W DOC AIRBUS | AMM A320F

Functional Test of the ADM Accuracy


TASK 34-13-00-720-010-A
Functional Test of the ADM Accuracy


WARNING: MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
CAUTION: TO PREVENT DAMAGE TO INSTRUMENTS, OBEY THESE PRECAUTIONS WHEN YOU DO THE TEST:
  • THE PRESSURES SET MUST NOT BE MORE THAN 1050 hPa (31 in Hg) OR LESS THAN 115 hPa (3.39 in Hg)
  • CHANGES IN STATIC AND TOTAL PRESSURES MUST NOT BE MORE THAN 6000 FEET/MINUTE
  • DO NOT SUDDENLY OPEN LINES TO AMBIENT AIR WHILE THE PRESSURE GENERATOR IS CONNECTED.
CAUTION: THE TOTAL PRESSURE IN THE PITOT SYSTEM MUST NEVER BE LESS THAN THE STATIC PRESSURE. THE DIFFERENCE BETWEEN THE PITOT AND THE STATIC PRESSURE CIRCUITS MUST NEVER BE MORE THAN 368 hPa (10.86 in Hg).
ZONE: 120
ZONE: 210
ZONE: 230
1. Reason for the Job
Refer to the MPD TASK: 341300-13
FUNCTIONAL TEST OF THE ADM ACCURACY
To make sure that the static and total pressure values from the ADMs are accurate.
NOTE: The effectivity of this task is "ALL". To know if this task is applicable for your aircraft, refer to the MPD applicability and related MPD task source document.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SHEET - PLASTIC
No specific
AR
TAPE - ADHESIVE
No specific
AR
WARNING NOTICE(S)
ALT34100001
1
PITOT AND STATIC TEST SET
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
120
AVIONICS COMPARTMENT
210
CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
230
FWD PASSENGER COMPARTMENT
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 27-50-00-866-009-A
Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01
Retraction of the Flaps/Slats on the Ground
TASK 31-36-00-740-008-A
Access to the Parameter Call-Up Menus
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 34-10-00-860-002-A
ADIRS Start Procedure
TASK 34-10-00-860-005-A
ADIRS Stop Procedure
TASK 34-11-17-000-001-A
Removal of the Air Data Module
TASK 34-11-17-400-001-A
Installation of the Air Data Module (ADM)
TASK 34-13-00-790-002-A
Leak Test of the Principal Static and Total Air Data System
TASK 34-21-00-790-001-A
Low-Range Leak Test of the Standby Pneumatic Circuits
TASK 34-22-25-790-001-A
Low range Leak Test of the Standby Pneumatic circuits
3. Job Set-up
Subtask 34-13-00-860-106-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Remove the protective covers from the sensors and the probes (AOA, Static, Pitot and TAT)
   (2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (3) Do the EIS start procedure (PFD DUs only) (Ref. AMM TASK 31-60-00-860-001).
   (4) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
   (5) Make sure that the flaps are in the fully retracted position (Ref. AMM TASK 27-50-00-866-009).
   (6) Access to the parameter call-up menus (If available) (Ref. AMM TASK 31-36-00-740-008).
   (7) On the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at NORM.
   (8) On the FCU, on the EFIS control section, do the steps that follow:
  • Set the two "in Hg/hPa" selector switches to hPa
  • Pull the baro-reference selector knob.
   (9) On the CAPT and F/O PFDs, make sure the STD indication is shown below the altitude scale.
Subtask 34-13-00-875-056-A ** ON A/C NOT FOR ALL
WARNING: BEFORE YOU OPEN PHC CIRCUIT BREAKERS 2DA1(2,3), OPEN PROBE HEATER CIRCUIT-BREAKERS 1DA1(2), 3DA1(2,3), 4DA1(2,3) AND 5DA1(2,3). IF YOU DO NOT OBEY THIS SEQUENCE: - THE PROBES WILL BECOME TOO HOT. - THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL.
