R (2) On the ELEC panel 35VU:
R - push, release and push again the GEN 2 pushbutton switch (3XU2).

R (3) Do the operational test of the GAPCU (Ref. AMM TASK 24-41-00-740-R 002).

R (4) Start the engine 2 (Ref. AMM TASK 71-00-00-710-003).

R (5) Do this test:

R -------------------------------------------------------------------------------R ACTION RESULT
R -------------------------------------------------------------------------------
R On the ECAM control panel: On the lower ECAM DU:
R - get the ELEC page. - the correct electrical parameters of
R the GEN 2 are shown and the AC2
R busbar is supplied by the GEN 2.

R 5. Close-up

________ R A. Put the aircraft back to its initial configuration. R (1) Stop the engine 2 (Ref. AMM TASK 71-00-00-710-028). R (2) Do the EIS stop procedure
R (Ref. AMM TASK 31-60-00-860-002).
R (3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY
R potentiometers to OFF.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 401-499, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page B255
 Aug 01/05 CESR (4) De-energize the aircraft electrical circuits R (Ref. AMM TASK 24-41-00-862-002).

R TASK 24-20-00-810-906

R IDG 1 Manual Disconnect R 1. Possible Causes
_______________
R - IDG (4000XU)
R - GCU-1 (1XU1)
R - P/BSW-ELEC/IDG 1 (5XT)
R - wiring

R 2. Job Set-up Information

______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 12-13-24-612-041 R R AMM 24-21-00-210-046 R R AMM 24-21-00-210-047 R R AMM 24-21-00-720-041 R R AMM 24-21-51-000-040 R R AMM 24-21-51-400-040 R R AMM 24-22-34-000-001 R AMM 24-22-34-400-001 R AMM 24-41-00-740-002 R AMM 24-41-00-861-002 R R AMM 24-41-00-862-002 R R AMM 31-60-00-860-001 R AMM 31-60-00-860-002 R AMM 71-00-00-710-003 R AMM 71-00-00-710-028 R ASM 24-21/01
R 3. Fault Confirmation
__________________
R A. Test
R Not applicable.

IDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check Check of the Oil Level and Oil-Filter Differential-Pressure Indicator (DPI) Visual Inspection of the IDG for Oil Leaks and Check of the Electrical Circuits Operational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine in Operation Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) Installation of the Integrated Drive Generator -IDG 1(2),(4000XU) Removal of the GCU-1(2) (1XU1, 1XU2) Installation of the GCU-1(2) (1XU1, 1XU2) Operational Check of GAPCU via CFDS Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power EIS Start Procedure EIS Stop Procedure Engine Automatic Start Engine Shutdown
R NOTE : As the GEN 1 was set to off because of a true fault, the fault
____ R confirmation is not necessary.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 401-499, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page B257
 Aug 01/05 CES

R 4. Fault Isolation
_______________

R A. If the fault symptom is identified by the maintenance message IDG1 R (E1-4000XU) MANUAL DISCONNECT and by the upper ECAM-DU warnings IDG 1 OIL R LO PR or IDG 1 OIL OVHT:
R NOTE : You can find this message with other CFDS fault messages. First,
____ R do the trouble shooting for all the other CFDS fault message.
R (1) Read the flight log book and the maintenance log book to identify the
R cause of the IDG disconnect.

R (2) If there is no cause or if the cause is unknown:
R - do a check of the Differential Pressure Indicator (DPI) of the IDG
R 1 (Ref. AMM TASK 24-21-00-210-046),
R - do a check of the scavenge filter and charge filter (if installed).

R (a) If the DPI is extended:
R - replace the engine 1 IDG (4000XU) (Ref. AMM TASK 24-21-51-000-R 040) and (Ref. AMM TASK 24-21-51-400-040).

R (b) If the DPI is not extended:
R - do a visual check of the IDG 1 oil level (Ref. AMM TASK 24-21-R 00-210-046).

R  1_  If the oil level is not correct:
R  - do a visual inspection of the IDG 1 for oil leaks (Ref. AMM 
R  TASK 24-21-00-210-047). 

R a_ If you find leaks:
R - repair or replace the components as necessary to remove
R the oil leaks.

R b_ If you find no leaks:
R - add oil (Ref. AMM TASK 12-13-24-612-041)
R - connect the IDG 1 (if disconnected)
R - do a dynamic disconnect test of the IDG 1 (Ref. AMM TASK
　
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