R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 21-61-11Page 405 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1
 Compressor Outlet - Temperature Sensor 
 Figure 401A/TASK 21-61-11-991-001-A  
R 1EFF :  401-499,  1  21-61-11 Page 406  
1  1  Aug 01/05 
 1  1 
 1CES  1
 TASK 21-61-11-400-001 Installation of the Compressor Outlet - Temperature Sensor 12HH (32HH) 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
 -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN 
R (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
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FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
3 packing 21-61-03 08 -050 3 packing 21-61-03 08 -050A
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
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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
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 21-61-11-991-001 Fig. 401
R **ON A/C 401-499,
 21-61-11-991-001-A Fig. 401A
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 21-61-11-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
 (2)
 Make sure that the access panel/s is are removed (Ref. TASK 53-35-13-000-002).
 (a)
 FOR 12HH
-191KB.
 (b)
 FOR 32HH
 -192KB.
 Subtask 21-61-11-865-051 
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged 
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 12HH  
R  **ON A/C 401-499, 
R  49VU AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 52HH  D08  
R  122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC  1HH 3HH  X22X21  
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,  
R R  122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,  4HH  Y19  
R R  122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC **ON A/C 106-149, 303-399,  2HH  Y18  
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  49HH 51HH 50HH  X22 X21Y18
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C ALL 
 FOR 32HH  
 
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