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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

 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 57-52-00-860-084
 C. Aircraft Configuration
 (1) Retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-52-00-942-056
 D. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the warning notice(s).

 (3)
 Remove the safety barriers.

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 621 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


 INTENTIONALLY BLANK

R 1 1
57-52-00Page 622
1 1 May 01/05 1 1 1CES 1

R **ON A/C ALL


 TASK 57-52-00-200-005
 Detailed Visual Inspection of Outer Wing Inboard Flap Track 2 Carriage Forging
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 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.
 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
__________________
 Refer to the MPD TASK: 575250-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) R No specific clamp R No specific protective pad
 No specific safety barriers No specific warning notices R No specific access platform 2.5 m (8 ft. 2 in.)


 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  Material No. 11-026 Material No. 19-003  GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  27-50-00-866-008 27-50-00-866-009 27-54-61-000-001 27-54-61-000-003 27-54-61-400-001 27-54-61-400-003 27-60-00-866-002 57-55-11-010-001 57-55-11-410-001 ASRM 575100 57-52-00-991-005  Extension of the Flaps on the GroundRetraction of the Flaps on the GroundRemoval of the Inboard Flap Removal of the Inboard Double-Slotted FlapInstallation of the Inboard Flap Installation of the Inboard Double-Slotted FlapExtension-Retraction of the Spoilers for MaintenanceTo Lower the Flap Track No. 2 Movable Fairing for AccessTo Lift the Flap Track No. 2 Movable Fairing after Access(for corrective action)Fig. 605
 3. Job Set-up__________
 Subtask 57-52-00-941-058
 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 57-52-00-860-085
 B. Aircraft Maintenance Configuration
 (1)
 Extend the spoilers (Ref. TASK 27-60-00-866-002).

 (2)
 Extend the flaps fully (Ref. TASK 27-50-00-866-008).

 (3)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.

 (4)
 Put the access platform below the applicable wing trailing edge at flap track 2, zone 531 (631).


 Subtask 57-52-00-865-064
 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
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 
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