(1) Aircraft Maintenance Configuration

 (a) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).

 (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).

 (2) On the ELEC panel 35VU:

 - push, release and push again the GEN 1 pushbutton switch (3XU1).

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

 (4) Start the engine 1 (Ref. AMM TASK 71-00-00-710-003).

 C. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the ECAM control panel:  On the lower ECAM display unit:
 - push the ELEC key to get the ELEC  - the correct electrical parameters of
 page.  GEN 1 are shown and the AC 1 busbar is supplied by the GEN 1.
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 (1) Stop the engine 1 (Ref. AMM TASK 71-00-00-710-028).

 (2) Do the EIS stop procedure
 (Ref. AMM TASK 31-60-00-860-002).

 (3) De-energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-862-002).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page A221
 201-299, 301-399, Aug 01/05 CES

 TASK 24-20-00-810-848

 Low Oil Pressure of the IDG 2
 1. Possible Causes
_______________
 - IDG (4000XU)

 - EGIU-2 (22XU2)

 - GCU-2 (1XU2)
 - oil cooler

 - tubings
 - oil filter

 - wiring

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-21-00-810-816

AMM  12-13-24-612-041 
AMM  12-13-24-680-040 
AMM  24-21-00-210-044 
AMM  24-21-00-210-046 
AMM  24-21-00-210-047 
AMM  24-21-49-000-003 
AMM  24-21-49-000-004 
AMM  24-21-49-400-003 
AMM  24-21-49-400-004 
AMM  24-21-51-000-040 
AMM  24-21-51-000-041 
AMM  24-21-51-400-040 
AMM  24-21-51-400-041 
AMM  24-22-33-000-001 
AMM  24-22-33-400-002 
AMM  24-22-34-000-001 
AMM  24-22-34-400-001 
AMM  24-41-00-740-002 
AMM  24-41-00-861-002 

The Differential Pressure Indicator (DPI) of the IDG2 Oil Filter is Extended - Alternate ProcedureIDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level CheckDraining of the Oil from the IDGInspection of the Filter Element(s)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 CircuitsRemoval of the IDG Cooling Oil-in Tubes and HosesRemoval of the IDG Cooling Oil-out Tubes and HosesInstallation of the IDG Cooling Oil-in Tubes and HosesInstallation of the IDG Cooling Oil-out tubes and HosesRemoval of the Integrated Drive Generator -IDG 1(2),(4000XU)Removal of the IDG Oil Filter(s)Installation of the Integrated Drive Generator -IDG 1(2),(4000XU)Installation of the IDG Oil Filter(s)Removal of the EGIU-1(2) (22XU1, 22XU2)Installation of the EGIU-1(2) (22XU1, 22XU2)Removal of the GCU-1(2) (1XU1, 1XU2)Installation of the GCU-1(2) (1XU1, 1XU2)Operational Test of the Ground power Control Unit (GPCU)Energize the Aircraft Electrical Circuits from the External Power
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page A222
 201-299, 301-399, Aug 01/05 CES

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 71-00-00-710-003 Engine Automatic Start AMM 71-00-00-710-028 Engine Shutdown AMM 73-11-60-000-002 Removal of the Integrated Drive Generator (IDG) Oil
　
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