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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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_______ GEAR.
 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.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific warning notices No specific access platform 3.0 m (9 ft. 10 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 1EFF : ALL 1 27-54-62Page 483 1 1 May 01/05R 1 1 1CES 1


 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-012  USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (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
 CMM 575321

 **ON A/C 001-049, 051-056, 301-399,
 27-54-62-991-031  Fig. 423
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
 27-54-62-991-031-A  Fig. 423A **ON A/C ALL


 3. Job Set-up
__________
 Subtask 27-54-62-941-062

 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notices is 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 27-54-62-860-063
 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)
 Make sure that the flaps are extended fully (Ref. TASK 27-50-00-866-008).

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

 (3)
 Make sure that the access platform is below the applicable flap.


 4. Procedure
_________
 **ON A/C 001-049, 051-056, 301-399,

 (Ref. Fig. 423/TASK 27-54-62-991-031) R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 423A/TASK 27-54-62-991-031-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.
 Subtask 27-54-62-420-097
 A. Preparation for Installation
 (1)
 Do an inspection of the component interface and/or the adjacent area.

 (2)
 Clean the interface of the leading edge panel (2) and the outboard flap with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 

R **ON A/C 001-049, 051-056, 301-399,
 Subtask 27-54-62-420-066
 B. Installation of the Leading Edge Panels 2 and 5 on the Outboard Flap
 (1)
 Apply a layer of SEALANTS (Material No. 09-016) to the interface of the leading edge panel (2) and the outboard flap.

 (2)
 Apply a layer of COMMON GREASE (Material No. 04-012) to the contact areas of the leading edge panel (2).

 (3)
 Install the leading edge panel (2) with the screws (1).
 
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