- at the electrical connector (23HKA) do a check for a short circuit between:
* pins D and E and,
* GND and pins D and E.
(a) If there is no short circuit connect the electrical connector (23HKA).
(b) If there is a short circuit repair the related wiring between:
* connector (23HKA) pin D and ZC connector (8HKAA) pin 8K,
* connector (23HKA) pin E and ZC connector (8HKAA) pin 8J.
- connect the electrical connector (23HKA).
(9) If the fault continues:
- disconnect the electrical connector (24HKA) from the SENSOR-MIXER UNIT TEMPERATURE COCKPIT (24HK).
- at the electrical connector do a check for a short circuit between:
* pins C and D and,
* GND and pins C and D.
(a) If there is no short circuit connect the electrical connector (24HKA).
(b) If there is a short circuit repair the related wiring between:
* connector (24HKA) pin C and ZC connector (8HKAA) pin 8H,
* connector (24HKA) pin D and ZC connector (8HKAA( pin 8G.
- connect the electrical connector (24HKA).
(10) If the fault continues:
- disconnect the electrical connector (25HKA) from the SENSOR-MIXER UNIT TEMPERATURE CABIN (25HK).
- at the electrical connector (25HKA) do a check for a short circuit between:
* pins C and D and,
* GND and pins C and D.
(a) If there is no short circuit connect the electrical connector (25HKA).
(b) If there is a short circuit repair the related wiring between:
* connector (25HKA) pin C and ZC connector (8HKAA) pin 10H,
* connector (25HKA) pin D and ZC connector (8HKAA) pin 10G.
- connect the electrical connector (25HKA).
- install the CONT-ZONE TEMPERATURE (8HK). (Ref. AMM TASK 21-63-34-000-001).
- on the circuit breaker panel 122VU close the CBIs 1HK (V17), 2HK (V18), 3HK (V19) and 4HK (V20).
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, ∞∞21-63-00∞∞∞∞∞∞∞∞∞∞Page A203
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, ∞∞21-63-00∞∞∞∞∞∞∞∞∞∞Page A204
201-299, 301-399, Aug 01/05 CES
**ON A/C ALL
TASK 21-63-00-810-846
Actual Zone Temperatures are above Selected Zone Temperatures (Cockpit)
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 12-33-21-618-001 Pre-conditioning through the HP Ground Connection AMM 21-52-00-200-011 General Visual Inspection of the Bellows between the Pack Outlet and the Mixer Unit AMM 21-52-43-210-001 Detailed Visual Inspection of Pack-Air Check-Valve Flappers for Condition and Operation
3. Fault Confirmation
__________________
A. Functional Test of the Cockpit Temperature Control
(1) Do the pre-conditioning through the HP ground connection (Ref. AMM TASK 12-33-21-618-001).
(2) With your hand or a piece of paper do a check for air flow at the cockpit air-outlets.
4. Fault Isolation
_______________
A. If there is not a sufficient airflow from the cockpit air-outlets do the steps which follow:
(1) Do a check of the belly-fairing blowout-panel.
- If the belly-fairing blowout panel is open, then close it.
(2) Do a detailed visual inspection of the bellows between the air-pack 1 outlet and the mixer unit (Ref. AMM TASK 21-52-00-200-011).
(3) Replace the bellows if nessesary. NOTE : If the bellows are damaged, do a detailed visual inspection of
____ the flap of the pack 1 downstream check-valve (15HM)for condition and operation (Ref. AMM TASK 21-52-43-210-001).
Aug 01/05R CES
TASK 21-63-00-810-847
Actual Zone Temperatures are above Selected Zone Temperatures (Cabin)
1. Possible Causes
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AIR CONDITIONING 空調2(135)
