Failure of the IDG 1 Servo Valve or its Wiring
TASK 24-20-00-810-876-A
Failure of the IDG 1 Servo Valve or its Wiring
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Isolation
Subtask 24-20-00-860-130-E ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:17 UTC
Failure of the IDG 1 Servo Valve or its Wiring
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-41-00-740-002 | Operational Check of the GAPCU via the CFDS |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| AMM 31-60-00-860-001 | EIS Start Procedure |
| AMM 31-60-00-860-002 | EIS Stop Procedure |
| AMM 71-00-00-860-814 | Shutdown of the Engine |
| AMM 71-00-00-860-823 | Start the Engine (Normal Automatic Start) |
CAUTION:
BEFORE YOU START THE CHECK OF IDG WIRING THAT INCLUDES CONNECTORS, EXAMINE EACH CONNECTOR TO MAKE SURE THAT THERE IS NO CONTAMINATION IN IT.
IF YOU FIND CONTAMINATION, CLEAN THE CONNECTOR AND CONNECT IT AGAIN.
IF THE FAILURE CONTINUES, DO THE TROUBLE SHOOTING PROCEDURE AS GIVEN BELOW.
Subtask 24-20-00-710-103-C ** ON A/C NOT FOR ALL A. Do this operational test to make sure that the system operates correctly.
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(2) In the cockpit, on the ELEC panel 35VU:
(4) Start engine 1 AMM 71-00-00-860-823.
(5) Do this test:
4. Close-up(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(2) In the cockpit, on the ELEC panel 35VU:
- Push, release and push again the GEN 1 pushbutton switch (3XU1).
(4) Start engine 1 AMM 71-00-00-860-823.
(5) Do this test:
| ACTION | RESULT |
|---|---|
On the ECAM control panel:
| On the lower ECAM DU:
|
Subtask 24-20-00-860-130-E ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Stop engine 1 AMM 71-00-00-860-814.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
(1) Stop engine 1 AMM 71-00-00-860-814.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.