ZC (8HK) connector AB/K8 and GND,
ZC (8HK) connector AB/J13 and CB (3HK) (Ref. ASM 21-63/01).
(2) If the fault continues:
- do a check and repair the wiring if necessary of the signal: ARINC 429 XTR INT (P) from the ZC (8HK) to the PC 1 (7HH) and the PC 2 (27HH), ARINC 429 XTR INT (S) from the ZC (8HK) to the PC 1 (7HH) and the PC 2 (27HH), ARINC 429 RCV INT (S) from the ZC (8HK) to the PC 1 (7HH), ARINC 429 RCV INT (P) from the ZC (8HK) to the PC 2 (27HH) (Ref. ASM 21-63/02).
(3) If the fault continues:
- do the trouble shooting procedures for the zone cont electrical component with short circuit (Ref. TASK 21-63-00-810-827).
R B. If the test gives the maintenance message NO 28V ON ZONE MAIN:
- do a check and repair the wiring between: ZC (8HK) connector AC/10 and CB (3HK), ZC (8HK) connector AC/8 and GND (Ref. ASM 21-63/01).
R C. If the test gives the maintenance message NO 28V ON ZONE SECD:
- do a check and repair the wiring between: ZC (8HK) connector AC/9 and CB (4HK), ZC (8HK) connector AC/7 and GND (Ref. ASM 21-63/01).
R D. Do the test as given in the Para. 3.A.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
TASK 21-63-00-810-802
Cockpit Trim-Air Valve Fault
1. Possible Causes
_______________
- TRIM VALVE CKPT (11HK)
- CONT-ZONE TEMPERATURE (8HK)
- CONT-AIR COND SYSTEM 1 (47HH)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 21-61-34-000-002 Removal of the Air-Conditioning System Controller (47HH, 57HH) AMM 21-61-34-400-002 Installation of the Air-Conditioning System Controller (47HH, 57HH) AMM 21-63-00-710-004 Operational Test of the Cockpit and Cabin Temperature
Control with CFDS/MCDU AMM 21-63-34-000-001 Removal of the Zone Controller (8HK) AMM 21-63-34-400-001 Installation of the Zone Controller (8HK) AMM 21-63-51-000-001 Removal of the Trim Air Valve (11HK,12HK,13HK) AMM 21-63-51-400-001 Installation of the Trim Air Valve (11HK,12HK,13HK) ASM 21-63/02
3. Fault Confirmation
__________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
A. Confirmation of the Fault
(1) Do the operational test of the cockpit and cabin temperature-control system with CFDS/MCDU (Ref. AMM TASK 21-63-00-710-004).
NOTE : If a fault is detected, the ZC gives a fault code for shop
____ maintenance in addition to the related CFDS message(s). For detailed information see the applicable Page Block 301.
(2) Do a read out of the POST FLIGHT REPORT and the PREVIOUS LEG REPORT.
「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 ∞∞21-63-00∞∞∞∞∞∞∞∞∞∞Page 203
Aug 01/05 CES
R **ON A/C 401-499,
A. Confirmation of the Fault
(1) Do the operational test of the cockpit and cabin temperature-control system with CFDS/MCDU (Ref. AMM TASK 21-63-00-710-004).
(2) Do a read out of the POST FLIGHT REPORT and the PREVIOUS LEG REPORT.
**ON A/C ALL
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
A. If the test gives the maintenance message TEST OK, but the POST FLIGHT REPORT and the PREVIOUS LEG REPORT give the maintenance message TRIM VALVE CKPT:
- replace the TRIM VALVE CKPT (11HK) (Ref. AMM TASK 21-63-51-000-001) and (Ref. AMM TASK 21-63-51-400-001).
B. If the test gives the maintenance message TRIM VALVE CKPT:
- replace the TRIM VALVE CKPT (11HK) (Ref. AMM TASK 21-63-51-000-001) and (Ref. AMM TASK 21-63-51-400-001).
(1) If the fault continues:
- do a check and repair the wiring (Ref. ASM 21-63/02) from:
- the TRIM VALVE CKPT (11HK) to the ZC (8HK) and,
- the TRIM VALVE CKPT (11HK) to ground.
C. If the test gives the maintenance message TEST OK, but the cockpit trim-air valve symbol on the ECAM COND page is replaced by amber XX:
- replace the CONT-ZONE TEMPERATURE (8HK) (Ref. AMM TASK 21-63-34-000-001) and (Ref. AMM TASK 21-63-34-400-001).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) AIR CONDITIONING 空調(diào)2(98)
