W DOC AIRBUS | TSM A320F

Failure of the FRV of the Engine 2 in the Closed Position, on Channel B


TASK 73-10-00-810-820-A
Failure of the FRV of the Engine 2 in the Closed Position, on Channel B


1. Possible Causes
  • harness J8
  • fuel return valve
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 73-11-50-000-002
Removal of the Fuel Return Valve (FRV)
AMM 73-11-50-400-002
Installation of the Fuel Return Valve
AMM 73-21-50-000-041
Removal of the HJ8 Harness for SAC Engines
AMM 73-21-50-400-041
Installation of the HJ8 Harness for SAC Engines
AMM 73-21-60-000-001
Removal of the Electronic Control Unit (ECU)
AMM 73-21-60-400-001
Installation of the Electronic Control Unit (ECU)
ASM 732518
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 73-10-00-710-086-A ** ON A/C NOT FOR ALL
A. Not applicable.
4. Fault Isolation
Subtask 73-10-00-810-073-A ** ON A/C NOT FOR ALL
A. The fault is generated when the fuel return valve fails to reach the opened position when commanded by the ECU.
   (1) Inspect the J8 harness and associated connectors for sign of damage or contamination ASM 732518.
   (2) If damage is found:
   (3) If nothing is found:
   (4) If the fault continues:
   (5) If the fault continues:
Subtask 73-10-00-710-087-A ** ON A/C NOT FOR ALL
B. Test sensor to force the opening of the fuel return valve.
   (1) Perform an operational test with engine motoring AMM 73-29-00-710-040 and check that the fault does not duplicate.
[Rev.8 from Aug 2018] 2026.04.04 04:35:14 UTC