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时间:2011-03-27 12:37来源:蓝天飞行翻译 作者:航空
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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)
 1EFF : ALL 1 57-20-00Page 635 1 1 Aug 01/05R 1 1 1CES 1


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 572100 (for corrective action) R 57-20-00-991-006 Fig. 607
 3. Job Set-up
__________
 Subtask 57-20-00-941-054

 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (3)
 Put warning notices in the cockpit to tell persons not to operate the flaps or slats.

 (4)
 Put the access platform below the applicable wing rear spar, zone 574(674).


 4. Procedure
_________ R (Ref. Fig. 607/TASK 57-20-00-991-006) Subtask 57-20-00-110-055
 A. Preparation for Inspection
 (1) Use a clean MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026), to clean:
 -the rear spar aft-face between RIB1 and RIB5.


R  Details of the Rear-Spar Aft Face - RIB1 thru RIB5 Figure 607/TASK 57-20-00-991-006
 1EFF : 1 1 1CES  ALL  1 111 57-20-00 Page 637 Aug 01/05

 

 Subtask 57-20-00-210-054
 B. Detailed Inspection of Outer Wing, Rear Spar Aft Face, Between RIB1 and Gear Support RIB5, including Rear Spar Angle
 (1)
 Examine the rear spar aft face between RIBS 1 and 5, together with the rear spar angle, and make sure that:

 -
there is no corrosion or damage

 -
there are no scratches or scores

 -
there are no cracks

 -
there are no loose or damaged fasteners


 -the surface protection is in the correct condition.

 (2)
 If necessary, refer to the ASRM (Ref. ASRM 572100) for the correct repair procedure.


 5. Close-up
________ Subtask 57-20-00-942-055
 A. Removal of Equipment
 (1)
 Remove the safety barriers

 (2)
 Remove the access platform(s).

 (3)
 Remove the warning notice(s).

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


 1EFF : ALL 1 57-20-00Page 638 1 1 Aug 01/05R 1 1 1CES 1


 TASK 57-20-00-200-006
 Special Detailed Inspection of the Outer Wing Rear-Spar Aft-Face Spar Joint Plate at RIB6
 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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 572008-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notices No specific access platform 2 m (6 ft. 7 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
 1EFF : ALL 1 57-20-00Page 639 1 1 Aug 01/05R 1 1 1CES 1


 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 064157 P. Block 1
 NTM 57-20-08 PART 9
 ASRM 572100 (for corrective action)

R 57-20-00-991-007 Fig. 608
 3. Job Set-up
__________
 Subtask 57-20-00-941-055

 A. Safety Precautions
 (1)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
 
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