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时间:2011-03-28 22:45来源:蓝天飞行翻译 作者:航空
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 (b) If there is no 28 VDC:


 - do a check of the ON-OFF SWITCH 3LJ and replace it if necessary.

 (2) If the fault continues:


 - do a check and repair the wiring between: ON-OFF SWITCH 3LJ pin 2 and CB 1LJ, ON-OFF SWITCH 3LJ pin 1 and SERVICE AREA LIGHT 5LJ pin 1, ON-OFF SWITCH 3LJ pin 1 and SERVICE AREA LIGHT 4LJ pin 1, SERVICE AREA LIGHT 5LJ pin 2 and GND, SERVICE AREA LIGHT 4LJ pin 2 and GND (Ref. ASM 33-31/01).
 C. Do the test as given in the Para. 3.A .
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.

 TASK 33-31-00-810-802


 Socket - No 28 VDC at the Maintenance Socket in Section 19
 1. Possible Causes
_______________
 - SOCKET

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASM 33-31/01
 3. Fault Confirmation
__________________
 A. Measure the voltage at the maintenance socket with a voltmeter.
 4. Fault Isolation
_______________
 A. If there is no 28 VDC:
 - replace the related SOCKET
 (1) If the fault continues:
 - do a check and repair the wiring between:
 SOCKET 8LJ pin + and CB 1LJ,
 SOCKET 8LJ pin N and GND,
 SOCKET 10LJ pin + and CB 1LJ,
 SOCKET 10LJ pin N and GND (Ref. ASM 33-31/01).

 B. Do the test as given in the Para. 3.A .
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.

 TASK 33-31-00-810-803


 Service Area Lights - The Service Area Light in the APU Compartment does not come on
 1. Possible Causes
_______________
 - lamp

 - SERVICE AREA LIGHT 6LJ

 - ON-OFF SWITCH 11LJ

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 33-31-00-710-001 Operational Test of the Service Area Lighting AMM 33-31-11-000-001 Removal of the Service Area Light 6LJ AMM 33-31-11-400-001 Installation of the Service Area Light 6LJ ASM 33-31/01
 3. Fault Confirmation
__________________
 A. Do the operational test of the Service Area Lighting (Ref. AMM TASK 33-31-00-710-001).
 4. Fault Isolation
_______________
 A. If the operational test shows that the SERVICE AREA LIGHT 6LJ, in the APU compartment, does not come on:
 - replace the lamp.
 (1) If the fault continues:

 - do a check for 28 VDC at the SERVICE AREA LIGHT 6LJ (Ref. ASM 33-31/01).
 (a) If there is approx. 28 VDC:

 - replace the SERVICE AREA LIGHT 6LJ (Ref. AMM TASK 33-31-11-000-001) and (Ref. AMM TASK 33-31-11-400-001).

 (b) If there is no 28 VDC::


 - do a check of the ON-OFF SWITCH 11LJ and replace it if necessary.

 (2) If the fault continues:

 


 - do a check and repair the wiring between: ON-OFF SWITCH 11LJ pin 2 and CB 2LJ, ON-OFF SWITCH 11LJ pin 1 and SERVICE AREA LIGHT 6LJ pin 1, SERVICE AREA LIGHT 6LJ pin 2 and GND (Ref. ASM 33-31/01).
 B. Do the test as given in the Para. 3.A .
 5. Close-up
________
 A. Put the aircraft back to its initial configuration.


 AIR CONDITIONING DUCT AND ACCESSORY COMPARTMENT LIGHTING
________________________________________________________ FAULT ISOLATION PROCEDURES
__________________________
 TASK 33-32-00-810-801
 Socket - No 28 VDC at the Maintenance Socket of the Air Conditioning Compt.
 1. Possible Causes
_______________
 - MAINTENANCE SOCKET (2LK)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM  33-32-00-720-001 Functional Test of the Maintenance Socket in the Air Conditioning Duct and Accessory Compartment (LK) ASM 33-32/01
 3. Fault Confirmation
__________________
 A. Do the functional test of the maintenance socket (Ref. AMM TASK 33-32-00-720-001).
 4. Fault Isolation
 
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