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时间:2011-03-21 14:21来源:蓝天飞行翻译 作者:admin
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 Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
58 cotter pins 27-54-05 35C-040H 58 cotter pins 27-54-05 35C-040J 58 cotter pins 27-54-05 35C-040K 58 cotter pins 27-54-05 35C-040L 58 cotter pins 27-54-05 35H-040 137 cotter pins 27-54-46 06B-035 138 crushable spacers 27-54-46 06B-080 155 cotter pin 57-53-21 03 -340 155 cotter pin 57-53-21 03B-340 155 cotter pin 57-53-21 03B-340A
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-62Page 414 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 D. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)-
27-50-00-000-002  Removal of the Inboard and Outboard Flap
 Hoisting-Sling
 27-50-00-400-002  Installation of the Inboard and Outboard Flap
 Hoisting-Sling
 27-50-00-866-011  Manual Extension of the Flaps
 27-50-00-866-012  Manual Retraction of the Flaps
 27-51-00-820-003  To Do a Check of the Flap Rigged Position (With the
 Sharks Fin)
 27-51-00-820-008  Adjustment of the Flap Rigged Position With the
 Sharks Fin Tool (A318/319/320)
 27-51-44-400-001  Installation of the Interconnecting Strut
 27-54-00-710-001  Operational Test of the Flap System
 27-54-61-000-002  Removal of the Flap Kink-Seals
 27-54-61-400-006  Installation of the Flap Kink-Seals
 27-54-62-000-001  Removal of the Outboard Flap
 27-54-62-400-001  Installation of the Outboard Flap
 27-54-63-000-001  Removal of the Flap Guide-Roller Assembly
 27-54-63-400-001  Installation of the Flap Guide-Roller Assembly
 27-60-00-866-002  Extension-Retraction of the Spoilers for Maintenance
 27-64-00-710-001  Operational Test of the Spoiler Hydraulic Actuation
 27-64-00-820-001  Adjustment of the Spoilers
 57-51-37-000-002  Removal of the Access Panels 573AB(673AB),
 573BB(673BB), 573CB(673CB)
 57-51-37-000-004  Removal of the Access Panels
 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB
 (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
 57-51-37-400-002  Installation of the Access Panels 573AB(673AB),
 573BB(673BB), 573CB(673CB)
 57-51-37-400-004  Installation of the Access Panels
 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB
 (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
 57-55-11-010-002  To Lower the Flap Track No. 3 & No. 4 Movable
 Fairings for Access
 57-55-11-410-002  To Lift the Flap Track No. 3 & No. 4 Movable Fairings
 after Access
 27-54-62-991-009  Fig. 402
 27-54-62-991-010  Fig. 403
 27-54-62-991-014  Fig. 404 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-62Page 415 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


27-54-62-991-016 Fig. 405 27-54-62-991-013 Fig. 406 27-54-62-991-003-A Fig. 407 27-54-62-991-017 Fig. 408
 3. Job Set-up
__________
 Subtask 27-54-62-941-060
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notices are in position to tell persons not to pressurize the hydraulic system.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.


 Subtask 27-54-62-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
 
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