3. Fault Confirmation
__________________
A. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
NOTE : If a fault is detected, the PC gives a fault code for shop
____ maintenance in addition to the related CFDS message(s) (refer to TSM chapter 21-63-00, page block 301).
4. Fault Isolation
_______________
A. If the test gives the maintenance message P1 PRESS INL SENSOR:
- replace the SENSOR-PACK INLET PRESSURE (16HH) (Ref. AMM TASK 21-61-16-000-001) and (Ref. AMM TASK 21-61-16-400-002).
(1) If the fault continues:
- do a check and repair the wiring between: CONNECTOR (7559VC) pin C and PC 1 (7HH) connector AA/10C, CONNECTOR (7559VC) pin B and PC 1 (7HH) connector AA/10D, CONNECTOR (7559VC) pin A and PC 1 (7HH) connector AB/15C, CONNECTOR (7559VC) pin D and PC 1 (7HH) connector AB/15D (Ref. AWM 21-61-04) and (Ref. AWM 21-61-04).
B. Do the test as given in the Para. 3.A.
「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 A211
201-299, 301-399, Aug 01/05 CES
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「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 A212
201-299, 301-399, Aug 01/05 CES
TASK 21-61-00-810-823
Pack 2 Pressure Inlet Sensor Fault
1. Possible Causes
_______________
- SENSOR-PACK INLET PRESSURE (36HH)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-61-00-710-001 Operational Test of the Pack Temperature-Control
System 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)
AWM 21-61-09
AWM 21-61-09
3. Fault Confirmation
__________________
A. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
NOTE : If a fault is detected, the PC gives a fault code for shop
____ maintenance in addition to the related CFDS message(s) (refer to TSM chapter 21-63-00, page block 301).
4. Fault Isolation
_______________
A. If the test gives the maintenance message P2 PRESS INL SENSOR:
- replace the SENSOR-PACK INLET PRESSURE (36HH) (Ref. AMM TASK 21-61-16-000-001) and (Ref. AMM TASK 21-61-16-400-002).
(1) If the fault continues:
- do a check and repair the wiring between: CONNECTOR (7560VC) pin C and PC 2 (27HH) connector AA/10C, CONNECTOR (7560VC) pin B and PC 2 (27HH) connector AA/10D, CONNECTOR (7560VC) pin A and PC 2 (27HH) connector AB/15C, CONNECTOR (7560VC) pin D and PC 2 (27HH) connector AB/15D (Ref. AWM 21-61-09) and (Ref. AWM 21-61-09).
B. Do the test as given in the Para. 3.A.
「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 A213
201-299, 301-399, Aug 01/05 CES
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「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 A214
201-299, 301-399, Aug 01/05 CES
**ON A/C ALL
TASK 21-61-00-810-824
Pack 1 Compressor Temperature Sensor Fault
1. Possible Causes
_______________
- SENSOR-COMPRESSOR TEMPERATURE (12HH))
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AIR CONDITIONING 空調2(53)
