R **ON A/C ALL
4. Fault Isolation
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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
A. If the test gives the maintenance message P2 CONT OR ANTI ICE VALVE:
- 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).
(1) 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).
- replace the VALVE-ANTI-ICE (37HH) (Ref. AMM TASK 21-61-41-000-001) and (Ref. AMM TASK 21-61-41-400-001).
(3) If the fault continues:
- do a check and repair the wiring (Ref. ASM 21-61/02) from:
- the VALVE (37HH)A pin A and the PC 2 (27HH)AB pin 8A and,
- the VALVE (37HH)A pins B and C to ground.
R **ON A/C 401-499,
R A. If the test gives the maintenance message P2 ANTI ICE VALVE(37HH):
R - swap the ACSC2 (57HH) and the ACSC1 (47HH) (Ref. AMM TASK 21-61-34-000-R 002) and (Ref. AMM TASK 21-61-34-400-002).
R (1) If the fault moves with the ACSC2:
R - swap back the ACSC2 (57HH) and the ACSC1 (47HH) and,
R - replace the CONT-AIR COND SYSTEM 2 (57HH).
R (2) If the fault does not move with the ACSC2:
R - swap back the ACSC2 (57HH) and the ACSC1 (47HH) (Ref. AMM TASK 21-R 61-34-000-002) and (Ref. AMM TASK 21-61-34-400-002).
R - replace the VALVE-ANTI-ICE (37HH) (Ref. AMM TASK 21-61-41-000-001)
R and (Ref. AMM TASK 21-61-41-400-001).
R (3) If the fault continues:
R - do a check and repair the wiring (Ref. ASM 21-61/02) from:
R - the VALVE (37HH) to the ACSC2 (57HH) and,
R - the VALVE (37HH) to ground.
「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 : ALL ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 275
Aug 01/05 CES
R **ON A/C ALL
B. Do the test as given in the Para. 3.A.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
R
TASK 21-61-00-810-820
Pack 1 Electrical Component with Short Circuit (AIR PACK 1 REGUL FAULT)
1. Possible Causes
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- ACTUATOR-AIR INLET FLAP (8HH)
- ACTUATOR-AIR OUTLET FLAP (9HH)
- CONTROLLER-PACK 1 TEMP (7HH)
- CONT-AIR COND SYSTEM 1 (47HH)
- SENSOR-WATER EXTRACTOR TEMPERATURE (11HH)
- VALVE-TURBINE BYPASS (10HH)
- SENSOR-COMPRESSOR TEMPERATURE (12HH)
- VALVE-FLOW CTL (11HB)
- FLOW CTL UNIT - PACK 1 (23HB)
- SENSOR-PACK INLET PRESSURE (16HH)
- SENSOR-PRESS, PACK 1 INLET (23HB1)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-51-13-000-001 Removal of the Pack-Inlet Pressure Sensor 23HB1
(24HB1)
AMM 21-51-13-400-002
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 AMM 21-61-11-000-001 Removal of the Compressor Outlet - Temperature Sensor 12HH (32HH) AMM 21-61-11-400-001 Installation of the Compressor Outlet - Temperature Sensor 12HH (32HH) 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 21-61-16-000-001 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 21-61-34-000-001 Removal of the Pack Controller (7HH, 27HH)
AMM 21-61-34-000-002 Removal of the Air-Conditioning System Controller
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AIR CONDITIONING 空調2(38)
