R TASK 24-20-00-810-862
R Failure of the Generator 1 Channel R 1. Possible Causes
_______________
R - GLC-1 (9XU1) R - BTC-1 (11XU1) R - feeders
R 2. Job Set-up Information
______________________ R A. Fixtures, Tools, Test and Support Equipment R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION R -------------------------------------------------------------------------------R No specific circuit breaker(s) safety clip(s)
R B. Referenced Information R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 24-22-55-000-001 R AMM 24-22-55-400-002 R 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 24-22/01 R ASM 24-22/02
R 3. Fault Confirmation
__________________
R A. Job Set-Up Removal of the Contactors (9XU1, 9XU2, 11XU1, 11XU2) Installation of the Contactors (9XU1, 9XU2, 11XU1, 11XU2) 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 (1) Make sure that the aircraft electrical circuits are de-energized. R (2) Do not start the engines.
R B. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION
R -------------------------------------------------------------------------------R 123VU BUS 1/131XP-A/SPLY 5XN1 AB12
R 123VU BUS 1/103XP/SPLY 3XN1 AB11
R 123VU TR1/SPLY 2PU1 AB10
R 123VU AC ESS/BUS ON/BUS 1 1XC AC12
R 123VU BUS 1/101XP/SPLY 1XN1 AD11
R 123VU AVNCS VENT/BLOWER/FAN 1HQ AD10
R 123VU BUS 1/110XP/SPLY 7XN1 AF11
R 123VU ANTI ICE/L/WHSLD 1DG1 AF10
R C. Test
R Not applicable.
R NOTE : As the GEN 1 was set to OFF because of a true failure, the fault
____ R confirmation is not necessary.
R 4. Fault Isolation
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R A. If the fault symptom is identified by the CFDS message DELTA CURRENT GEN1 R CHANNEL or OVERCURRENT GEN1 CHANNEL and the upper ECAM-DU warnings GEN 1 R FAULT and AC BUS 1 FAULT: R - do a check of the feeders (Ref. ASM 24-22/01) for a short circuit or a R short to ground between:
R . pin L1 of the Current Transformer Assembly (CTA) (51XU1) and terminal R D of the GLC 1 (9XU1)
R . pin L2 of the CTA and terminal E of the GLC 1
R . pin L3 of the CTA and terminal F of the GLC 1.
R (1) If the feeders are not correct:
R - repair or replace the feeders as necessary.
R (2) If the feeders are correct:
R - do a check of the power distribution feeders (Ref. ASM 24-22/02)
R for a short circuit or a short to ground between:
R . terminals G, H and J of the GLC 1 and the primary circuit R breakers of bus 1XP
R . terminal M of the GLC 1 and terminal D of the BTC 1
R . terminal L of the GLC 1 and terminal E of the BTC 1
R . terminal K of the GLC 1 and terminal F of the BTC 1
R . terminals R, P and N of the GLC 1 and the lightning strike R protection module (19XU1).
R (a) If the feeders are not correct:
R - repair or replace the feeders as necessary.
R (b) If the feeders are correct:
R - replace the GLC-1 (9XU1) (Ref. AMM TASK 24-22-55-000-001) and
R (Ref. AMM TASK 24-22-55-400-002).
「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 : 401-499, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page A249
Aug 01/05 CES
R 1_ If the fault continues:
R - replace the BTC-1 (11XU1) (Ref. AMM TASK 24-22-55-000-001)
R and (Ref. AMM TASK 24-22-55-400-002).
R B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
R breaker(s):
R 1XN1, 7XN1, 3XN1, 5XN1, 1XC, 1DG1, 1HQ, 2PU1
R C. Do this operational test to make sure that the system operates correctly.
R (1) Aircraft Maintenance Configuration
R (a) Energize the aircraft electrical circuits 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 2(11)