B. Open, safety and tag these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PITOT/13DA1D02
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
49VUANTI ICE/PROBES/AOA/14DA1D04
122VUANTI ICE/PROBES/2/AOA4DA2Y13
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/1/TAT1DA1Z12
122VUANTI ICE/PROBES/2/TAT1DA2Y15
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/PROBES/PHC/22DA2Y12
122VUANTI ICE/PROBES/PHC/32DA3Y16
Subtask 34-13-00-860-106-B ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Remove the protective covers from the sensors and the probes (AOA, Static, Pitot and TAT)
   (2) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (3) Do the EIS start procedure (PFD DUs only) (Ref. AMM TASK 31-60-00-860-001).
   (4) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
   (5) Make sure that the flaps are in the fully retracted position (Ref. AMM TASK 27-50-00-866-009).
   (6) Access to the parameter call-up menus (If available) (Ref. AMM TASK 31-36-00-740-008).
   (7) On the SWITCHING panel 8VU, make sure that the AIR DATA selector switch is at NORM.
   (8) On the FCU, on the EFIS control section, do the steps that follow:
  • Set the two "in Hg/hPa" selector switches to hPa.
  • Pull the baro-reference selector knob.
   (9) On the CAPT and F/O PFDs, make sure the STD indication is shown below the altitude scale.
   (10) On the ENG section of the panel 50VU:
  • Make sure that the ON legend of the ENG/FADEC GND PWR 1 and ENG/FADEC GND PWR 2 pushbutton switches are off.
  • Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC system.
Subtask 34-13-00-875-056-B ** ON A/C NOT FOR ALL
WARNING: BEFORE YOU OPEN PHC CIRCUIT BREAKERS 2DA1(2,3), OPEN PROBE HEATER CIRCUIT-BREAKERS 1DA1(2), 3DA1(2,3), 4DA1(2,3) AND 5DA1(2,3). IF YOU DO NOT OBEY THIS SEQUENCE: - THE PROBES WILL BECOME TOO HOT. - THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL.
D. Open, safety and tag these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PITOT/13DA1D02
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
49VUANTI ICE/PROBES/AOA/14DA1D04
122VUANTI ICE/PROBES/2/AOA4DA2Y13
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/1/TAT1DA1Z12
122VUANTI ICE/PROBES/2/TAT1DA2Y15
121VUCOM NAV/RAD ALTM/11SA1K11
121VUCOM NAV/RAD ALTM/21SA2K12
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/PROBES/PHC/22DA2Y12
122VUANTI ICE/PROBES/PHC/32DA3Y16
Subtask 34-13-00-865-112-A
E. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUNAV PROBES/ADIRU 1/AND AOA 1/26VAC5FP1F07
49VUNAV PROBES/ADIRU1/115VAC4FP1F06
105VUADIRS/ADIRU1/28VDC6FP1C02
** ON A/C NOT FOR ALL
121VUADIRS/ADIRU/2PWR/SHED10FPN10
** ON A/C ALL
121VUADIRS/ADIRU/3PWR/SWTG9FPN09
121VUADIRS/ADIRU/2/26VAC AND AOA5FP2N08
121VUADIRS/ADIRU/3/26VAC AND AOA5FP3N07
121VUADIRS/ADIRU/2/115VAC4FP2N06
121VUADIRS/ADIRU/3/115VAC4FP3N05
121VUADIRS/ADIRU/2/28VDC6FP2N04
121VUADIRS/ADIRU/3/28VDC6FP3N03
** ON A/C NOT FOR ALL
121VUADIRS/2PWR/SHED &/AOA2 MON10FPN10
** ON A/C NOT FOR ALL
FOR FIN: 2CE1 (ELAC1)
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
** ON A/C ALL
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
FOR FIN: 2CE2 (ELAC2)
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
Subtask 34-13-00-790-054-A ** ON A/C NOT FOR ALL
F. Do these procedures:
Subtask 34-13-00-790-054-B ** ON A/C NOT FOR ALL
F. Do these procedures:
Subtask 34-13-00-480-057-A
G. Installation of the Ground Pressure Generator
   (1) When you operate the ground pressure generator, use the parameters that follow:
  • The altitude between -1000 ft. (-304.79 m) and 50000 ft. (15239.72 m) (accuracy +/- 0.1 hPa (0.00145 psi)) or the values in feet that follow, in relation to the altitude level:
    Sea level: +/- 3 ft. (0.91 m)
    5000 ft. (1523.97 m): +/- 4 ft. (1.22 m)
    30000 ft. (9143.83 m): +/- 8 ft. (2.44 m)
    50000 ft. (15239.72 m): +/- 18 ft. (5.49 m).
