EIU-2 Fault to Supply EEC B

TASK 73-25-00-810-A70-A
EIU-2 Fault to Supply EEC B

1. Possible Causes

EIU-2 [1KS2]
aircraft wiring
HARNESS-FAN, WF01 [4217KS]

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	PLIERS - JAWED, SOFT
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER

B. Referenced Information

REFERENCE	DESIGNATION
AMM 73-21-61-000-802	Removal of the Electronic Engine Control (EEC) Wiring Harness (WF01)
AMM 73-21-61-400-802	Installation of the Electronic Engine Control (EEC) Wiring Harness (WF01)
AWM 732504
AMM 73-25-34-000-802	Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-802	Installation of the Engine Interface Unit (EIU)
AMM 73-25-34-710-802	Operational Test of the Engine Interface Unit (EIU) with the Centralized Fault Display System (CFDS)

3. Fault Confirmation
Subtask 73-25-00-710-509-A ** ON A/C NOT FOR ALL

A. Do the operational test of the Engine Interface Unit (EIU) with the Centralized Fault Display System (CFDS) to confirm this fault AMM 73-25-34-710-802.

4. Fault Isolation
Subtask 73-25-00-810-358-A ** ON A/C NOT FOR ALL

A. If there is confirmation of the fault:
(1) Replace EIU-2 [1KS2] AMM 73-25-34-000-802 and AMM 73-25-34-400-802.
(2) Do the test given in Para. 3.
(3) If the fault continues:
(a) Troubleshoot as follows:

Subtask 73-25-00-865-104-A ** ON A/C NOT FOR ALL

B. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VU	ENGINE/ENG2/FADEC B/AND EIU 2	4KS2	Q40

Subtask 73-25-00-810-359-A ** ON A/C NOT FOR ALL

C. Check for harness fault.
(1) Use a PLIERS - JAWED, SOFT to disconnect connector (P403) and check for 28 VDC at pin 21 of connector (403VC2).
(2) If there is 28 VDC at pin 21 of connector (403VC2):
(a) Repair or replace aircraft wiring AWM 732504.
(b) Do the test given in Para. 3.
(3) If there is not 28 VDC:
(a) Replace HARNESS-FAN, WF01 [4217KS] AMM 73-21-61-000-802 and AMM 73-21-61-400-802.
(b) Do the test given in Para. 3.
(4) If necessary, connect connector (P403).

5. Close-up
Subtask 73-25-00-860-127-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.

Subtask 73-25-00-865-105-A ** ON A/C NOT FOR ALL

B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2)
121VU	ENGINE/ENG2/FADEC B/AND EIU 2	4KS2	Q40

[Rev.8 from Aug 2018] 2026.04.04 04:36:46 UTC