 EIU2 07B.2.134.XX DISCRETE EEC ARINC WORD #06 |
| STW36 EIU1 07B.1.144.XX DISCRETE EEC ARINC WORD #07 |
| STW36 EIU2 07B.2.144.XX DISCRETE EEC ARINC WORD #07 |
| STW37 EIU1 07B.2.157.XX DISCRETE EEC ARINC WORD #30 |
| (FOR EHM) |
| STW37 EIU2 07B.2.157.XX DISCRETE EEC ARINC WORD #30 |
| (FOR EHM) |
| STW39 EIU1 07B.2.355.XX DISCRETE EEC ARINC WORD #32 |
| PROVISION |
| STW39 EIU2 07B.2.355.XX DISCRETE EEC ARINC WORD #32 |
| PROVISION |
| STW40 EIU1 07B.2.361.XX DISCRETE EEC ARINC WORD #33 |
| PROVISION |
| STW40 EIU2 07B.2.361.XX DISCRETE EEC ARINC WORD #33 |
| PROVISION |
| STW41 EIU1 07B.2.363.XX DISCRETE EEC ARINC WORD #35 |
| PROVISION |
| STW41 EIU2 07B.2.363.XX DISCRETE EEC ARINC WORD #35 |
| PROVISION |
| STW42 EIU1 07B.2.364.XX DISCRETE EEC ARINC WORD #36 |
| PROVISION |
| STW42 EIU2 07B.2.364.XX DISCRETE EEC ARINC WORD #36 |
| PROVISION |
| STW43 EIU1 07B.2.365.XX DISCRETE EEC ARINC WORD #37 |
| PROVISION |
| STW43 EIU2 07B.2.365.XX DISCRETE EEC ARINC WORD #37 |
| PROVISION |
| STW44 EIU1 07B.2.375.XX DISCRETE EEC ARINC WORD #38 |
| PROVISION |
| STW44 EIU2 07B.2.375.XX DISCRETE EEC ARINC WORD #38 |
| PROVISION |
| SVA EIU1 07B.1.325.XX % SVA.1 The engine Starter |
| Vane actuator feedback |
| SVA EIU2 07B.2.325.XX % SVA.2 The engine Starter |
| Vane actuator feedback |
| T14 EIU1 07B.1.327.XX DEG C T14.1 Synthesized air flow |
| at station 14 |
| T14 EIU2 07B.2.327.XX DEG C T14.2 Synthesized air flow |
| at station 14 |
| T2 EIU1 07B.1.130.XX DEG C T2.1 Local corrected sensed |
| engine inlet total |
| temperature |
| T2 EIU2 07B.2.130.XX DEG C T2.2 Local corrected sensed |
| engine inlet total |
| temperature |
| T25 EIU1 07B.1.263.XX DEG C T25.1 Total air temperature |
| from engine gas path |
| (Station 2.5) |
| T25 EIU2 07B.2.263.XX DEG C T25.2 Total air temperature |
| from engine gas path |
| (Station 2.5) |
| T3 EIU1 07B.1.265.XX DEG C T3.1 Engine Selected T3 |
| temperature |
| T3 EIU2 07B.2.265.XX DEG C T3.2 Engine Selected T3 |
| temperature |
| TAIL1 ACTAIL1 A/C ident word #1 |
| (DMU computed) |
| TAIL2 ACTAIL2 A/C ident word #2 |
| (DMU computed) |
| TAT ADC1 006.1.211.01 DEG C TAT_1 Total air temperature |
| (BNR)(switched |
| parameter) |
| TAT ADC2 006.2.211.10 DEG C TAT_2 Total air temperature |
| (BNR)(switched |
| parameter) |
| TCC EIU1 07B.1.330.XX % TCC.1 Engine Turbine Gas |
| cooling valve feedback |
| TCC EIU2 07B.2.330.XX % TCC.2 Engine Turbine Gas |
| cooling valve feedback |
| TCCOC EIU1 07B.1.305.XX % TCCOC.1 Turbine clearance control |
