• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:47来源:蓝天飞行翻译 作者:admin
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

 

 (4)
 If you find damage to the surface protection:

 (a)
 Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data about the paint coating of the aircraft.

 (b)
 Repair the damage to the paint system (Ref. TASK 51-75-12-300-001) or (Ref. TASK 51-75-12-300-003), as necessary.

 

 


R  **ON A/C 301-399, 
R  Subtask 53-31-00-210-084-B 
R  A. Inspection Procedure 
R  (1) Do a general visual inspection of the external surfaces of the upper 
R  skins of the longitudinal lap joints and the crack stopper areas. Do 
R  this at STGR6 LH/RH, between FR35.8 and FR47: 
R  (a) Look for scratches, dents, cracks, corrosion and damage to the 
R  surface protection. 
R  (2) If you find scratches, dents and/or cracks: 
R  (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification 
R  of the damage. 
R  (b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable 
R  damage limits for this structure. 
R  (c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
R  300-001) or (Ref. TASK 51-73-11-300-004), as necessary. 
R  (d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
R  003). 
R  (e) For damage that is more than the limits for minor damage, refer 
R  to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data. 
R  (3) If you find corrosion: 
R  (a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general 
R  corrosion data. 
R  (b) Repair the corroded areas (Ref. TASK 51-74-11-300-001) or 
R  (Ref. TASK 51-74-11-300-002), as necessary. 
R  (4) If you find damage to the surface protection: 
R  (a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data 
R  about the paint coating of the aircraft. 
R  (b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
R  001) or (Ref. TASK 51-75-12-300-003), as necessary. 

 CES  **ON A/C ALL


 5. Close-up
________ Subtask 53-31-00-942-076
 A. Remove the Ground Support Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the access platform(s).

 


 TASK 53-31-00-210-036
 General Visual Inspection of Upper Skin of Longitudinal Lap Joints and Crack Stopper Areas at STGR18 LH/RH, between FR35(FR35.8) and FR47, External Surface
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______ FALL CAN INJURE OR KILL YOU.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 533125-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 EFF : ALL  53-31-00Page A689

May 01/04
R
 CES


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-73-11-300-001 Repair of Minor Damage on Aluminum Clad Components 51-73-11-300-003 Repair of Dents in Skin Panels 51-73-11-300-004 Repair of Minor Damage on Unclad Components 51-74-11-300-001 Repair of Corroded Areas 51-74-11-300-002 Removal of the Corrosion on Unpainted Light Alloy 51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
 
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 FUSELAGE 机身2(89)