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时间:2011-03-26 23:38来源:蓝天飞行翻译 作者:admin
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 (Ref. 20-31-00)

 ANTI-CORROSION PRIMER (POLYURETHANE ) (Ref. 20-31-00)
GB BAEP 3536
 POLYURETHANE TOPCOAT GREY (FOR INTERNAL APPLIC.)
 (Ref. 20-31-00)
USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
6  cotter pin  52-11-11 09 -060
 7  cotter pin  52-11-11 07 -180
 20  cotter pin  52-11-11 18 -010
 37  cotter pin  52-11-11 09 -200
 45  cotter pin  52-11-11 09 -200
 68  cotter pin  52-11-11 07 -180
 71  cotter pin  52-11-11 06 -010
 76  cotter pin  52-11-11 09 -200
 85  cotter pin  52-11-11 07 -010
 97  cotter pin  52-11-11 02E-160
 101  cotter pin  52-11-11 08 -010
 106  cotter pin  52-11-11 08 -050

 1EFF : ALL 1 52-11-21Page 437 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
134 lockwasher 171 cotter pin 195 cotter pin 205 cotter pin 220 cotter pin 294 cotter pin 301 cotter pin 308 cotter pin 321 cotter pin 325 cotter pin 343 lockwasher 401 cotter pin 401 cotter pin 401 cotter pin 416 cotter pin 420 cotter pin 450 cotter pin 450 cotter pin 450 cotter pin 506 cotter pin 549 cotter pin 602 cotter pin
D. Referenced Information52-11-11 08 -37052-11-11 02E-01052-11-11 02E-48052-11-11 02E-16052-11-11 06 -01052-11-11 05 -01052-11-11 14 -23052-11-11 02E-16052-11-11 13 -01052-11-11 14 -15052-11-11 14 -34052-11-01 04C-15052-11-01 04G-15052-11-11 12 -06052-11-11 13 -01052-11-11 14 -01052-11-01 04C-15052-11-01 04G-15052-11-11 12 -06052-11-11 13 -17052-11-11 13 -01053-16-01 23A-020
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-22-00-400-001  Installation of STA-LOK Nuts and Lockwashers
 20-28-00-912-002  Electrical Bonding of Components With Conductive Bolts and Screws in the Tanks
 25-23-46-400-001 25-62-44-400-001 52-10-00-080-001 52-10-00-080-001 52-10-00-410-001 52-10-00-860-001  Installation of the Door Linings at the FWD Passenger/Crew DoorsInstallation of the Escape-Slide Pack-AssemblyRemoval of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape SlideRemoval of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide/RaftClosing of the Passenger/Crew DoorSpecial Precautions before Work on the Passenger/Crew Door

 1EFF : ALL 1 52-11-21Page 438 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door 52-11-21-220-001 Detailed Visual Inspection of the Door Locking Mechanism 52-11-21-820-001 Adjustment/Test of the Door Locking Mechanism of the
 FWD Passenger/Crew Door 52-11-31-400-001 Installation of the Lining Flap 52-71-00-820-002 Adjustment of the Proximity Switches (4WN1, 4WN2,
 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the CHECKING TOOL-DOORS 56-31-11-400-002 Installation of the Window of the Forward
 Passenger/Crew Door
 52-11-21-991-012 Fig. 401
 52-11-21-991-008 Fig. 402
 52-11-21-991-011 Fig. 403
 52-11-21-991-007 Fig. 404
 52-11-21-991-009 Fig. 405
 52-11-21-991-006 Fig. 406
 52-11-21-991-013 Fig. 407
 52-11-21-991-015 Fig. 408
 52-11-21-991-016 Fig. 409
 52-11-21-991-017 Fig. 410
 52-11-21-991-019 Fig. 411
 52-11-21-991-021 Fig. 412
 52-11-21-991-010 Fig. 413
 52-11-21-991-023 Fig. 414
 52-11-21-991-014 Fig. 415

 **ON A/C 001-049, 051-056,
 52-11-21-991-032 Fig. 416
R **ON A/C 057-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 52-11-21-991-032-A Fig. 416A
 **ON A/C ALL
 52-11-21-991-018 Fig. 417
 52-11-21-991-020 Fig. 418
 52-11-21-991-022 Fig. 419

 1EFF : ALL 1 52-11-21Page 439 1 1 Aug 01/05 1 1 1CES 1


 3. Job Set-up
__________
 Subtask 52-11-21-860-050
 A. Aircraft Maintenance Configuration
 
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