W DOC AIRBUS | TSM A320F

Failure of the T/R Inhibition System on Engine 2


TASK 73-25-00-810-870-A
Failure of the T/R Inhibition System on Engine 2


1. Possible Causes
  • RELAY-THRUST REV INHIBITION, ENG 2 [14KS2]
  • EIU-2 [1KS2]
  • wiring from the EIU-2 (1KS2) to the engine 2 thrust reverser inhibition relay (14KS2)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 732516
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 73-25-34-710-043
Operational Test of the Engine Interface Unit
3. Fault Confirmation
Subtask 73-25-00-710-200-A ** ON A/C NOT FOR ALL
A. Test
Do the operational test of the engine interface unit through the CFDS AMM 73-25-34-710-040.
Subtask 73-25-00-710-200-B ** ON A/C NOT FOR ALL
A. Test
Do the operational test of the engine interface unit through the CFDS AMM 73-25-34-710-043.
4. Fault Isolation
Subtask 73-25-00-810-125-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message CHECK 14KS2 RELAY CIRCUIT OR EIU 2:
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring from the EIU-2 (1KS2) to the engine 2 thrust reverser inhibition relay (14KS2) pin AB/10A to pin X of the relay ASM 732516 and ASM 732516.
Subtask 73-25-00-710-201-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:35:45 UTC