A320飞机维护手册 AMM WINGS 机翼3(112)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  -------------------------------------------------------------------------------
R  REFERENCE DESIGNATION 
R  -------------------------------------------------------------------------------
R  ASRM 512100 (for corrective action) 
R  ASRM 572111 (for corrective action) 
R  57-51-00-991-029 Fig. 622 
R  3. Job Set-up__________ 
R  Subtask 57-51-00-941-084 
R  A. Safety Precautions 
R  (1) Put warning notices in the cockpit to tell persons not to operate the 
R  flaps or slats. 
R  (2) Put the safety barriers in position. 
R  (3) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) 
R  on the flap/slat control lever. 
R  Subtask 57-51-00-865-109 
R  B. Open, safety and tag this(these) circuit breaker(s): 
R  -------------------------------------------------------------------------------
R  PANEL DESIGNATION IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 
R  121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21

 

R Subtask 57-51-00-010-087

R  C. Get Access 
R  (1) Put the access platform below the applicable wing trailing edge at 
R  the MLG support RIB5, zone 574(674). 
R  (2) Open the applicable access panels: 
R  - for the left wing, open 574AB, 574BB 
R  - for the right wing, open 674AB, 674BB. 
R  4. Procedure_________ 
R  (Ref. Fig. 622/TASK 57-51-00-991-029) 
R  Subtask 57-51-00-110-092 
R  A. Preparation for Inspection 
R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______ 
R  EDGE: 
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. 
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. 
R  - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. 
R  INCORRECT INSTALLATION CAN CAUSE DAMAGE. 
R  (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING 
R  AGENTS (Material No. 11-026) to clean: 
R  - the wing bottom skin panel No. 3 upper surface (between the rear 
R  spar and false rear spar and between the gear support RIB5 and 
R  RIB8). 
R  Subtask 57-51-00-210-075 
R  B. Inspection 
R  NOTE : Make sure the area of the bottom skin panel along the____ 
R  inboard/outboard lower RIB6A foot (between the inner rear spar aft 
R  face and false rear spar forward face) is carefully examined. 
R  (1) Inspect the bottom skin panel No. 3 upper surface (between the rear 
R  spar and false rear spar and between the gear support RIB5 and RIB8). 
R  Make sure that: 
R  - there is no damage 
R  - there are no cracks and/or scores 
R  - there is no corrosion 
R  - the surface protection is in the correct condition.

 

R R  Outer Wing - Bottom Skin Panel No. 3 Figure 622/TASK 57-51-00-991-029
 1EFF : 1 1 1CES  ALL  1 111 57-51-00 Page A635 Nov 01/04

 

R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 572111) for the____ 
R  correct repair procedure. 
R  5. Close-up________ 
R  Subtask 57-51-00-916-050 
R  A. Application of Corrosion Protection Material 
R  (1) Apply a new layer of surface protection material to the bottom skin 
R  panel No. 3 upper surface (between the rear spar and false rear spar 
R  and between the gear support RIB5 and RIB8) (Ref. ASRM 512100). 
R  Subtask 57-51-00-410-086 
R  B. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Close the applicable access panels: 
R  - for the left wing, close 574AB, 574BB 
R  - for the right wing, close 674AB, 674BB. 
R  Subtask 57-51-00-865-110 
R  C. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  6CV, 8CV. 
R  Subtask 57-51-00-942-085 
R  D. Removal of Equipment 
R  (1) Remove the access platform(s). 
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM WINGS 机翼3(112)