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时间:2011-02-24 09:55来源:蓝天飞行翻译 作者:admin
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R A. Aircraft Maintenance Configuration
R (1) Make sure that the aircraft electrical circuits are energized R (Ref. TASK 24-41-00-861-002).
R (2) Make sure that the access panel(s) are removed (Ref. TASK 53-35-13-R 000-002).
R (a) FOR 25HH R - 191KB.
R (b) FOR 40HH R - 192KB.


R  Subtask 21-61-41-865-058 
R  B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and 
R  tagged 
R  -------------------------------------------------------------------------------
R  PANEL  DESIGNATION  IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  FOR 10HM 
R  122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC  1HH  X22 
R  122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC  3HH  X21 
R  **ON A/C 106-149, 303-399, 
R  122VU  4HH  Y19 
R  **ON A/C 106-149, 159-199, 211-299, 301-399, 
R  122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC  2HH  Y18 
R  **ON A/C 159-199, 211-299, 301-302, 
R  122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC  4HH  Y19 
R  **ON A/C 106-149, 159-199, 211-299, 301-399, 
R  FOR 11HM 
R  122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC  21HH  W22 
R  122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC  23HH  W21 
R  122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC  24HH  Y21 
R  122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC  22HH  Y20

 

R  4. Procedure_________ 
R  (Ref. Fig. 403/TASK 21-61-41-991-003) 
R  Subtask 21-61-41-420-052 
R  A. Installation of the Back Up Solenoid 
R  (1) Put the back up solenoid (5) in position and install the screw (4), 
R  the washer (6), and the nut (7). 
R  (2) Remove the blanking plugs from the disconnected line ends. 
R  (3) Apply a small quantity of COMMON GREASE (Material No. 04-014A) to the 
R  threaded parts of the connectors (2) and (3). 
R  (4) At the solenoid (5), install the sense line connectors (2) and (3). 
R  (5) TORQUE the sense line connectors (2) and (3) to between 0.9 and 0.915 
R  m.daN (79.64 and 80.97 lbf.in). 
R  (6) Remove the blanking caps and connect the electrical connector (1). 
R  Subtask 21-61-41-865-059 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  (1) FOR 25HH 
R  - 1HH, 2HH, 3HH, 4HH. 
R  (2) FOR 40HH 
R  - 21HH, 22HH, 23HH, 24HH. 
R  Subtask 21-61-41-710-052 
R  C. Leak and Operational Test of the Sense Lines Assembly 
R  (1) Do the pre-conditioning through the HP ground connector or with the 
R  APU (Ref. TASK 12-33-21-618-001) (Ref. TASK 12-33-21-618-001). 
R  (2) Do a leak check of the sense line connectors (2) and (3) at the back 
R  up solenoid (5). 
R  NOTE : Leaks are not permitted.____

 

R  (3) After approx. 15 minutes stop the pre-conditioning (Ref. TASK 12-33-
R  21-618-001) (Ref. TASK 12-33-21-618-001). 
R  (4) Do the operational test of the pack temperature control system 
R  (Ref. TASK 21-61-00-710-001). 
R  5. Close-up________ 
R  Subtask 21-61-41-410-054 
R  A. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Install the access panel(s) (Ref. TASK 53-35-13-400-002). 
R  (a) FOR 25HH 
R  - 191KB. 
R  (b) FOR 40HH 
R  - 192KB. 
R  Subtask 21-61-41-862-052 
R  B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R  002).

 

 ACTUATOR - AIR INLET FLAP (8HH,28HH) - REMOVAL/INSTALLATION
___________________________________________________________
 TASK 21-61-51-000-001
 Removal of the Air-Inlet Flap Actuator 8HH and 28HH
 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.

 NOTE : The procedure is the same for the air-inlet flap actuator 8HH and 28HH.
____
 1.
 Reason for the Job
 
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