EIU Signal Replaced
TASK 21-31-00-810-816-A
EIU Signal Replaced
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 21-31-00-710-080-A
Subtask 21-31-00-810-108-A
Subtask 21-31-00-860-065-A
[Rev.8 from Aug 2018]
2026.04.04 04:24:42 UTC
EIU Signal Replaced
1. Possible Causes
- wiring
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| ASM 213102 | |
| AMM 73-25-34-710-043 | Operational Test of the Engine Interface Unit |
Subtask 21-31-00-710-080-A
A. Not applicable, you cannot confirm this fault on the ground.
4. Fault IsolationNOTE: In the flight phases 4 and 5 the maintenance message EIU SIGNAL REPLACED shows that:
- during the take-off at least one of the throttle levers was not set to take-off power >70%.
Subtask 21-31-00-810-108-A
A. If the CPC 1 (11HL) and/or CPC 2 (12HL) CLASS 3 FAULTS gives the maintenance messsage EIU SIGNAL REPLACED (17) caused in flight phase 7 or 8, no other maintenance action is necessary.
Subtask 21-31-00-810-089-A NOTE: The fault is caused by LDG 'bouncing' or by a hard landing.
B. If the CPC 1 (11HL) CLASS 3 FAULTS gives the maintenance messsage EIU SIGNAL REPLACED (17) caused in flight phase other than 7 or 8 and,
the take off was performed with the minimum max. climb setting (throttle levers set at 70%):
(2) If the fault continues:
Subtask 21-31-00-810-090-A the take off was performed with the minimum max. climb setting (throttle levers set at 70%):
- do the operational test of the engine interface unit AMM 73-25-34-710-043.
(2) If the fault continues:
- do a check and repair the wiring between:
CPC 1 (11HL) AB/7D and EIU 1 (1KS1) AB/G1,
CPC 1 (11HL) AB/8D and EIU 2 (1KS2) AB/G1 ASM 213102.
C. If the CPC 2 (12HL) CLASS 3 FAULTS gives the maintenance messsage EIU SIGNAL REPLACED (17) caused in flight phase other than 7 or 8:
(2) If the fault continues:
Subtask 21-31-00-710-081-A - do the operational test of the engine interface unit AMM 73-25-34-710-043.
(2) If the fault continues:
- do a check and repair the wiring between:
CPC 2 (12HL) AB/8D and EIU 2 (1KS2) AB/G1,
CPC 2 (12HL) AB/7D and EIU 1 (1KS2) AB/G1 ASM 213102.
D. Do the test as given in the Para. 3.A.
5. Close-upSubtask 21-31-00-860-065-A
A. Put the aircraft back to its initial configuration.