W DOC AIRBUS | TSM A320F

Failure of the Control of the Solenoid 1 of the Fuel Return Valve on Channel A, Engine 2


TASK 73-20-00-810-906-A
Failure of the Control of the Solenoid 1 of the Fuel Return Valve on Channel A, Engine 2


1. Possible Causes
  • ECU [4000KS]
  • fuel return valve
  • harness J7
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
BRUSH - BRISTLED
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2011)
stoddard solvent
 C. 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 73-21-50-000-040
Removal of the HJ7 Harness for SAC Engines
AMM 73-21-50-210-002
Visual Inspection of the Wiring Harnesses
AMM 73-21-50-400-040
Installation of the HJ7 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 73-20-00-710-208-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational test of the FADEC 2A on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-20-00-810-174-A ** ON A/C NOT FOR ALL
A. The fault is generated when the ECU detects an open circuit or a short to ground on the fuel return valve solenoid for first level cooling or on associated electrical harness.
   (1) If the test does not give the maintenance message J7, FRV(SOL 1), ECU or if the fault is repetitive:
  • Inspect the harness J7 and associated connectors to the fuel return valve and ECU for sign of looseness, damage or contamination ASM 732518.
    Pay particular attention on pins 4 and 5 at the connector to the ECU and at pins 1 and 2 at the connector to the fuel return valve.
  • Re-tighten, clean or replace harness as required.
     (a) If no defect is found either or on the harness or the connector no further action is due.
     (b) If the fault continues or is repetitive:
     (c) If the fault continues:
     (d) If the fault continues:
   (2) If the test gives the maintenance message J7, FRV(SOL 1), ECU:
  • disconnect the harness J7 from the ECU.
  • do a visual inspection of the harness connector and receptacle. Look for contamination or oxidation or pins that have damage.
  • if you find damage, repair or replace as required.
  • clean the connector and receptacle with a BRUSH - BRISTLED and stoddard solvent (Material No.CP2011) AMM 73-21-50-210-002.
  • do a resistance check of the harness J7 between:
    . pins 4 and 5 (18 to 38 ohms)
    . pins 4 and 1 (> 10 megohms)
    . pin 4 and the ground (> 10 megohms).
     (a) If the resistance values are in the specified limits:
     (b) If the resistance values are out of the specified limits:
  • disconnect the harness J7 from the fuel return valve.
  • do a visual inspection of the harness connector and receptacle. Look for contamination or oxidation or pins that have damage.
  • if you find damage, repair or replace as required.
  • clean the connector and receptacle with a BRUSH - BRISTLED and stoddard solvent (Material No.CP2011) AMM 73-21-50-210-002.
  • do a resistance check between:
    . pins 1 and 2 (18 to 38 ohms)
    . pin 1 and the ground (> 10 megohms)
       1 If the resistance values are out of the specified limits:
       2 If the resistance values are in the specified limits:
Subtask 73-20-00-710-209-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:41:04 UTC