| valve percent open |
| command |
| TCCOC EIU2 07B.2.305.XX % TCCOC.2 Turbine clearance control |
| valve percent open |
| command |
| TEC EIU1 07B.1.313.XX DEG C TEC.1 Electronic Engine |
| Control Box (EEC) |
| internal temperature |
| TEC EIU2 07B.2.313.XX DEG C TEC.2 Electronic Engine |
| Control Box (EEC) |
| internal temperature |
| TFUEL EIU1 07B.1.115.XX DEG C TFUEL.1 Fuel temperature from |
| engine |
| TFUEL EIU2 07B.2.115.XX DEG C TFUEL.2 Fuel temperature from |
| engine |
| THDG IRS1 004.1.044.01 DEG THDG_1 TRUE HEADING system #1 |
| THDG IRS2 004.2.044.10 DEG THDG_2 TRUE HEADING system #2 |
| TLA EIU1 07B.1.133.XX DEG TLA.1 Thrust Lever Angle |
| Position feedback from |
| the engine EEC |
| TLA EIU2 07B.2.133.XX DEG TLA.2 Thrust Lever Angle |
| Position feedback from |
| the engine EEC |
| TLAR EIU1 07B.1.134.XX DISCRETE TLAR.1 TLA in Reverse |
| TLAR EIU2 07B.2.134.XX DISCRETE TLAR.2 TLA in Reverse |
| TN EIU1 07B.1.322.XX DEG C TN.1 Nacelle Temperature |
| (Engine cre compartment) |
| TN EIU2 07B.2.322.XX DEG C TN.2 Nacelle Temperature |
| (Engine cre compartment) |
| TNR DEG DTNREF_5 Delta TN reference value |
| in climb |
| TNR DEG DTNREF_6 Delta TN reference value |
| in climb |
| TO DESTINATION Destination |
| (DMU computed) |
| TP PC/ACSC1 08E.1.121.11 DEG C TP.1 Pack outlet temperature |
| LH |
| TP PC/ACSC2 08E.2.121.00 DEG C TP.2 Pack outlet temperature |
| LH |
| TPO BMC1 06F.1.141.01 DEG C TPO_1 Precooler eng #1 outlet |
| temperature |
| TPO BMC2 06F.2.141.10 DEG C TPO_1 Precooler eng #1 outlet |
| temperature |
| TPO BMC1 06F.1.140.01 DEG C TPO_2 Precooler eng #2 outlet |
| temperature |
| TPO BMC2 06F.2.140.10 DEG C TPO_2 Precooler eng #2 outlet |
| temperature |
| TRL EIU1 07B.1.275.XX DISCRETE TRL.1 T/R Lockout Switch |
| activated |
| TRL EIU2 07B.2.275.XX DISCRETE TRL.2 T/R Lockout Switch |
| activated |
| TRS EIU1 07B.1.146.XX % TRS.1 T/R Stowed |
| TRS EIU2 07B.2.146.XX % TRS.2 T/R Stowed |
| TR EIU1 07B.1.137.XX % TR.1 Selected thrust reverser |
| percent deployed |
| TR EIU2 07B.2.137.XX % TR.2 Selected thrust reverser |
| percent deployed |
| TRF EIU1 07B.1.146.XX DISCRETE TRF.1 Thrust Reverser Fully |
| deployed |
| TRF EIU2 07B.2.146.XX DISCRETE TRF.2 Thrust Reverser Fully |
| deployed |
| TRFA EIU1 07B.1.120.XX DISCRETE TRFA.1 T/R Failed |
| TRFA EIU2 07B.2.120.XX DISCRETE TRFA.2 T/R Failed |
| TW PC/ACSC1 08E.1.111.11 DEG C TW_1 Pack water extr. |
| temperature LH |
| TW PC/ACSC2 08E.2.111.00 DEG C TW_2 Pack water extr. |
| temperature RLH |