  • The speed between 0 and 500 kts.
  • The climb rate between 0 and +/- 6000 ft.min (1828.77 m.min) (+/- 7%).
   (2) Remove the slip-on covers from all the static and pitot probes.
   (3)      (a) The static probes with the ADAPTER STATIC PROBE (4):
       1 For the CAPT circuit (Air Data/Inertial Reference Unit 1 (ADIRU 1)) and the F/O circuit (ADIRU 2):
  • 7DA1 ZONE 127 Station (STA) 8750 for the left static-pressure Air Data Module (ADM) (19FP5)
  • 7DA2 ZONE 127 STA 8700 for the left static-pressure ADM (19FP7)
  • 8DA1 ZONE 128 STA 9300 for the right static-pressure ADM (19FP4)
  • 8DA2 ZONE 128 STA 9350 for the right static-pressure ADM (19FP6).
     (b) The static probes with the ADAPTER STATIC PROBE (5):
       1 For the standby circuit (ADIRU 3):
  • 7DA3 ZONE 121 STA 4250 for the static pressure ADM (19FP8), or
  • 8DA3 ZONE 122 STA 4250 for the static pressure ADM (19FP8).
     (c) The pitot probes with the ADAPTER PITOT PROBE (2) or (3) for the Thales probes or the ADAPTER PITOT PROBE (3) for the Rosemount (Aerospace)/Goodrich probes:
       1 For the CAPT circuit (ADIRU 1):
  • 9DA1 ZONE 125 STA 5500 for the total pressure ADM (19FP1).
       2 For the F/O circuit (ADIRU 2):
  • 9DA2 ZONE 126 STA 5500 for the total pressure ADM (19FP2).
       3 For the standby circuit (ADIRU 3):
  • 9DA3 ZONE 125 STA 5500 for the total pressure ADM (19FP3).
   (4) Seal the pitot drain holes of the Thales pitot probes (C16195AA or C16195AB):
CAUTION: WHEN YOU SEAL THE DRAIN HOLE IN THE PITOT PROBE, DO NOT SEAL THE HOLE DIRECTLY WITH THE COLORED ADHESIVE TAPE. ALWAYS PUT A PIECE OF PLASTIC ON THE HOLE FIRST AND USE THE COLORED ADHESIVE TAPE TO ATTACH THE PLASTIC. IF YOU SEAL THE DRAIN HOLE DIRECTLY WITH THE ADHESIVE TAPE, THERE IS A RISK THAT SOME OF THE ADHESIVE WILL STAY ON THE HOLE AND COLLECT PARTICLES. THIS CAN SUBSEQUENTLY CAUSE BLOCKAGE OF THE HOLE AND THUS INCORRECT OPERATION OF THE PROBE.
     (a) Seal the drain holes of the pitot probes with the SHEET - PLASTIC and the color TAPE - ADHESIVE.
     (b) Make sure that you can see the adhesive tape from the ground.
   (5) Seal the opposite static probe of the standby ADM with the ADAPTER STATIC PROBE.
   (6) Set the Angle Of Attack (AOA) sensors to the high stop position
     (a) Slowly turn the vanes of the three AOA sensors to the high stop position.
     (b) Keep the vanes in position with the adhesive tape.
   (7) Start the ground pressure generator.
