ICU A and B Supplies Fault on EIU-2
TASK 73-25-00-810-A17-A
ICU A and B Supplies Fault on EIU-2
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Fault Confirmation
Subtask 73-25-00-710-454-A ** ON A/C NOT FOR ALL
Subtask 73-25-00-810-281-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:36:27 UTC
ICU A and B Supplies Fault on EIU-2
1. Possible Causes
- EIU-2 [1KS2]
- aircraft wiring
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| REFERENCE | DESIGNATION |
|---|---|
| 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) |
| AWM 783605 |
Subtask 73-25-00-710-454-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 IsolationSubtask 73-25-00-810-281-A ** ON A/C NOT FOR ALL
A. If there is confirmation of the fault:
(1) Check on report for any failure of normal BUS bar (202PP) and (204PP).
(a) Troubleshoot as necessary (Ref. TSM Chap. 24).
(b) Do the test given in Para. 3.
(c) If no fault regarding the BUS bar is reported or if fault continues, go to the Para. 4.C.
Subtask 73-25-00-865-067-A ** ON A/C NOT FOR ALL (1) Check on report for any failure of normal BUS bar (202PP) and (204PP).
(a) Troubleshoot as necessary (Ref. TSM Chap. 24).
(b) Do the test given in Para. 3.
(c) If no fault regarding the BUS bar is reported or if fault continues, go to the Para. 4.C.
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 73-25-00-810-282-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENG 2) | |||
| 121VU | ICU B/ENG2 PWR SPLY | 101KS2 | R43 |
| 121VU | ICU A/ENG2 PWR SUPPLY | 22KS2 | R40 |
C. If no fault regarding the BUS bar is reported or if fault continues:
(1) Remove EIU-2 [1KS2] AMM 73-25-34-000-802.
(2) Close both circuit breakers. Refer to the Para. 4.D.
(3) Check for 28 VDC at pins 13A and 13C of connector AB on 85VU.
(4) Open both circuit breakers. Refer to the Para. 4.B.
(5) If any damage found:
(a) Repair or replace aircraft wiring AWM 783605.
(6) If no problem is found or if fault continues:
(a) Replace EIU-2 [1KS2] AMM 73-25-34-400-802.
(b) Make sure that the both circuit breakers are closed. Refer to the Para. 4.D.
(c) Do the test given in Para. 3.
Subtask 73-25-00-865-069-A ** ON A/C NOT FOR ALL (1) Remove EIU-2 [1KS2] AMM 73-25-34-000-802.
(2) Close both circuit breakers. Refer to the Para. 4.D.
(3) Check for 28 VDC at pins 13A and 13C of connector AB on 85VU.
(4) Open both circuit breakers. Refer to the Para. 4.B.
(5) If any damage found:
(a) Repair or replace aircraft wiring AWM 783605.
(6) If no problem is found or if fault continues:
(a) Replace EIU-2 [1KS2] AMM 73-25-34-400-802.
(b) Make sure that the both circuit breakers are closed. Refer to the Para. 4.D.
(c) Do the test given in Para. 3.
D. 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 | ICU B/ENG2 PWR SPLY | 101KS2 | R43 |
| 121VU | ICU A/ENG2 PWR SUPPLY | 22KS2 | R40 |