- do a check and repair the wiring (Ref. ASM 21-61/02) from:
- the ACSC1 (47HH) to the CB (49HH),
- the ACSC1 (47HH) to the CB (50HH) and,
- the ACSC1 (47HH) to ground.
(2) If the fault continues:
- do the trouble shooting procedures for the pack 1 electrical component with short circuit (Ref. TASK 21-61-00-810-820).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
C. If the test gives the maintenance message NO 28V ON PACK 1 MAIN:
- do a check and repair the wiring between: PC 1 (7HH) connector AA/8C and CB (3HH), PC 1 (7HH) connector AA/8D and GND (Ref. ASM 21-61/03).
D. If the test gives the maintenance message NO 28V ON PACK 1 SECD:
- do a check and repair the wiring between: PC 1 (7HH) connector AB/9A and CB (4HH), PC 1 (7HH) connector AB/9B and GND (Ref. ASM 21-61/03).
**ON A/C ALL
E. Do the test as given in the Para. 3.A.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page 239
Aug 01/05 CES TASK 21-61-00-810-806
Pack Controller 2 (ACSC2) Fault
1. Possible Causes
_______________
- CONTROLLER-PACK 2 TEMP (27HH)
- CONT-AIR COND SYSTEM 2 (57HH)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-61-00-810-821 Pack 2 Electrical Component with Short Circuit (AIR
PACK 2 REGUL FAULT) ASM 2151S01 ASM 216101 AMM 21-61-00-710-001 Operational Test of the Pack Temperature-Control
System 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
(47HH, 57HH)
AMM 21-61-34-400-001 Installation of the Pack Controller (7HH, 27HH)
AMM 21-61-34-400-002 Installation of the Air-Conditioning System
Controller (47HH, 57HH)
AMM 32-69-00-740-001 BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operative
ASM 21-51/01
ASM 21-61/01
ASM 21-63/02
3. Fault Confirmation
__________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
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).
R **ON A/C 401-499,
A. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
**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 FAILED with the fault code (6E):
- do a check for a ground signal at the PC 2 (27HH) connector AA/9B (Ref. ASM 21-61/01).
(1) If there is no ground signal:
- do the BITE test of the landing gear (Ref. AMM TASK 32-69-00-740-001).
(2) If test gives a different maintenance message refer to the Fault Symptom List.
(a) If the fault continues:
- do a check and repair the wiring if necessary between: PC 2 (27HH) connector AA/9B and LGCIU 2 (5GA2) connector AB/3J (Ref. ASM 21-61/01).
(3) If the fault continues:
- do a check and repair the wiring between: PC 2 (27HH) connector AB/6B and FCV (8HB) connector A/D, PC 2 (27HH) connector AA/1D and FCV (8HB) connector A/E, PC 2 (27HH) connector AA/1C and FCV (8HB) connector A/F, PC 2 (27HH) connector AA/1B and FCV (8HB) connector A/G, PC 2 (27HH) connector AA/1A and FCV (8HB) connector A/V, PC 2 (27HH) connector AA/11C and FCV (8HB) connector A/J, PC 2 (27HH) connector AA/11B and FCV (8HB) connector A/K, PC 2 (27HH) connector AA/11A and FCV (8HB) connector A/L (Ref. ASM 21-51/01).
B. If the test gives the maintenance message P2 CONT:
- replace the CONTROLLER-PACK 2 TEMP (27HH) (Ref. AMM TASK 21-61-34-000-001) and (Ref. AMM TASK 21-61-34-400-001).
(1) If the fault continues:
- do a check and repair the wiring if necessary between: PC 2 (27HH) connector AA/5A and CB (21HH), PC 2 (27HH) connector AA/5B and GND, PC 2 (27HH) connector AB/13D and CB (22HH),
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 Trouble Shooting Manual 排故手册 AIR CONDITIONING 空调2(28)