__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking plugs
No specific circuit breaker(s) safety clip(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure 21-61-18-991-001 Fig. 401
3. Job Set-up
__________ Subtask 21-61-18-861-050
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
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Subtask 21-61-18-865-050
B. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 10HM9 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
R 122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC 4HH Y19
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
R **ON A/C 106-149, 303-399,
R 122VU 4HH Y19
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
FOR 11HM9 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 21HH 23HH 24HH 22HH W22W21Y21Y20
Subtask 21-61-18-010-050
C. Get Access
(1) Remove the access panel/s (Ref. TASK 53-35-13-000-002).
R (a) FOR 10HM9 - 191KB.
R (b) FOR 11HM9 - 192KB.
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4. Procedure
_________
(Ref. Fig. 401/TASK 21-61-18-991-001) Subtask 21-61-18-020-050
A. Removal of the Compressor Pneumatic Overheat-Sensor
(1)
Disconnect the sense line (2).
(2)
Put blanking plugs on the disconnected line ends.
(3)
Remove and discard the lockwire.
(4)
Remove the screws (3), the washers (4) and the compressor pneumatic overheat-sensor (5).
(5)
Remove the packing (6) from the compressor pneumatic overheat-sensor (5).
(6)
Put blanking plugs on the disconnected line ends.
5. Close-up
________
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Compressor Pneumatic Overheat-Sensor
Figure 401/TASK 21-61-18-991-001
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Installation of the Compressor Pneumatic Overheat-Sensor 10HM9 (11HM9)
WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM
_______ FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-012 USA VV-P-236
PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 19-009 USA AMS 5687
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本文链接地址：A320飞机维护手册 AMM AIR CONDITIONING 空调 5(33)
