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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  24-41-00-861-002  Energize the Aircraft Electrical Circuits from the 
R  External Power 
R  53-35-13-000-002  Removal of the Quick-Release Access Panels from the 
R  Belly Fairing Structure 
R  21-61-41-991-003  Fig. 403 
R  3. Job Set-up__________ 
R  Subtask 21-61-41-861-052 
R  A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 

R  Subtask 21-61-41-865-057 
R  B. Open, safety and tag this(these) circuit breaker(s): 
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  Subtask 21-61-41-010-052 
R  C. Get Access 
R  (1) Remove the access panel(s) (Ref. TASK 53-35-13-000-002) 
R  (a) For FIN 25HH 
R  - 191KB. 
R  (b) For FIN 40HH 
R  - 192KB.

 

R  4. Procedure_________ 
R  (Ref. Fig. 403/TASK 21-61-41-991-003) 
R  Subtask 21-61-41-020-054 
R  A. Removal of the Back Up Solenoid 
R  (1) At the back up solenoid (5), disconnect the electrical connector (1). 
R  (2) Put blanking caps on the disconnected electrical connectors. 
R  (3) Disconnect the sense line connectors (2) and (3). 
R  (4) Remove the nut (7), the washer (6), the screw (4) and the back up 
R  solenoid (5). 
R  (5) Put blanking plugs on the disconnected line ends.

 

R Back Up Solenoid R Figure 403/TASK 21-61-41-991-003
 1EFF : 106-149, 159-199, 211-299, 301-399, 1 21-61-41Page 440 1 1 Aug 01/05 1 1 1CES 1


R  TASK 21-61-41-400-003 
R  Installation of the Back Up Solenoid 
R  WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM_______ 
R  FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. 
R  HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL. 
R  NOTE : The procedure is the same for the back up solenoids 25HH and 40HH.____ 
R  1. Reason for the Job__________________ 
R  Self Explanatory 
R  2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R  -------------------------------------------------------------------------------
R  REFERENCE  QTY DESIGNATION 
R  -------------------------------------------------------------------------------
R  No specific  Torque Wrench : range 0.00 to 1.20 m.daN 
R  (0.00 to 9.00 lbf.ft) 
R  B. Consumable Materials 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------
R  Material No. 04-014A  USA MIL-PRF-907 
R  HIGH TEMPERATURECOMPOUND (Ref. 20-31-00)

 

R C. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 12-33-21-618-001 R 12-33-21-618-001 R 21-61-00-710-001 R R 24-41-00-861-002 R R 24-41-00-862-002 R R 53-35-13-000-002 R R 53-35-13-400-002 R R 21-61-41-991-003
R 3. Job Set-up
__________
R Subtask 21-61-41-860-053 Pre-conditioning through the HP Ground Connection Pre-conditioning with the APU Operational Test of the Pack Temperature-Control System Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the Quick-Release Access Panels from the Belly Fairing Structure Installation of the Quick-Release Access Panels on the Belly Fairing Structure Fig. 403
 
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