R 1EFF : 401-499, 1 21-52-32Page 411 1 1 Aug 01/05 1 1 1CES 1
Attachment Components - Condensor Figure 402/TASK 21-52-32-991-002
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TASK 21-52-32-400-001
Installation of the Condenser 10HM2 (11HM2)
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 condensor 10HM2 (11HM2).
____
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. 04-007 USA MIL-M-7866
MOLYBDENUM DISULFIDE POWDER (Ref. 20-31-00) Material No. 04-012 USA VV-P-236
PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 06-007 USA SS-G-659
GRAPHITE POWDER DRY LUBRICANT (Ref. 20-31-00) Material No. 19-009 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA
(Ref. 20-31-00)
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C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 packing
5 packing
5 packing
6 nuts
6 nuts
7 washers
7 washers
9 seal
9 seals
9 seal
9 seals
9 seal
9 seals
9 seal
9 seals
9 seal
9 seals
16 packing
16 packing
16 packing
20 sleeve
20 sleeve
20 sleeve
21 packing
21 packing
21 packing
22 packing
22 packing
23 sleeve
23 sleeve
23 sleeve
25 packing
25 packing
21-52-03 26 -10021-52-03 26 -100A21-52-03 26A-10021-52-03 26 -14021-52-03 26A-14021-52-03 26 -15021-52-03 26A-15021-52-03 26 -18021-52-03 26 -18021-52-03 26 -180A21-52-03 26 -180A21-52-03 26 -180B21-52-03 26 -180B21-52-03 26 -180C21-52-03 26 -180C21-52-03 26A-18021-52-03 26A-18021-52-03 26 -04021-52-03 26 -040A21-52-03 26A-04021-52-03 08 -01021-52-03 11A-01021-52-03 11B-01021-52-03 26 -12021-52-03 26 -120A21-52-03 26A-12021-61-03 06 -02021-61-03 06 -020A21-52-03 08 -01021-52-03 11A-01021-52-03 11B-01021-61-03 06 -02021-61-03 06 -020A
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D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 12-33-21-618-001 20-26-00-910-002 21-52-00-200-003 Pre-conditioning through the HP Ground ConnectionPre-conditioning with the APUInstallation of Expansion JointsDetailed Visual Inspection of the Anti-Ice Valve Sense-Lines
21-52-43-000-001 Removal of the Pack Downstream Check-Valves 15HM and
16HM
21-52-43-400-001 Installation of the Pack Downstream Check-Valves 15HM
and 16HM
21-63-00-710-004 24-41-00-861-002 Operational Test of the Cockpit and Cabin Temperature Control with CFDS/MCDUEnergize 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
53-35-13-400-002 Belly Fairing StructureInstallation 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,
R 21-52-32-991-001 **ON A/C 401-499, Fig. 401
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