W DOC AIRBUS | TSM A320F

Loss of the Oil Temperature Signal from Sensor 4004EN or Disagree with Oil Temperature Signal from ECU Oil Temperature Sensor on Engine 2


TASK 79-32-00-810-822-A
Loss of the Oil Temperature Signal from Sensor 4004EN or Disagree with Oil Temperature Signal from ECU Oil Temperature Sensor on Engine 2


1. Possible Causes
  • SENSOR-OIL TEMP [4004EN]
  • aircraft wiring
  • EIU-2 [1KS2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 71-51-43-000-001
Removal of the Left Side Harness
AMM 71-51-43-400-001
Installation of the Left Side Harness
AMM 73-25-34-000-040
Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-040
Installation of the Engine Interface Unit (EIU)
AMM 73-25-34-710-040
Operational Test of the Engine Interface Unit
AMM 79-32-15-000-041
Removal of the Oil Temperature Sensor (Engine Condition Monitoring Sensor)
AMM 79-32-15-400-041
Installation of the Oil Temperature Sensor (Engine Condition Monitoring Sensor)
ASM 793601
3. Fault Confirmation
Subtask 79-32-00-710-092-A ** ON A/C NOT FOR ALL
A. Not applicable.
4. Fault Isolation
Subtask 79-32-00-810-075-A ** ON A/C NOT FOR ALL
A. Procedure.
NOTE: The fault is triggered if the oil temperature sensor (4004EN) indicates a temperature greater than 140 deg. C while the ECU temperature sensor indicates a temperature in between - 55 deg. C and 135 deg. C. This is indicative of a faulty output of oil temperature sensor (4004EN).
   (1) Check carrefully electrical connector at the oil temperature sensor (4004EN) for looseness, damaged pins or contamination.
     (a) If damage is found:
  • repair or replace as necessary.
     (b) If nothing is found:
   (2) If the fault continues:
  • do a check of the aircraft wiring between the oil temperature sensor (4004EN) and the EIU (1KS2) for open or short to ground ASM 793601 pin AA/1 to pin AA/10F. Pay particular attention to engine to pylon connectors 4005VC-A, 405VC-A, 4006VC-A and 406VC-A and to ground wire connections (9951DC, 9956DC and 9957DC) on Engine Fan Case (check for looseness or contamination).
     (a) if damage is found:
     (b) if nothing is found:
Subtask 79-32-00-710-093-A ** ON A/C NOT FOR ALL
B. Do the operational test of the Engine Interface Unit (EIU) through the CFDS AMM 73-25-34-710-040.
   (1) Check that failure message ECU2 4000KS OR OIL TEMP SENSOR 2 4004EN is no longer present.
[Rev.8 from Aug 2018] 2026.04.04 04:38:23 UTC