W DOC AIRBUS | TSM A320F

APU Fuel System - Low Pressure


TASK 28-22-00-810-801-A
APU Fuel System - Low Pressure


1. Possible Causes
  • PRESS SWITCH-APU FUEL PRESSURE [7QC]
  • RELAY 6QC
  • RELAY 5QC
  • RELAY 9QC
  • wiring
  • PUMP-APU FUEL [4QC]
  • RELAY 4KD
  • SWITCH-APU FUEL LP [5030QM]
  • wiring and connectors between the switch 5030QM and the ECB
  • ELECTRONIC CONTROL BOX [59KD]
  • VALVE-AIR RELEASE, L WING TK [86QM]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 28-21-41-000-001
Removal of the Low Pressure (LP) Air-Release-Valve 86QM(87QM)
AMM 28-21-41-400-001
Installation of the Low Pressure (LP) Air-Release-Valve 86QM(87QM)
ASM 282201
AMM 28-22-14-000-001
Removal of the APU Fuel LP-Switch
AMM 28-22-14-400-001
Installation of the APU Fuel LP-Switch
AMM 28-22-15-000-001
Removal of the APU Fuel Pressure Switch
AMM 28-22-15-400-001
Installation of the APU Fuel Pressure Switch
AMM 28-22-51-000-001
Removal of the APU Fuel Pump
AMM 28-22-51-400-001
Installation of the APU Fuel Pump
ASM 282901
AMM 49-31-00-710-001
Operational Test of the APU Fuel Low Pressure Circuit (GTCP 36-300)
AMM 49-31-00-710-002
Operational Test of the APU Fuel Low Pressure Circuit (APS 3200)
AMM 49-31-00-710-003
Operational Test of the APU-Fuel Low-Pressure Circuit ((131-9(A))
ASM 496102
AMM 49-61-34-000-003
Removal of the Electronic Control Box (ECB) (131-9(A))
AMM 49-61-34-400-003
Installation of the Electronic Control Box (ECB) (131-9(A))
3. Fault Confirmation
Subtask 28-22-00-710-050-A
A. Operational test
   (1) Do the Operational Test of the APU Fuel Low Pressure Circuit:
   (2) Make sure that the subsequent system is serviceable before you start the fault isolation procedure:
  • the main fuel pump system (Ref. 28-21-00),
  • the APU LP fuel shutoff system (Ref. 28-29-00).
4. Fault Isolation
Subtask 28-22-00-810-051-A
A. If the test gives the subsequent results:
.on the lower ECAM display unit, the FUEL LO PR advisory is off with the L main fuel pump in operation,
.on the lower ECAM display unit, the FUEL LO PR advisory comes on and the APU fuel pump does not operate:
  • push the FUEL LINE pushbutton switch 8QC to operate the APU FUEL PUMP 4QC.
   (1) If the APU FUEL PUMP 4QC operates:
     (a) If the fault continues:
  • Do a check of the RELAY 6QC and replace if necessary.
     (b) If the fault continues:
  • Do a check of the RELAY 5QC and replace if necessary.
     (c) If the fault continues:
  • Do a check of the RELAY 9QC and replace if necessary.
     (d) If the fault continues:
  • Do a check and repair the wiring from the:
    CB 2QC to the RELAY 6QC A/B2,
    RELAY 6QC A/C3 to the PRESS SWITCH 7QC A/B,
    RELAY 5QC A/X1 to the PRESS SWITCH 7QC A/A,
    RELAY 5QC A/X2 to the GND ASM 282201.
   (2) If the APU FUEL PUMP 4QC does not operate:
     (a) If the fault continues:
  • Do a check of the RELAY 5QC and replace if necessary.
     (b) If the fault continues:
  • Do a check of the RELAY 6QC and replace if necessary.
     (c) If the fault continues:
  • Do a check of the RELAY 9QC and replace if necessary.
     (d) If the fault continues:
  • Do a check of the RELAY 4KD and replace if necessary.
     (e) If the fault continues:
  • Do a check and repair the wiring from the:
    CB 1QC to the RELAY 5QC A/B2 via the RELAY 9QC,
    CB 2QC to the RELAY 9QC A/A1,
    CB 2QC to the RELAY 9QC A/X1,
    RELAY 5QC A/B1,A3 to the APU FUEL PUMP 4QC A/A,
    RELAY 6QC A/B1 to the RELAY 5QC A/A2,
    RELAY 6QC A/C2 to the CB 1QF via the RELAYs 4KD, 5WF, 6WF,
    APU FUEL PUMP 4QC A/B to the GND ASM 282201 and ASM 282901.
Subtask 28-22-00-810-052-A
B. If the test gives on the lower ECAM display unit the FUEL LO PR advisory is on, but the test was correct with the L main fuel pump and the APU fuel pump:
   (1) If the fault continues, do a check and repair the wiring and connectors between the switch 5030QM and the ECB :
APU FUEL LP SWITCH 5030QM P17 to the ECB 59KD AB/B7,B8 ASM 496102.
   (2) If the fault continues:
Subtask 28-22-00-810-054-A
C. If the fault continues:
   (1) Replace the VALVE-AIR RELEASE, L WING TK [86QM] AMM 28-21-41-000-001 and AMM 28-21-41-400-001.
Subtask 28-22-00-710-051-A
D. Do the test given in Para. 3.
5. Close-up
Subtask 28-22-00-860-050-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:28:40 UTC