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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  122VU  4HH  Y19 
R  **ON A/C 401-499, 
R R  122VU AIR COND/TEMP CTL SYS 1/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 1/CHAN A/28VDC 122VU AIR COND/TEMP CTL SYS 1/CHAN B/115VAC **ON A/C ALL 49HH 51HH 50HH  X22 X21Y18
 FOR 34HH

 

R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 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 
R  **ON A/C 401-499,
R R  122VU AIR COND/TEMP CTL SYS 2/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 2/CHAN A/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/115VAC  53HH 55HH 56HH 54HH  W22W21 Y21Y20 
**ON A/C ALL
 Subtask 21-61-15-010-050-A
 C. Get Access
 (1) Remove the access panel/s (Ref. TASK 53-35-13-000-002).
 (a) FOR 13HH - 191BB.
 (b) FOR 34HH - 192FB.
 4. Procedure_________
 (Ref. Fig. 401/TASK 21-61-15-991-001)
 Subtask 21-61-15-020-051
 A. Removal of the Pack Outlet-Temperature Sensor
 (1) Disconnect the electrical connector (2).
 (2) Put blanking caps on the disconnected electrical connectors.

 

 Pack Outlet - Temperature Sensor Figure 401/TASK 21-61-15-991-001
 1EFF : 1 1R 1CES  ALL  1 11 1 21-61-15 Page 404 Feb 01/05

 

 (3)
 Remove and discard the lockwire.

 (4)
 Remove the pack outlet-temperature sensor (1) and the packing (3).

 (5)
 Remove the packing (3) from the pack outlet-temperature sensor (1).

 (6)
 Put blanking plugs on the disconnected line ends.


 5. Close-up
________
 1EFF : ALL 1 21-61-15Page 405 1 1 Aug 01/05R 1 1 1CES 1


 TASK 21-61-15-400-001 Installation of the Pack Outlet - Temperature Sensors 13HH and 34HH 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 pack outlet temperature sensors 13HH and
____ 34HH
 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 LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 packing 21-61-03 06 -020 3 packing 21-61-03 06 -020A
 1EFF : ALL 1 21-61-15Page 406 1 1 Aug 01/05R 1 1 1CES 1


 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
21-61-00-710-001  Operational Test of the Pack Temperature-Control System
 24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied from the External Power
 53-35-13-000-002  Removal of the Quick-Release Access Panels from the Belly Fairing Structure
 53-35-13-400-002  Installation of the Quick-Release Access Panels on the Belly Fairing Structure
 21-61-15-991-001  Fig. 401
 3. Job Set-up__________
 Subtask 21-61-15-860-050-A
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
 
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