R (1) If the fault continues:
R - do a check of the external power feeders (Ref. ASM 24-41/01) for a
R correct phase connection between:
R . terminal A of the external power receptacle (20XG) and terminal K
R of the EPC (3XG)
R . terminal B of the external power receptacle and terminal L of the
R EPC
R . terminal C of the external power receptacle and terminal M of the
R EPC.
R (a) If the feeders are not correct:
R - connect the feeders as necessary to get the correct phase
R sequence.
R (b) If the feeders are correct:
R - do a check of the Point-Of-Regulation (POR) sense wiring (Ref.
R ASM 24-41/01) for a correct phase connection between:
R . terminal J of the EPC (3XG) and pin B/15J of the GAPCU (phase
R A)
R . terminal H of the EPC and pin B/14J of the GAPCU (phase B)
R . terminal G of the EPC and pin B/13J of the GAPCU (phase C).
R 1 If the wiring is not correct:_
R - connect the wiring as necessary to get the correct phase
R sequence.
R 2 If the wiring is correct and the fault continues:_
R - replace the external power source.
R B. Make sure that the aircraft electrical circuits operate correctly in
R external power configuration.
R (1) Energize the Aircraft Electrical Circuits from the external power
R (Ref. AMM TASK 24-41-00-861-002).
R (2) De-energize the aircraft electrical circuits from the external power
R (Ref. AMM TASK 24-41-00-862-002).
R TASK 24-41-00-810-824 R Failure of the APU Generator Feeders or APU Generator POR-Wiring R 1. Possible Causes
_______________
R - GAPCU (24XG) R - wiring R - feeders
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 24-41-00-861-002 R R AMM 24-41-00-862-002 R R AMM 24-41-34-000-001 R R AMM 24-41-34-400-001 R R ASM 24-23/01
R 3. Fault Confirmation
__________________
R A. Test
R Not applicable.
Energize the Aircraft Electrical Circuits from the APU De-energize the Aircraft Electrical Circuits Supplied from the APU Removal of the Ground Auxiliary Power Control Unit (GAPCU) (24XG) Installation of the Ground Auxiliary Power Control Unit (GAPCU) (24XG)
R NOTE : As the APU GEN was set to OFF because of a true failure, the fault
____ R confirmation is not necessary.
R 4. Fault Isolation
_______________
R A. If the fault symptom is identified by the CFDS message WRG: POR/ WRG: APU
R GEN FEEDER/ GAPCU (24XG) and the upper ECAM-DU warning APU GEN FAULT:
R - do a check of the Point-Of-Regulation (POR) sense wiring (Ref. ASM 24-R 23/01) for a correct phase connection between:
R . terminal F of the APU GLC (3XS) and pin A/14G of the GAPCU (phase A)
R . terminal E of the APU GLC and pin A/15H of the GAPCU (phase B)
R . terminal D of the APU GLC and pin A/15G of the GAPCU (phase C).
R (1) If the wiring is not correct:
R - connect the wiring as necessary to get the correct phase sequence.
「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, ∞∞24-41-00∞∞∞∞∞∞∞∞∞∞Page 246
Aug 01/05 CES
R (2) If the wiring is correct:
R - do a check of the APU generator feeders (Ref. ASM 24-23/01) for a
R correct phase connection between:
R . terminal T1 of the APU generator and terminal F of the APU GLC
R (3XS)
R . terminal T2 of the APU generator and terminal E of the APU GLC
R . terminal T3 of the APU generator and termianl D of the APU GLC.
R (a) If the wiring is not correct:
R - connect the wiring as necessary to get the correct phase
R sequence.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 3(109)
