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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  (b) If the wiring is correct: 
R  - replace the GAPCU (24XG) (Ref. AMM TASK 24-41-34-000-001) and 
R  (Ref. AMM TASK 24-41-34-400-001). 
R  B. Make sure that the aircraft electrical circuits operate correctly in APU 
R  configuration. 
R  (1) Energize the aircraft electrical circuits from the APU (Ref. AMM TASK 
R  24-41-00-861-002). 
R  (2) Let the APU generator operate for five minutes to make sure that it 
R  operates correctly. 
R  (3) De-energize the aircraft electrical circuits from the APU (Ref. AMM 
R  TASK 24-41-00-862-002).

 

R TASK 24-41-00-810-825 R Failure of the ARINC 429 Bus betwwen the GAPCU and the CFDIU R 1. Possible Causes
_______________
R - GAPCU (24XG) R - wiring R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 24-41-00-740-002 R AMM 24-41-34-000-001 R R AMM 24-41-34-400-001 R R ASM 24-41/01
R 3. Fault Confirmation
__________________
R A. Test Operational Check of GAPCU via CFDS Removal of the Ground Auxiliary Power Control Unit (GAPCU) (24XG) Installation of the Ground Auxiliary Power Control Unit (GAPCU) (24XG)
R (1) Read the Class 3 Faults of the GAPCU (Ref. AMM TASK 24-41-00-740-R 002).
R 4. Fault Isolation
_______________
R A. If the Class 3 Faults gives the maintenance message CFDIU(1TW)/GAPCU
R (24XG):

R (1) Do the trouble shooting for chapter 31 or CFDIU messages that come
R into view with this message.

R (2) If there are no chapter 31 or CFDIU messages or if the fault
R continues after the trouble shooting :
R - do a check of the wiring of the ARINC 429 bus (Ref. ASM 24-41/01)
R for an open circuit, a short circuit, a short to ground or a short
R to shield between:

R . pin A/7E of the GAPCU and pin B/11E of the CFDIU (1TW)

R . pin A/8E of the GAPCU and pin B/11D of the CFDIU

R . pins A/7E and A/9E of the GAPCU

R . pins A/8E and A/9E of the GAPCU.


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

 「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 248
 Aug 01/05 CES


R  (b) If the wiring is correct: 
R  - replace the GAPCU (24XG) (Ref. AMM TASK 24-41-34-000-001) and 
R  (Ref. AMM TASK 24-41-34-400-001). 
R  B. When you replace a component or repair the wiring: 
R  - do the subsequent flight before you do the check of the Class 3 Faults 
R  of the GAPCU from the CFDS to make sure that the system operates 
R  correctly. 
R  If the test continues to give the fault message, continue the trouble 
R  shooting procedure.

 

R  TASK 24-41-00-810-826 
R  Impossibility to Connect the External Power on the Aircraft 
R  1. Possible Causes_______________ 
R  - GAPCU (24XG) 
R  - wiring 
R  2. Job Set-up Information______________________ 
R  A. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------

R  AMM  24-41-00-861-002 

R  AMM  24-41-00-862-002 

R  AMM  24-41-34-000-001 

R  AMM  24-41-34-400-001 

R  ASM  24-41/01 

R 3. Fault Confirmation
__________________ R A. Job Set-up
Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the Ground Auxiliary Power Control Unit (GAPCU) (24XG) Installation of the Ground Auxiliary Power Control Unit (GAPCU) (24XG)
R (1) Energize the aircraft electrical circuits from the external power
R (Ref. AMM TASK 24-41-00-861-002).

R B. Test

R (1) If on the POWER CENTER-AC/DC EMERGENCY panel 106VU, the AVAIL legend
R of the ELEC/EXT PWR pushbutton switch (10XG) is on and the EXT
R PWR/AVAIL caution light (9XG) is on:
R - do the trouble shooting given in the Para. 4.A.

R (2) If on the POWER CENTER-AC/DC EMERGENCY panel 106VU, the AVAIL legend
 
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