| UTC FDIU1 017.1.150.00 UTC UTC (Universal time |
| coordinated BNR) |
| V3 FAC1 00A.1.263.00 KTS V3 V3 (min. speed flaps |
| retr.) |
| V3 FAC2 00A.2.263.00 KTS V3 V3 (min. speed flaps |
| retr.) |
| V4 FAC1 00A.1.264.00 KTS V4 V4 (min. speed flaps |
| retr.) |
| V4 FAC2 00A.2.264.00 KTS V4 V4 (min. speed flaps |
| retr.) |
| VA ZC/ACSC2 05D.2.220.10 % VA CAB temp reg vlv group 3 |
| VACC IRS1 004.1.364.01 G VACC Vertical acceleration |
| VACC IRS2 004.2.364.10 G VACC Vertical acceleration |
| VB EIU1 07B.1.135.XX CU VB1.1 N1 vibration |
| VB EIU2 07B.2.135.XX CU VB1.2 N1 vibration |
| VB2 EIU1 07B.1.136.XX CU VB2.1 N2 vibration |
| VB2 EIU2 07B.2.136.XX CU VB2.2 N2 vibration |
| VF ZC/ACSC2 05D.2.206.10 % VF CAB temp reg vlv group 1 |
| VLS FAC1 00A.1.245.00 KTS VLS VLS (min airspeed) |
| VLS FAC2 00A.2.245.00 KTS VLS VLS (min airspeed) |
| VMAN FAC1 00A.1.265.00 KTS VMAN V MAN (maneuvering speed) |
| VMAN FAC2 00A.2.265.00 KTS VMAN V MAN (maneuvering speed) |
| VMAX FAC1 00A.1.207.00 KTS VMAX V MAX (max allowed speed) |
| VMAX FAC2 00A.2.207.00 KTS VMAX V MAX (max allowed speed) |
| VORF DMC1 025.1.034.01 MHZ VOR1_FREQ VOR 1 frequency |
| VORF DMC2 025.2.034.10 MHZ VOR2_FREQ VOR 2 frequency |
| VORRC EIU1 07B.1.200.XX VORRC.1 Variable Oil Reduction |
| Valve Position Request/ |
| Command |
| VORRC EIU2 07B.2.200.XX VORRC.2 Variable Oil Reduction |
| Valve Position Request/ |
| Command |
| VORV EIU1 07B.1.177.XX % VORV.1 Variable Oil Reduction |
| Valve Position Feedback |
| VORV EIU2 07B.2.177.XX % VORV.2 Variable Oil Reduction |
| Valve Position Feedback |
| VOTM EIU1 07B.1.213.XX mA VOTM.1 VORV TM Current |
| VOTM EIU1 07B.1.213.XX mA VOTM.1 VORV TM Current |
| VRTA SDAC1 029.1.333.01 G VRTACC Normal acceleration |
| VRTA SDAC2 029.2.333.10 G VRTACC Normal acceleration |
| VRTG IRS1 004.1.333.01 G VRTG Body normal acceleration |
| VRTG IRS2 029.2.333.10 G VRTG Body normal acceleration |
| VSCB PRESS1 05C.1.150.01 FT/MIN VSCB Cabin v/s |
| VSCB PRESS2 05C.2.150.10 FT/MIN VSCB Cabin v/s |
| VSVA EIU1 07B.1.314.XX % VSVA.1 Variable stator vane |
| actuator percent open |
| command |
| VSVA EIU2 07B.2.314.XX % VSVA.2 Variable stator vane |
| actuator percent open |
| command |
| VW ZC/ACSC2 05D.2.207.10 % VW CAB temp reg vlv pos |
| group 2 |
| W14 EIU1 07B.1.360.XX PPS W14.1 Synthesized Air Flow at |
| station 14 |
| W14 EIU2 07B.2.360.XX PPS W14.21 Synthesized Air Flow at |
| station 14 |
| WAI SDAC1 029.1.001.11 WAI_VLV_CL_1 LH wing anti ice valve |
| closed system #1 |
