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

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

 B. Test

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: On the lower ECAM DU:
 - push the ELEC key to get the  - the frequency parameter of the IDG1 ELEC page. is amber.
 NOTE : In normal operation, the color
____ of the IDG frequency parameter is green.
 4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 A. If the test confirms the fault:
 - replace the EGIU-1 (22XU1) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
 (1) If the IDG1 frequency parameter stays amber:
 (a) The frequency parameter value is out of the 390Hz-410Hz range:
 - adjust the IDG1 frequency (Ref. AMM TASK 24-21-00-730-040).
 1 If the IDG1 frequency parameter stays amber:
_
 - replace the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040).
 (b) The frequency parameter value is out of the 363Hz-433Hz range:
 - replace the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040).
R **ON A/C 401-499,

R A. If the test confirms the fault:
R - replace the GCU-1 (1XU1) (Ref. AMM TASK 24-22-34-000-001) and (Ref. AMM
R TASK 24-22-34-400-001).

R (1) The frequency parameter value stays amber:
R - replace the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref.
R AMM TASK 24-21-51-400-040).

R **ON A/C ALL

 B. Do the test given in para. 3.
 「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 : ALL ∞∞24-21-00∞∞∞∞∞∞∞∞∞∞Page 222
 Aug 01/05 CES

 5. Close-up
________

 A. Put the aircraft back to its initial configuration.
 (1) Stop the engine 1 (Ref. AMM TASK 71-00-00-710-027).

 (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).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-21-00∞∞∞∞∞∞∞∞∞∞Page 223
 Aug 01/05R
 CES

 TASK 24-21-00-810-812

 The steady-state Operating Frequency of the Integrated Drive Generator (IDG2)
 is out of the 390Hz-410Hz range
 1. Possible Causes
_______________
 - EGIU-2 (22XU2)
 - IDG (4000XU) R - GCU-2 (1XU2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-21-00-730-040 System Test of the IDG Frequency (P/N 740119) AMM 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-21-51-400-040 Installation of the Integrated Drive Generator -IDG
 1(2),(4000XU)
 AMM 24-22-33-000-001 Removal of the EGIU-1(2) (22XU1, 22XU2)
 AMM 24-22-33-400-002 Installation of the EGIU-1(2) (22XU1, 22XU2)

R AMM 24-22-34-000-001 Removal of the GCU-1(2) (1XU1, 1XU2) R AMM 24-22-34-400-001 Installation of the GCU-1(2) (1XU1, 1XU2) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine 1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the Engine 1(2)
 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 71-00-00-710-027 Engine Shutdown

 3. Fault Confirmation
__________________
 A. Job Set-up
 (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).

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

 B. Test
　
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