Operational Test of the AFT Cargo-Compartment Door
TASK 52-32-00-710-001-A
Operational Test of the AFT Cargo-Compartment Door
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 52-32-00-010-050-A
Subtask 52-32-00-710-050-C ** ON A/C NOT FOR ALL
Subtask 52-32-00-710-050-D ** ON A/C NOT FOR ALL
5. Close-up
Subtask 52-32-00-860-051-A
[Rev.10 from 2021]
2026.04.01 01:41:54 UTC
Operational Test of the AFT Cargo-Compartment Door
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 154AR |
| 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 29-14-00-614-002-A | Pressurization of the Hydraulic Reservoirs through the Ground Connector |
| TASK 29-14-00-614-002-A-01 | Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU) |
| TASK 29-24-00-864-001-A | Depressurize the Yellow Hydraulic System |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 52-30-00-860-002-A | Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump |
Subtask 52-32-00-010-050-A
A. Get Access
(1) Make sure that the AFT cargo compartment door (referred to as cargo door) is closed (Ref. AMM TASK 52-30-00-860-002).
(2) If necessary, put the ACCESS PLATFORM 2M (6 FT) in position below the closed cargo door.
(3) Open the access panel 154AR to get access to the selector of the control panel.
Subtask 52-32-00-865-050-A (1) Make sure that the AFT cargo compartment door (referred to as cargo door) is closed (Ref. AMM TASK 52-30-00-860-002).
(2) If necessary, put the ACCESS PLATFORM 2M (6 FT) in position below the closed cargo door.
(3) Open the access panel 154AR to get access to the selector of the control panel.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 52-32-00-860-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| ** ON A/C ALL | |||
| 122VU | DOORS/CARGO | 1MJ | T12 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
C. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) Make sure that the Yellow hydraulic system reservoir is pressurized (Ref. AMM TASK 29-14-00-614-002).
4. Procedure(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) Make sure that the Yellow hydraulic system reservoir is pressurized (Ref. AMM TASK 29-14-00-614-002).
Subtask 52-32-00-710-050-C ** ON A/C NOT FOR ALL
WARNING:
MAKE SURE THAT THE TRAVEL RANGE OF THE CARGO DOOR IS CLEAR BEFORE YOU UNLOCK IT. STAY AFT OF (LEFT OF) THE DOOR WHEN YOU UNLOCK IT BECAUSE IT CAN OPEN SUDDENLY AND CAUSE INJURY.
CAUTION:
IMMEDIATELY AFTER YOU OPEN THE CARGO COMPARTMENT DOOR, RECORD ON THE WORK CARD ON THE DOOR, THE DATE AND TIME WHEN YOU OPENED IT. IF THE CARGO COMPARTMENT DOOR STAYS OPEN FOR 12 HOURS OR MORE, YOU MUST BLEED THE HYDRAULIC SYSTEM RELATED TO IT. IF YOU DO NOT OBEY THESE PRECAUTIONS, THE DOOR CAN CLOSE SUDDENLY WHEN YOU SET THE DOOR TO "CLOSE". THIS CAN CAUSE DAMAGE TO THE DOOR AND TO THE AIRCRAFT STRUCTURE.
A. Do this test: | ACTION | RESULT |
|---|---|
| 1.On the AFT cargo door: | On the AFT cargo door: |
|
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| | On the lower ECAM DU:
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| | On the AFT cargo door: |
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| 2.On the control panel: | On the AFT cargo door: |
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| | On the control panel:
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| 3.On the AFT cargo door: | On the AFT cargo door: |
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| 4.On the control panel: | On the AFT cargo door: |
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| | On the control panel: |
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| | On the AFT cargo door: |
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| 5.On the AFT cargo door: | On the AFT cargo door: |
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| 6.On the control panel: | On the AFT cargo door: |
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| 7.On the AFT cargo door: | On the AFT cargo door: |
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| 8.On the control panel: | On the AFT cargo door: |
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| 9.On the AFT cargo door: | On the AFT cargo door: |
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| 10.On the control panel: | On the AFT cargo door: |
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| 11.On the AFT cargo door: | On the AFT cargo door: |
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| | On the lower ECAM DU:
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| 12.On the AFT cargo door: | On the AFT cargo door: |
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WARNING:
MAKE SURE THAT THE TRAVEL RANGE OF THE CARGO DOOR IS CLEAR BEFORE YOU UNLOCK IT. STAY AFT OF (LEFT OF) THE DOOR WHEN YOU UNLOCK IT BECAUSE IT CAN OPEN SUDDENLY AND CAUSE INJURY.
CAUTION:
IMMEDIATELY AFTER YOU OPEN THE CARGO COMPARTMENT DOOR, RECORD ON THE WORK CARD ON THE DOOR, THE DATE AND TIME WHEN YOU OPENED IT. IF THE CARGO COMPARTMENT DOOR STAYS OPEN FOR 12 HOURS OR MORE, YOU MUST BLEED THE HYDRAULIC SYSTEM RELATED TO IT. IF YOU DO NOT OBEY THESE PRECAUTIONS, THE DOOR CAN CLOSE SUDDENLY WHEN YOU SET THE DOOR TO "CLOSE". THIS CAN CAUSE DAMAGE TO THE DOOR AND TO THE AIRCRAFT STRUCTURE.
A. Do this test: | ACTION | RESULT |
|---|---|
| 1.On the AFT cargo door: | On the AFT cargo door: |
|
|
| | On the lower ECAM DU:
|
| | On the AFT cargo door: |
|
|
| 2.On the control panel: | On the AFT cargo door: |
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|
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|
|
| | On the control panel:
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| 3.On the AFT cargo door: | On the AFT cargo door: |
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| 4.On the control panel: | On the AFT cargo door: |
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| | On the control panel: |
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| | On the AFT cargo door: |
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| 5.On the AFT cargo door: | On the AFT cargo door: |
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| 6.On the control panel: | On the AFT cargo door: |
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| 7.On the AFT cargo door: | On the AFT cargo door: |
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| 8.On the control panel: | On the AFT cargo door: |
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| 9.On the AFT cargo door: | On the AFT cargo door: |
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| 10.On the control panel: | On the AFT cargo door: |
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| 11.On the AFT cargo door: | On the AFT cargo door: |
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| | On the lower ECAM DU:
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| 12.On the AFT cargo door: | On the AFT cargo door: |
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Subtask 52-32-00-860-051-A
A. Put the aircraft back to the serviceable condition.
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(2) Make sure that the Yellow auxiliary hydraulic system is depressurized (Ref. AMM TASK 29-24-00-864-001).
(3) Make sure that the aircraft electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
Subtask 52-32-00-410-050-A (1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(2) Make sure that the Yellow auxiliary hydraulic system is depressurized (Ref. AMM TASK 29-24-00-864-001).
(3) Make sure that the aircraft electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
B. Close Access
(1) Make sure that the cargo door is correctly closed (Ref. AMM TASK 52-30-00-860-002).
(2) Close the access panel 154AR.
(3) Remove the access platform(s).
(1) Make sure that the cargo door is correctly closed (Ref. AMM TASK 52-30-00-860-002).
(2) Close the access panel 154AR.
(3) Remove the access platform(s).