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时间:2011-03-28 13:22来源:蓝天飞行翻译 作者:航空
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R (a) If there is no continuity:
R - replace the GLC-APU (3XS) (Ref. AMM TASK 24-23-55-000-001) and
R (Ref. AMM TASK 24-23-55-400-001).

R (b) If there is continuity:
R - do a check of the wiring of the APU GLC control-circuit (Ref.
R ASM 24-23/02) for an open circuit between:

R . pin B/10J of the GAPCU and pin C/3 of the ELEC/APU GEN R pushbutton switch (2XS)

R . pin C/1 of the ELEC/APU GEN pushbutton switch and pin X/1 of R the APU GLC auxiliary control relay (4XS)

R . pin X/2 of the APU GLC auxiliary control relay and the ground

R . pin B/10J of the GAPCU and pin A/44 of the diode module R 1164VD

R . pin A/43 of the diode module 1164VD and pin A/D3 of the EPC R auxiliary control relay (5XG)

R . pin A/D2 of the EPC auxiliary control relay and pin B/10 of R the GLC 1

R . pin A/D2 of the EPC auxiliary control relay and pin B/8 of R the BTC 1

R . pin B/12 of the GLC 1, pin B/6 of the BTC 1, pin B/12 of the R GLC 2 and pin B/18 of the BTC 2

R . pin B/10 of the GLC 2 and pin A/C2 of the EPC auxiliary R control relay

R . pin B/20 of the BTC 2 and pin A/C2 of the EPC auxiliary R control relay

R . pin A/C3 of the EPC auxiliary control relay and pin A/B2 of R the APU GLC auxiliary control relay (4XS)

R . pin A/B1 of the APU GLC auxiliary control relay and pin B/24 R of the EPC (3XG)

R . pin B/22 of the EPC and pin B/3 of the APU GLC (3XS)


 「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, ∞∞24-23-00∞∞∞∞∞∞∞∞∞∞Page 239
 Aug 01/05 CES


R  . pin B/5 of the APU GLC and ground. 
R  - do a check of the contacts of the contactors and relays of the 
R  APU GLC control circuit (Ref. ASM 24-23/02) for correct 
R  operation. 
R  1_  If the wiring or the contacts do not operate correctly:
R  - repair or replace the wiring as necessary 
R  - replace the RELAY-APU GLC AUX CTL (4XS) as necessary 
R  - replace the RELAY-EPC AUX CTL (5XG) as necessary 
R  - replace the GLC-1 (9XU1), the GLC-2 (9XU2), the BTC-1 
R  (11XU1) or the BTC-2 (11XU2) (Ref. AMM TASK 24-22-55-000-
R  001) and (Ref. AMM TASK 24-22-55-400-002) as necessary. 
R  2_  If the wiring or the contacts operate correctly:
R  - replace the GAPCU (24XG) (Ref. AMM TASK 24-41-34-000-001) 
R  and (Ref. AMM TASK 24-41-34-400-001). 
R  C. Do the test given in para. 3.

 

R  TASK 24-23-00-810-819 
R  Failure of the Neutral-To-Phase System of the APU Generator or the Neutral 
R  Feeder 
R  1. Possible Causes_______________ 
R  - GEN-APU (8XS) 
R  - wiring 
R  2. Job Set-up Information______________________ 
R  A. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------

R  AMM  24-23-51-000-001 
R  AMM  24-23-51-400-001 
R  AMM  24-41-00-861-002 

R  AMM  24-41-00-862-002 

R  ASM  24-23/01 

R 3. Fault Confirmation
__________________
R A. Test
R Not applicable.

Removal of the APU Generator 8XS Installation of the APU Generator 8XS Energize the Aircraft Electrical Circuits from the APU De-energize the Aircraft Electrical Circuits Supplied from the APU
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: FEEDER
R NEUTRAL/ GEN APU (8XS) and the upper ECAM-DU warning APU GEN FAULT:
R - do a check of the wiring of the APU generator neutral-feeder for an
R open circuit or a high resistance condition between the terminal N of
R the APU generator and the airframe ground (Ref. ASM 24-23/01).

R (1) If the wiring is not correct:
R - repair or replace the neutral feeder as necessary.

R (2) If the wiring is correct:
R - do a check of the resistance of the neutral-to-phase connections
R (Ref. ASM 24-23/01) of the APU generator between:

R . terminal T1 and N (9.35 milliohms plus or minus 1.25 milliohms)

R . terminal T2 and N (9.35 milliohms plus or minus 1.25 milliohms)

R . terminal T3 and N (9.35 milliohms plus or minus 1.25 milliohms).
 
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