TASK 21-61-00-810-864 Pack 2 Control - No Test Result
 1. Possible Causes
_______________
 - VALVE-FLOW CTL (8HB)

 - wiring

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-51-51-000-001 Removal of the Pack Flow-Control Valve AMM 21-51-51-400-001 Installation of the Pack Flow-Control Valve AMM 21-61-00-710-001 Operational Test of the Pack Temperature-Control
 System ASM 21-51/02
 3. Fault Confirmation
__________________
 A. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives the message NO TEST RESULT RECEPTION FROM P2 CONT:
 - replace the VALVE-FLOW CTL (8HB) (Ref. AMM TASK 21-51-51-000-001) and (Ref. AMM TASK 21-51-51-400-001).
 (1) If the fault continues:
 - do a check and the repair the wiring (Ref. ASM 21-51/02): from the PC2 (27HH)AB/6B to the FCV (8HB)A/D, from the PC2 (27HH)AA/7B to the FCV (11HB)A/C, from the FCV (8HB)A/B to the ground.
 B. Do the test as given in the Para. 3.A.

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 TASK 21-61-00-810-866
 Pack 1 Electrical Component with Short Circuit (AIR PACK 1)
 1. Possible Causes
_______________
 - CONTROLLER-PACK 1 TEMP (7HH)

 - ACTUATOR-AIR INLET FLAP (8HH)

 - ACTUATOR-AIR OUTLET FLAP (9HH)

 - VALVE-TURBINE BYPASS (10HH)

 - SENSOR-COMPRESSOR OVHT (15HH)

 - SENSOR-PACK OUTLET TEMP (13HH)

 - SENSOR-BLEED TEMPERATURE (18HH)

 - SENSOR-WATER EXTRACTOR TEMPERATURE (11HH)

 - SENSOR-PRESSURE (10HB)

 - SENSOR-PACK INLET PRESSURE (16HH)

 - 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)
 「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 A281
 201-299, 301-399, Aug 01/05 CES

 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
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
 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 21-51/01
 ASM 21-61/04
 ASM 21-61/04

 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.
　
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