4. Procedure
Subtask 34-13-00-720-068-R ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.9 hPa (5.5191 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.49 hPa (0.1916 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40081 ft. (12216.46 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 63.64 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
6.On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
7.On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
8.On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
9.On the ground pressure generator, at the same time:
  • Slowly increase the pressure in the static and total pressure lines to get the atmospheric pressure at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
10.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
11.Refer to Table 36 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5958 and 6004
006
2
176
10
5958 and 6004
006
1
177
01
5958 and 6004
006
2
177
10
5958 and 6004
006
3
245
11
5958 and 6004
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-S ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.9 hPa (5.5191 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.49 hPa (0.1916 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40081 ft. (12216.46 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 63.64 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/18 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/18 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
6.On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/18 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/18 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
7.On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/18 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/18 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
8.On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/18 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/18 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
9.On the ground pressure generator, at the same time:
  • Slowly increase the pressure in the static and total pressure lines to get the atmospheric pressure at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
10.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
11.Refer to Table 38 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
23833 and 24013
006
2
176
10
23833 and 24013
006
1
177
01
23833 and 24013
006
2
177
10
23833 and 24013
006
3
245
11
23833 and 24013
006
1
242
01
24664 and 24844
006
2
242
10
24664 and 24844
006
3
242
11
24664 and 24844
Subtask 34-13-00-720-068-W ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.54 hPa (5.5085 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.85 hPa (0.2023 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40053 ft. (12207.93 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 62.42 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
6.On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
7.On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
8.On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
9.On the ground pressure generator, at the same time:
  • Slowly increase the pressure in the static and total pressure lines to get the atmospheric pressure at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
10.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
11.Refer to Table 46 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5946 and 5992
006
2
176
10
5946 and 5992
006
1
177
01
5946 and 5992
006
2
177
10
5946 and 5992
006
3
245
11
5946 and 5992
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-A0 ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.57 hPa (5.5094 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.82 hPa (0.2014 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40062 ft. (12210.67 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 62.82 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
6.On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
7.On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
8.On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
9.On the ground pressure generator, at the same time:
  • Slowly increase the pressure in the static and total pressure lines to get the atmospheric pressure at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
10.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
11.Refer to Table 54 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5947 and 5993
006
2
176
10
5947 and 5993
006
1
177
01
5947 and 5993
006
2
177
10
5947 and 5993
006
3
245
11
5947 and 5993
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-AA ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.57 hPa (5.5094 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.82 hPa (0.2014 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40062 ft. (12210.67 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 62.82 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
6.On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
7.On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
8.On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
9.On the ground pressure generator, at the same time:
  • Slowly increase the pressure in the static and total pressure lines to get the atmospheric pressure at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
10.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
11.Refer to Table 56 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5947 and 5993
006
2
176
10
5947 and 5993
006
1
177
01
5947 and 5993
006
2
177
10
5947 and 5993
006
3
245
11
5947 and 5993
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-AT ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.59 hPa (5.5100 in.Hg).
  • Set a total pressure (Pt) of 193.39 hPa (5.7108 in.Hg).
  • The associated impact pressure (Qc) is 6.8 hPa (0.2008 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40047 ft. (12206.10 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 62.13 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • The related label and databits come into view.
  • For the standby total-pressuure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
6.On the ground pressure generator, at the same time:
  • At the same time, slowly decrease the pressure in the static and total pressure lines to 0 mbar (0 psi) at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
7.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
8.Refer to Table 70 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5948 and 5994
006
2
176
10
5948 and 5994
006
1
177
01
5948 and 5994
006
2
177
10
5948 and 5994
006
3
245
11
5948 and 5994
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-AW ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.6 hPa (5.5103 in.Hg).
  • Set a total pressure (Pt) of 193.4 hPa (5.7111 in.Hg).
  • The associated impact pressure (Qc) is 6.8 hPa (0.2008 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40060 ft. (12210.06 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 63 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
6.On the ground pressure generator, at the same time:
  • Slowly decrease the pressure in the static and total pressure lines to 0 mbar (0 psi) at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
7.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
8.Refer to Table 74 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5949 and 5994
006
2
176
10
5949 and 5994
006
1
177
01
5949 and 5994
006
2
177
10
5949 and 5994
006
3
245
11
5949 and 5994
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-068-AZ ** ON A/C NOT FOR ALL
A. Functional Test of the Air Data Module (ADM) Accuracy
   (1) On the CAPT and F/O PFDs, make sure that the altitude and the airspeed values do not change during the test.
