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时间:2011-03-26 23:42来源:蓝天飞行翻译 作者:admin
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20-22-00-400-001  Installation of STA-LOK Nuts and Lockwashers
 20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
25-23-46-400-002 Installation of the Door Linings at the AFT Passenger/Crew Doors R 25-62-44-400-001 Installation of the Escape-Slide Pack-Assembly 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight
 (98D52103501000) for Escape Slide/Raft 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
 Door
 1EFF : ALL 1 52-13-21Page 435 1 1 Feb 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door 52-13-21-220-001 Detailed Visual Inspection of the Door Locking Mechanism 52-13-21-820-001 Adjustment of the Locking Hook of the Aft
 Passenger/Crew Door 52-13-31-400-001 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 56-31-13-400-002 Installation of the Window of the AFT Passenger/Crew
 Door
 52-13-21-991-010 Fig. 402
 52-13-21-991-006 Fig. 403
 52-13-21-991-008 Fig. 404
 52-13-21-991-005 Fig. 405
 52-13-21-991-012 Fig. 406
 52-13-21-991-014 Fig. 407
 52-13-21-991-016 Fig. 409
 52-13-21-991-018 Fig. 410
 52-13-21-991-020 Fig. 411
 52-13-21-991-009 Fig. 412
 52-13-21-991-022 Fig. 413
 52-13-21-991-013 Fig. 414

 **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 52-13-21-991-030 Fig. 415
R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 52-13-21-991-030-A Fig. 415A
 **ON A/C ALL
 52-13-21-991-017 Fig. 416
 52-13-21-991-019 Fig. 417
 52-13-21-991-021 Fig. 418
 52-13-21-991-011 Fig. 419

 1EFF : ALL 1 52-13-21Page 436 1 1 Aug 01/05 1 1 1CES 1


 3. Job Set-up
__________
 Subtask 52-13-21-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is in position at the applicable passenger/crew door.

 (2)
 Make sure that the door lining and the insulation are removed.

 (3)
 Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).


 Subtask 52-13-21-865-058
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
 Subtask 52-13-21-110-050
 C. Cleaning
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
 MATERIAL.
 THIS MATERIAL IS DANGEROUS.

 (1) Clean the component interface and/or the adjacent area.
 1EFF : ALL 1 52-13-21Page 437 1 1 Nov 01/00R 1 1 1CES 1


 INTENTIONALLY BLANK

R 1 1
52-13-21Page 438
1 1 Nov 01/00 1 1 1CES 1


 (2)
 If necessary, clean the components with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Make sure that the parts retained from the removed component are clean and in the correct condition. (Ref. TASK 52-13-21-220-001).


 4. Procedure
_________ Subtask 52-13-21-420-050
 A. Installation of the Inner Control Handle
 (Ref. Fig. 403/TASK 52-13-21-991-006)

 (1)
 Apply COMMON GREASE (Material No. 04-004) on the axle (174) of the gearbox.
 
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