| WAI SDAC2 029.1.001.00 WAI_VLV_CL_2 LH wing anti ice valve |
| closed system #2 |
| WAIV SDAC1 029.1.001.00 DISCRETE RHW11 Wing Anti-Ice valve |
| Closed Right Hand |
| WAIV SDAC2 029.2.001.00 DISCRETE RHW00 Wing Anti-Ice valve |
| Closed Right Hand |
| WAIV SDAC1 029.1.001.11 DISCRETE LHW.1.1 Wing Anti-Ice valve |
| Closed Right Hand |
| WAIV SDAC2 029.2.001.11 DISCRETE RHW.1.2 Wing Anti-Ice valve |
| Closed Right Hand |
| WARN FWC1 026.1.126.00 FWC126DSW1 FWC Discrete status |
| word |
| WARN FWC2 026.2.126.00 FWC126DSW1 FWC Discrete status |
| word |
| WB APU1 07A.1.123.01 KG/S WB APU bleed air flow |
| WD IRS1 004.1.316.01 DEG WD_1 WING DIRECTION true |
| system #1 |
| WD IRS2 004.2.316.10 DEG WD_2 WING DIRECTION true |
| system #2 |
| WEFA1 MP14E WEFA interlock |
| discrete 1 |
| WEFA2 TP14H WEFA interlock |
| discrete 2 |
| WEFA3 MP14G WEFA interlock |
| discrete 3 |
| WFQ FQIC 05A.2.257.10 KG/LBS WFQ_1 Fuel quantity LH inner |
| cell system #1 |
| WFQ FQIC 05A.2.261.10 KG/LBS WFQ_2 Fuel quantity LH inner |
| cell system #2 |
| WOW EIU1 07B.1.031.XX DISCRETE WOW.1 Aircraft On Ground |
| Selected |
| WOW EIU2 07B.2.031.XX DISCRETE WOW.2 Aircraft On Ground |
| Selected |
| WS IRS1 004.1.315.01 KTS WS_1 WIND SPEED system #1 |
| WS IRS2 004.2.315.10 KTS WS_2 WIND SPEED system #2 |
| WS1 BSCU1 06E.1.320.01 M/S WS1 Wheel 1 speed |
| WS1 BSCU2 06E.2.320.10 M/S WS1 Wheel 1 speed |
| WS2 BSCU1 06E.1.321.01 M/S WS2 Wheel 2 speed |
| WS2 BSCU2 06E.2.321.10 M/S WS2 Wheel 2 speed |
| WS3 BSCU1 06E.1.322.01 M/S WS3 Wheel 3 speed |
| WS3 BSCU2 06E.2.322.10 M/S WS3 Wheel 3 speed |
| WS4 BSCU1 06E.1.323.01 M/S WS4 Wheel 4 speed |
| WS4 BSCU2 06E.2.323.10 M/S WS4 Wheel 4 speed |
| XACC IRS1 004.1.331.01 G XACC.1 Aircraft longtitudinal |
| acceleration |
| XACC IRS2 004.2.331.10 G XACC.2 Aircraft longtitudinal |
| acceleration |
| XFV SDAC1 029.1.055.01 DISCRETE XFV.1 Xfeed Valve Closed |
| XFV SDAC2 029.2.055.10 DISCRETE XFV.1 Xfeed Valve Closed |
| YACC IRS1 004.1.332.01 G YACC.1 Aircraft lateral |
| acceleration |
| YACC IRS2 004.2.332.10 G YACC.2 Aircraft lateral |
| acceleration |
| YAW IRS1 004.1.330.01 DEG/S YAW Body axis YAW rate |
| YAW IRS2 004.2.330.10 DEG/S YAW Body axis YAW rate |
| ZCB PRESS1 05C.1.151.01 FEET ZCB Cabin altitude |
| ZCB PRESS2 05C.2.151.10 FEET ZCB Cabin altitude |
| ZDW1 ZC/ACSC2 05D.2.060.10 ZC060DW Discrete data word |
| (Label 060) Zone |
| Controller bus2 |
| ZLD PRESS1 05C.1.163.01 FEET ZLD Landing elevation |
| ZLD PRESS2 05C.2.163.10 FEET ZLD Landing elevation |