   (2) The number of digits of the EQ parameter code that you must enter (two or three digits) is related to the Data Management Unit (DMU)/Flight Data Interface and Management Unit (FDIMU) equipment installed (hardware and software version). The procedure and the table that follow show three digits. If you cannot enter the three digits, enter the last two digits. For example, 06 and not 006 or 26 and not 026.
   (3) To do this procedure, use the reference values given in the table that follows:
ACTION
RESULT
1.On the ground pressure generator:
  • Set a static pressure (Ps) of 186.6 hPa (5.5103 in.Hg).
  • Set a total pressure (Pt) of 193.4 hPa (5.7111 in.Hg).
  • The associated impact pressure (Qc) is 6.8 hPa (0.2008 in.Hg).
  • If you can get a stable pressure measurement:
    -Keep the electrovalves open.
  • If you cannot get a stable pressure measurement:
    -Close the electrovalves.

2.On the center pedestal, on SWITCHING panel 8VU:
  • Make sure that the AIR DATA selector switch is set to the NORM position.
On the CAPT and F/O PFDs:
  • Make sure that the altitude value is 40000 ft. (12191.78 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 60 kts +/- 5 kts.
3.On the center pedestal, on SWITCHING panel 8VU:
  • Set the AIR DATA selector switch to the CAPT/3 (F/O/3) position.
On the CAPT (F/O) PFD:
  • Make sure that the altitude value is 40045 ft. (12205.49 m) +/- 110 ft. (33.53 m).
  • Make sure that the speed value is 62 kts +/- 5 kts.
4.On the Multipurpose Control & Display Unit (MCDU):
  • On the MCDU MENU page, push the line key adjacent to the AIDS indication.
On the MCDU:
  • The AIDS menu page comes into view.
  • On the AIDS menu page, push the line key adjacent to the CALL-UP PARAM indication.
  • The AIDS PARAM CALL-UP page comes into view.
  • On the AIDS PARAM CALL-UP page, push the line key adjacent to the PARAM LABEL CALL-UP indication.
  • The AIDS PAR LAB CALL-UP 1/8 page comes into view.
5.On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • For the left static-pressure ADM (19FP5), enter 006/1/176/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 1/8 page:
  • The related label and databits come into view.
  • For the left static-pressure ADM (19FP7), enter 006/2/176/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 2/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • For the right static-pressure ADM (19FP4), enter 006/1/177/01/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 2/8 page:
  • The related label and databits come into view.
  • For the right static-pressure ADM (19FP6), enter 006/2/177/10/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 3/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • For the standby static-pressure ADM (19FP8), enter 006/3/245/11/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 3/8 page:
  • The related label and databits come into view.
  • For the left total-pressure ADM (19FP1), enter 006/1/242/01/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.

  • On the MCDU keyboard, push the NEXT PAGE key.
  • The AIDS PAR LAB CALL-UP 4/8 page comes into view.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • For the right total-pressure ADM (19FP2), enter 006/2/242/10/16 on the scratchpad, then push the line key adjacent to the first arrow.
On the MCDU, on the AIDS PAR LAB CALL-UP 4/8 page:
  • The related label and databits come into view.
  • For the standby total-pressure ADM (19FP3), enter 006/3/242/11/16 on the scratchpad, then push the line key adjacent to the second arrow.
  • The related label and databits come into view.
  • Push the line key adjacent to the PRINT indication and print this page.
6.On the ground pressure generator, at the same time:
  • Slowly decrease the pressure in the static and total pressure lines to 0 mbar (0 psi) at a maximum vertical speed of 6000 ft.min (1828.77 m.min).
  • Open the electrovalves, if necessary.
7.Disconnect the static and total pressure lines from the ground pressure generator to get the atmospheric pressure:
  • Stop the ground pressure generator.
