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时间:2011-03-28 09:16来源:蓝天飞行翻译 作者:航空
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 201-299, 301-399, Aug 01/05 CES


 TASK 21-61-00-810-867
 Pack 2 Electrical Component with Short Circuit (AIR PACK 2)
 1. Possible Causes
_______________
 - CONTROLLER-PACK 2 TEMP (27HH)

 - ACTUATOR-AIR INLET FLAP (28HH)

 - ACTUATOR-AIR OUTLET FLAP (29HH)

 - VALVE-TURBINE BYPASS (30HH)

 - SENSOR-COMPRESSOR OVHT (35HH)

 - SENSOR-PACK OUTLET TEMP (34HH)

 - SENSOR-BLEED TEMPERATURE (38HH)

 - SENSOR-WATER EXTRACTOR TEMPERATURE (31HH)

 - SENSOR-PRESSURE (9HB)

 - SENSOR-PACK INLET PRESSURE (36HH)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 21-51-11-000-001 Removal of the Differential Pressure Sensor 9HB (10HB) AMM 21-51-11-400-001 Installation of the Differential Pressure Sensor 9HB (10HB) AMM 21-61-12-000-001 Removal of the Compressor Overheat - Temperature Sensor 15HH (35HH) AMM 21-61-12-400-001 Installation of the Compressor Overheat - Temperature Sensor 15HH (35HH) AMM 21-61-13-000-001 Removal of the Water-Extractor Temperature Sensors 11HH and 31HH AMM 21-61-13-400-001 Installation of the Water-Extractor Temperature Sensors 11HH and 31HH AMM 21-61-15-000-001 Removal of the Pack Outlet - Temperature Sensors 13HH and 34HH AMM 21-61-15-400-001 Installation of the Pack Outlet - Temperature Sensors
 13HH and 34HH AMM 21-61-16-000-001 Removal of the Pack-Inlet Pressure Sensor 16HH (36HH) AMM 21-61-16-400-002 Installation of the Pack-Inlet Pressure Sensor 16HH
 (36HH) AMM 21-61-17-000-001 Removal of the Bleed Air Temperature Sensor 18HH (38HH) AMM 21-61-17-400-001 Installation of the Bleed Air Temperature Sensor 18HH
 (38HH) AMM 21-61-34-000-001 Removal of the Pack Controller (7HH, 27HH) AMM 21-61-34-400-001 Installation of the Pack Controller (7HH, 27HH) AMM 21-61-51-000-001 Removal of the Air-Inlet Flap Actuator 8HH and 28HH
 「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 : 001-049, 051-099, 101-149, 151-199, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page A289
 201-299, 301-399, Aug 01/05 CES


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-61-51-400-001 Installation of the Air-Inlet Flap Actuator 8HH and
 28HH AMM 21-61-52-000-001 Removal of the Air-Outlet Flap Actuator 9HH (29HH) AMM 21-61-52-400-001 Installation of the Air-Outlet Flap Actuator 9HH
 (29HH)
 AMM 21-61-53-000-001 Removal of the Bypass Valve 10HH (30HH)
 AMM 21-61-53-400-001 Installation of the Bypass Valve 10HH (30HH)
 ASM 21-51/01
 ASM 21-61/02
 ASM 21-61/02

 3. Fault Confirmation
__________________
 A. Do a read out of the post flight report.
 NOTE : The fault cannot be reproduced on the ground. You must fly the
____ aircraft to see if the corrective action has been succesfull or not.
 4. Fault Isolation
_______________
 A. Restricted Pack Controller Fault Isolation
 NOTE : This procedure is only applicable for:
____
 - Pack Controller Part Number 759A0000-xx

 - Pack Controller Part Number 759C0000-xx


 (1) If the post flight report gives the warning PACK 2 without a maintenance message:

 - swap the PC 2 (27HH) and the PC 1 (7HH) (Ref. AMM TASK 21-61-34-000-001) and (Ref. AMM TASK 21-61-34-400-001).
 (a) If the fault moves with the PC 2:
 - swap back the PC 2 (27HH) and the PC 1 (7HH) (Ref. AMM TASK 21-61-34-000-001) and (Ref. AMM TASK 21-61-34-400-001).

 - replace the CONTROLLER-PACK 2 TEMP (27HH) (Ref. AMM TASK 21-61-34-000-001) and (Ref. AMM TASK 21-61-34-400-001).

 

 (2) If the fault does not move with the PC 2:

 - swap back the PC 2 (27HH) and the PC 1 (7HH) (Ref. AMM TASK 21-61-34-000-001) and (Ref. AMM TASK 21-61-34-400-001).

 - disconnect the electrical connector (31HHA) (Ref. AMM TASK 21-61-13-000-001).

 - make sure that the electrical connector is clean and in the correct condition.

 - do a check for voltage at the electrical connector (31HHA) between pins C and D (Ref. ASM 21-61/02).

 


 「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 : 001-049, 051-099, 101-149, 151-199, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page A290
 
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