W DOC AIRBUS | TSM A320F

FWD and Aft Cargo Compartment Doors do not operate in the Normal Mode


TASK 52-36-00-810-806-A
FWD and Aft Cargo Compartment Doors do not operate in the Normal Mode


1. Possible Causes
  • LIGHT-AFT DOOR OPEN AND LOCKED [8MJ]
  • LIGHT-FWD DOOR OPEN AND LOCKED [9MJ]
  • RELAY-SCCB PWR SPLY [3811GX]
  • RELAY-TIME [6MJ]
  • RELAY-L/G POSITION, SYS 2 [12GB]
  • LGCIU-2 [5GA2]
  • RELAY-PTU VALVE [1803GL]
  • RELAY-GND INTERNAL LEAK TEST [1885GP]
  • TIME RELAY [3816GX]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 29-24-00-810-801-A
Loss or Fluctuation of the Pressure of the Yellow Electric Pump
TSM TASK 52-36-00-810-801-A
Fault during the Opening Procedure of the FWD Cargo-Compartment Door
TSM TASK 52-36-00-810-802-A
Fault during the Opening Procedure of the Aft Cargo-Compartment Door
TSM TASK 52-36-00-810-803-A
Fault during the Closing Procedure of the FWD Cargo-Compartment Door
TSM TASK 52-36-00-810-804-A
Fault during the Closing Procedure of the Aft Cargo-Compartment Door
AMM 52-30-00-860-001
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
AMM 52-35-12-400-001
Installation of the Indicator Light
3. Fault Confirmation
Subtask 52-36-00-860-056-A
A. Aircraft Maintenance Configuration
   (1) Operate the FWD or aft cargo-compartment door (referred to as cargo door) as necessary in the normal mode AMM 52-30-00-860-001.
NOTE: Make sure that a second person does not operate the other cargo door.
   (2) Operate the FWD or aft cargo door as necessary in the normal mode AMM 52-30-00-860-001.
NOTE: Make sure that a second person does not operate the other cargo door.
4. Fault Isolation
Subtask 52-36-00-810-063-B
A. If the fault confirmation shows that the two cargo doors do not operate in normal mode:
  • do a check of the CB (1MJ) to make sure that it is closed.
   (1) If the CB (1MJ) is open:
  • do a check of the LIGHT-AFT DOOR OPEN AND LOCKED [8MJ] and LIGHT-FWD DOOR OPEN AND LOCKED [9MJ] to make sure that they are serviceable.
NOTE: If necessary, replace the applicable light AMM 52-35-12-400-001.
   (2) If the CB (1MJ) is closed :
  • set the YELLOW ELEC PUMP P/SW (3804GX) on the cockpit panel 40VU to the ON position and see if the ELEC PUMP-Y (3075GX) operates.
NOTE: Make sure that the selector of the applicable manual selector valve is operated during the fault isolation procedure.
   (3) If the ELEC PUMP-Y (3075GX) operates:
   (4) If the ELEC PUMP-Y (3075GX) does not operate:
   (5) Set the YELLOW ELEC PUMP P/SW (3804GX) on the cockpit panel 40VU to the OFF position.
   (6) Do a check for 28 VDC between:
the RELAY-SCCB PWR SPLY [3811GX] connector A/A2 and GND (Ref. ASM 29-24/01).
     (a) If there is 28 VDC:
  • do a check and repair wiring between:
    the RELAY-SCCB PWR SPLY [3811GX] connector A/A2 and
    the DET-PHASE UNBALANCE, Y ELEC PUMP (3808GX) connector A/F.
     (b) If there is no 28 VDC:
  • do a check for continuity between:
    the RELAY-SCCB PWR SPLY [3811GX] connectors A/A1 and A/A2 (Ref. ASM 29-24/01).
       1 If there is no continuity:
  • do a check for 28 VDC between:
    the RELAY-SCCB PWR SPLY [3811GX] connector A/X1 and GND (Ref. ASM 29-24/01).
         a If there is 28 VDC:
  • replace the RELAY-SCCB PWR SPLY [3811GX] .
       2 If there is continuity:
  • do a check for continuity between:
    the TIME RELAY (6MJ) connector A2 and A1 (Ref. ASM 29-24/01).
         a If there is no continuity:
         b If there is continuity:
  • do a check and repair the wiring between:
    the TIME RELAY (6MJ) connector A2 and the CB (3803GX) (Ref. ASM 29-24/01).
   (7) If the fault continues:
  • do a check for continuity between:
    the RELAY-PTU VALVE [1803GL] connector 2 and A (Ref. ASM 29-24/01) and
    the RELAY-PTU VALVE [1803GL] connector 4 and B (Ref. ASM 29-24/01).
     (a) If there is no continuity:
  • replace RELAY-PTU VALVE [1803GL] .
       1 If the fault continues:
  • do a check and repair the wiring between:
    the RELAY-PTU VALVE [1803GL] connectors A and B and the TIME RELAY (6MJ)
    connector A1 (Ref. ASM 29-24/01).
     (b) If there is continuity:
  • do a check for continuity between:
    the RELAY-GND INTERNAL LEAK TEST [1885GP] connector 2 and A (Ref. ASM 29-24/01).
       1 If there is no continuity:
  • replace the RELAY-GND INTERNAL LEAK TEST [1885GP] .
         a If the fault continues:
  • do a check and repair the wiring between:
  • the RELAY-GND INTERNAL LEAK TEST [1885GP] connector A and the RELAY-PTU VALVE [1803GL] connector 2 (Ref. ASM 29-24/01).
  • the RELAY-GND INTERNAL LEAK TEST [1885GP] connector B and the RELAY-PTU VALVE [1803GL] connector 4 (Ref. ASM 29-24/01).
       2 If there is continuity:
  • do a check and repair the wiring between
    the RELAY-GND INTERNAL LEAK TEST [1885GP] connector 2 and the RELAY-SCCB PWR SPLY [3811GX] connector A1 (Ref. ASM 29-24/01).
     (c) If there is continuity:
  • do a check for continuity between:
    the RELAY-GND INTERNAL LEAK TEST [1885GP] connector 4 and B (Ref. ASM 29-24/01).
       1 If there is continuity:
  • do a check and repair the wiring between:
    the RELAY-GND INTERNAL LEAK TEST [1885GP] connector 4 and the TIME RELAY [3816GX] connector C1 (Ref. ASM 29-24/01).
   (8) If the fault continues:
  • do a check for continuity between:
    the TIME RELAY [3816GX] connector A/B2 and A/B1 (Ref. ASM 29-24/01).
     (a) If there is no continuity:
  • replace the TIME RELAY [3816GX] .
     (b) If there is continuity:
  • do a check and repair the wiring between:
    the TIME RELAY [3816GX] connector B1 and the RELAY-SCCB PWR SPLY [3811GX] connector X1 (Ref. ASM 29-24/01).
Subtask 52-36-00-869-055-A
B. Do the test given in Para. 3.A to make sure that the operation is correct.
[Rev.8 from Aug 2018] 2026.04.04 04:34:53 UTC