8.Refer to Table 78 to make sure that the printed values are in the correct range.

EQ
SYS
LAB
SDI
DATABIT must be between:
006
1
176
01
5949 and 5994
006
2
176
10
5949 and 5994
006
1
177
01
5949 and 5994
006
2
177
10
5949 and 5994
006
3
245
11
5949 and 5994
006
1
242
01
6166 and 6211
006
2
242
10
6166 and 6211
006
3
242
11
6166 and 6211
Subtask 34-13-00-720-070-B
B. If the recorded values during the test are not in the correct tolerance replace the ADMs as follows:
   (1) For the ADR1:
     (a) If the static pressure value is not in the correct tolerance:
     (b) If the total pressure value is not in the correct tolerance:
   (2) For the ADR2:
     (a) If the static pressure value is not in the correct tolerance:
     (b) If the total pressure value is not in the correct tolerance:
   (3) For the ADR3:
     (a) If the static pressure value is not in the correct tolerance:
     (b) If the total pressure value is not in the correct tolerance:
5. Close-up
Subtask 34-13-00-080-055-A
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 34-13-00-875-057-A ** ON A/C NOT FOR ALL
B. Remove the safety clips and tags and close these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/PROBES/PHC/22DA2Y12
122VUANTI ICE/PROBES/PHC/32DA3Y16
49VUANTI ICE/PROBES/PITOT/13DA1D02
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/2/AOA4DA2Y13
49VUANTI ICE/PROBES/AOA/14DA1D04
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
122VUANTI ICE/PROBES/1/TAT1DA1Z12
122VUANTI ICE/PROBES/2/TAT1DA2Y15
Subtask 34-13-00-875-057-B ** ON A/C NOT FOR ALL
B. Remove the safety clips and tags and close these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUANTI ICE/PROBES/PHC/12DA1D03
122VUANTI ICE/PROBES/PHC/22DA2Y12
122VUANTI ICE/PROBES/PHC/32DA3Y16
49VUANTI ICE/PROBES/PITOT/13DA1D02
122VUANTI ICE/PROBES/2/PITOT3DA2Y14
122VUANTI ICE/PROBES/3/PITOT3DA3Z16
122VUANTI ICE/PROBES/2/AOA4DA2Y13
49VUANTI ICE/PROBES/AOA/14DA1D04
122VUANTI ICE/PROBES/3/AOA4DA3Z15
122VUANTI ICE/PROBES/1/STATIC5DA1Z13
122VUANTI ICE/PROBES/2/STATIC5DA2Y11
122VUANTI ICE/PROBES/3/STATIC5DA3Z14
122VUANTI ICE/PROBES/1/TAT1DA1Z12
122VUANTI ICE/PROBES/2/TAT1DA2Y15
121VUCOM NAV/RAD ALTM/11SA1K11
121VUCOM NAV/RAD ALTM/21SA2K12
Subtask 34-13-00-860-107-A
C. Put the aircraft back to its initial configuration.
   (1) Remove the piece of plastic and the colored adhesive tape from the drain of the pitot probes.
   (2) Remove the colored adhesive tape from the AOA sensors.
   (3) Install the protective covers on the sensors and probes (AOA, Static, Pitot and TAT).
   (4) Do a reset of each Elevator Aileron Computer (ELAC):
     (a) FOR [2CE1] (ELAC-1)
       1 Open, then close circuit breakers 15CE1 and 16CE1.
     (b) FOR [2CE2] (ELAC-2)
       1 Open, then close circuit breakers 15CE2 and 16CE2.
   (5) On the center pedestal, on SWITCHING panel 8VU, set the AIR DATA selector switch to NORM.
   (6) On the MCDU, push the line key adjacent to the RETURN indication until the MAINTENANCE MENU 1/2 page comes into view.
   (7) On the FCU, set the baro-reference selector knob to its initial position.
   (8) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
   (9) On CAPT and F/O lighting/LOUD SPEAKER control panels 301VU & 500VU, set the PFD potentiometers to OFF.
   (10) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:23:10 UTC