(3) If the fault continues:
- do a check that the resistance of the FWD cabin-temperature sensor (22HK) measured between connector A/A and A/B and connector A/E and A/D is in these limits (Ref. ASM 21-63/03): Temp (Deg.C) OHMS ---------------------------
+ 10 18820 +/- 5 %
+ 18 13340 +/- 5 %
+ 25 10000 +/- 5 %
+ 30 8197 +/- 5 %
+ 40 5598 +/- 5 %
+ 50 3903 +/- 5 %
(a) If the resistance values are out of the specified limits:
- replace the SENSOR-TEMPERATURE, FWD CABIN (22HK) (Ref. AMM TASK 21-63-17-000-001) and (Ref. AMM TASK 21-63-17-400-001).
(4) If the fault continues:
- do a potentiometer test of the FWD cabin-temperature selector (28HK) (Ref. CMM 216312).
(a) If the test is not OK:
- replace the SEL-TEMPERATURE, AIR COND/FWD CABIN (28HK) (Ref. AMM TASK 21-63-11-000-001) and (Ref. AMM TASK 21-63-11-400-001).
(5) If the fault continues:
- replace the CONT-AIR COND SYSTEM 1 (47HH) (Ref. AMM TASK 21-61-34-000-002) and (Ref. AMM TASK 21-61-34-400-002).
(6) If the fault continues:
- replace the CONT-AIR COND SYSTEM 2 (57HH) (Ref. AMM TASK 21-61-34-000-002) and (Ref. AMM TASK 21-61-34-400-002).
D. If the test confirms the fault for the AFT cabin zone, with the pushbutton switch HOT AIR, which is installed on the panel 30VU, set to on (with FAULT and OFF legends off) or OFF:
- do a check that the resistance of the AFT cabin-duct temperature sensor (17HK) measured between connector A/E and A/F and connector A/C and A/D is in these limits (Ref. ASM 21-63/03):
Temp (Deg.C) OHMS ---------------------------
+ 10 18820 +/- 5 %
+ 18 13340 +/- 5 %
+ 25 10000 +/- 5 %
+ 30 8197 +/- 5 %
+ 40 5598 +/- 5 %
+ 50 3903 +/- 5 %
(1) If the resistance values are out of the specified limits:
- replace the SENSOR-DUCT TEMPERATURE,AFT CABIN (17HK) (Ref. AMM TASK 21-63-15-000-001) and (Ref. AMM TASK 21-63-15-400-001).
R (2) If the fault continues:
R - do a check that the AFT cabin-temperature sensor (23HK), housing,
R ducts and flexible hoses are free from contamination, are not
R damaged and that the sense line has no leakage (Ref. AMM TASK 21-R 63-17-210-001).
R (3) If the fault continues:
R - do a check that the resistance of the AFT cabin-temperature sensor
R (23HK) measured between connector A/A and A/B and connector A/E and
R A/D is in these limits (Ref. ASM 21-63/03):
R Temp (Deg.C) OHMS
R ---------------------------R + 10 18820 +/- 5 %
R + 18 13340 +/- 5 %
R + 25 10000 +/- 5 %
R + 30 8197 +/- 5 %
R + 40 5598 +/- 5 %
R + 50 3903 +/- 5 %
R (a) If the resistance values are out of the specified limits:
R - replace the SENSOR-TEMPERATURE, AFT CABIN (23HK) (Ref. AMM TASK
R 21-63-17-000-001) and (Ref. AMM TASK 21-63-17-400-001).
R (4) If the fault continues:
R - do a potentiometer test of the AFT cabin-temperature selector
R (29HK) (Ref. CMM 216312).
R (a) If the test is not OK:
R - replace the SEL-TEMPERATURE, AIR COND/AFT CABIN (29HK) (Ref.
R AMM TASK 21-63-11-000-001) and (Ref. AMM TASK 21-63-11-400-R 001).
R (5) If the fault continues:
R - replace the CONT-AIR COND SYSTEM 1 (47HH) (Ref. AMM TASK 21-61-34-R 000-002) and (Ref. AMM TASK 21-61-34-400-002).
R (6) If the fault continues:
R - replace the CONT-AIR COND SYSTEM 2 (57HH) (Ref. AMM TASK 21-61-34-R 000-002) and (Ref. AMM TASK 21-61-34-400-002).
R **ON A/C ALL
E. Do the test as given in the Para. 3.A.
- Make sure that the belly-fairing blowout-panel is closed:
- If the belly-fairing blowout-panel is open, do a check for damage of the bellows between the mixer-unit and the air-pack.
5. Close-up
________
A. Put the aircraft back to its initial configuration. R
「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 255
Feb 01/05 CESR **ON A/C 051-052, 106-149, 303-399,
TASK 21-63-00-810-823
Cockpit Duct Overheat Detection
1. Possible Causes
_______________
- SENSOR-DUCT TEMPERATURE,COCKPIT (15HK)
- SENSOR-DUCT OVHT TEMPERATURE,COCKPIT (18HK)
- TRIM VALVE CKPT (11HK)
- VALVE-PRESSURE REGULATING (14HK)
- CONT-ZONE TEMPERATURE (8HK)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) AIR CONDITIONING 空調(diào)2(116)
