• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:50来源:蓝天飞行翻译 作者:航空
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

Material No. 08-061A D DAN 220
 ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
 Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground
 27-50-00-866-009 Retraction of the Flaps on the Ground

R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 401-499,
 57-52-00-991-035-B Fig. 631
 **ON A/C 051-052,
 57-52-00-991-035-C Fig. 631A
 **ON A/C 301-399,
 57-52-00-991-035-A Fig. 631B **ON A/C ALL


 3. Job Set-up
__________ Subtask 57-52-00-941-085
 A. Safety Precautions
 (1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
 (2) Put the safety barriers in position. Subtask 57-52-00-860-109
 B. Aircraft Maintenance Configuration 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.
 (1)
 Fully extend the flaps (Ref. TASK 27-50-00-866-008).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.


 Subtask 57-52-00-865-115
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 57-52-00-010-088
 D. Get Access
 (1) Put the access platform in position below the applicable inboard flap.
 1EFF : ALL 1 57-52-00Page A686 1 1 May 01/05R 1 1 1CES 1


 4. Procedure
_________
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 631/TASK 57-52-00-991-035-B)
 **ON A/C 051-052,

 (Ref. Fig. 631A/TASK 57-52-00-991-035-C)
 **ON A/C 301-399,
 (Ref. Fig. 631B/TASK 57-52-00-991-035-A)
 **ON A/C ALL
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
 EDGE:

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.


 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 Subtask 57-52-00-210-068
 A. Inspection of Inboard Flap, Bottom Surface, Drain Holes and Inspection Holes
 (1)
 Examine the inboard flap, bottom surface drain holes. Make sure that:

 -there are no covers installed on the drain holes
 -the drain holes are not blocked.

 (2)
 If a drain hole is blocked, remove all unwanted material from around the hole. Use a 5.0mm (0.2 in.) dia. non-metallic probe to remove the blockage from the hole.

 (3)
 Examine the inboard flap, bottom surface inspection holes. Make sure that:

 -
the covers are correctly installed on each inspection hole

 -
the covers are in good condition.

 

 


 Inboard Flap, Bottom Surface, Drain Holes and Inspection Holes Figure 631/TASK 57-52-00-991-035-B
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 57-52-00Page A688 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Inboard Flap, Bottom Surface, Drain Holes and Inspection Holes R Figure 631A/TASK 57-52-00-991-035-C


R 1EFF : 051-052, 1 57-52-00Page A689 1 1 May 01/05 1 1 1CES 1


 Inboard Flap, Bottom Surface, Drain Holes and Inspection Holes R Figure 631B/TASK 57-52-00-991-035-A
R 1EFF : 301-399, 1 57-52-00Page A690 1 1 May 01/05 1 1 1CES 1


 Subtask 57-52-00-960-050

 B. Replace Defective or Missing Inspection Hole Covers
 (1)
 Remove and discard the damaged inspection hole cover(s).

 (2)
 Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the external surfaces around the applicable inboard flap, bottom surface inspection hole(s).

 (3)
 Use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A) cut to the correct dimensions, to make new cover(s) for the applicable inspection hole(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4(60)