「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, ∞∞24-21-00∞∞∞∞∞∞∞∞∞∞Page 263
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R (3) Do an electrical resistance test of the IDG 1 exciter field between
R pins A/9 and A/10 (8.4 ohms plus or minus 0.84 ohm) (Ref. ASM 24-R 22/01).
R (a) If the resistance values are out of the specified limits:
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 resistance values are in the specified limits:
R - do an electrical resistance test of the IDG 1 PMG stator (Ref.
R ASM 24-22/01) between:
R . pins B/12 and B/13 (1 ohm plus or minus 0.05 ohm)
R . pins B/12 and B/14 (1 ohm plus or minus 0.05 ohm)
R . pins B/13 and B/14 (1 ohm plus or minus 0.05 ohm).
R 1_ If the resistance values are out of the specified limits:
R - replace the engine 1 IDG (4000XU) (Ref. AMM TASK 24-21-51-
R 000-040) and (Ref. AMM TASK 24-21-51-400-040).
R 2_ If the resistance values are in the specified limits:
R - do a check of the wiring of the PMG stator and exciter field
R (Ref. ASM 24-22/01) for a short to ground, a short circuit
R or an open circuit between:
R . pin B/12 of the IDG 1 and pin C/10 of the GCU 1
R . pin B/13 of the IDG 1 and pin C/11 of the GCU 1
R . pin B/14 of the IDG 1 and pin C/9 of the GCU 1
R . pins C/10, C/11, C/9 and C/7 of the GCU 1 (short to shield R of the PMG stator)
R . pin A/9 of the IDG 1 and pin C/12 of the GCU 1
R . pin A/10 of the IDG 1 and pin C/13 of the GCU 1
R . pins C/12, C/13 and pin C/7 of the GCU 1 (short to shield R of the exciter field).
R a_ If the wiring is not correct:
R - repair or replace as necessary.
R b_ If the wiring is correct:
R - replace the GCU-1 (1XU1) (Ref. AMM TASK 24-22-34-000-001)
R and (Ref. AMM TASK 24-22-34-400-001).
R B. Do this operational test to make sure that the system operates correctly.
R (1) Aircraft Maintenance Configuration
R (a) Energize the aircraft electrical circuits
R (Ref. AMM TASK 24-41-00-861-002).
R (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
R (Ref. AMM TASK 31-60-00-860-001).
R (2) On the ELEC panel 35VU:
R - push, release and push again the GEN 1 pushbutton switch (3XU1).
「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, ∞∞24-21-00∞∞∞∞∞∞∞∞∞∞Page 264
Aug 01/05 CES
R (3) Do the operational test of the GAPCU (Ref. AMM TASK 24-41-00-740-
R 002).
R (4) Start the engine 1 (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 1 are shown and the AC1
R busbar is supplied by the GEN 1.
R 5. Close-up________
R A. Put the aircraft back to its initial configuration.
R (1) Stop the engine 1 (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.
R (4) De-energize the aircraft electrical circuits
R (Ref. AMM TASK 24-41-00-862-002).
R TASK 24-21-00-810-827
R Failure of the IDG 2 Control Circuits or of its Wiring to the GCU 2 R 1. Possible Causes
_______________
R - IDG (4000XU) R - GCU-2 (1XU2) R - wiring
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION 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 ASM 24-22/01
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 2(120)
