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时间:2011-03-27 12:40来源:蓝天飞行翻译 作者:航空
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 (3) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (3)
 Examine the pylon rear attachment and adjacent structure for:


 -cracks
 -damaged paint and sealant
 -distortion
 -correct condition of all fasteners and safety devices.


 Subtask 57-26-12-420-050-A
 B. Installation of the Pylon Rear Attachment Bearing
 WARNING : DO NOT GET THE COMPOUND ON YOUR SKIN.

_______
 IF YOU DO:

 -RUB IT OFF IMMEDIATELY WITH A CLEAN CLOTH
 -WASH THE SKIN WITH SOAP AND RINSE WITH CLEAN WATER.
 (1) Apply SEALANTS (Material No. 09-005) to the interface of the bearing
 (4) and the pylon rear attachment.
 NOTE : The sealant must still be wet when you install the bearing (4)

____
 in the pylon attachment.

 (2) Install the bearing (4), or a new bearing (4) if applicable, in the pylon rear attachment (3).
 NOTE : The bearing (4) must be installed from the front.
____
 (3)
 Install the new tab washer (2). Make sure that the internal tag of the washer (2) is engaged in the slot on the bearing (4).

 (4)
 If the slotted nut (1) was found to be damaged, replace it with a new slotted nut (1).


 NOTE : Put a small bend in the tabs of the tab washer (2) before you
____ install the slotted nut (1). This will make it easier to bend the tabs when you subsequently lock the slotted nut.
 (5)
 Install the slotted nut (1) on the bearing (4) with the chamfered face against the tab washer (2).

 (6)
 Hold the bearing (4) with the SPANNER - PYLON PICK-UP (98D57004027000). TORQUE the slotted nut (1) with the SOCKET - PYLON PICK-UP (98D57004026000) to between 15 and 21 m.daN (110.61 and

 154.86 lbf.ft).

 (7)
 Safety the slotted nut (1) with the tab washer (2).


 1EFF : ALL 1 57-26-12Page 409 1 1 May 01/04R 1 1 1CES 1


 5. Close-up
________ Subtask 57-26-12-410-050
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable aft attach fitting (Ref. TASK 54-51-17-400-002).


 Subtask 57-26-12-942-050
 B. Removal of Equipment
 (1)
 Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) from the flap/slat control lever.

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the access platform(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 


 ATTACHMENT - MAIN LANDING GEAR - REMOVAL/INSTALLATION
_____________________________________________________
 TASK 57-26-13-000-001
 Removal of the Bearing Assembly of the Forward Pintle Pin
 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 : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific plastic spatula No specific safety barriers No specific warning notices No specific access platform 3 m (9 ft. 10 in.) 98D57004003000 1 SOCKET-RING (FOR NUT OF FWD PINTLE BEARING)
 1EFF : ALL 1 57-26-13Page 401 1 1 May 01/05R 1 1 1CES 1


 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 32-00-00-481-002 32-11-11-000-001  Installation of the Safety Devices on the Landing GearsInstallation of the Safety Devices on the Landing Gear DoorsRemoval of the MLG Leg Assembly 
R  **ON A/C 051-052, 
R  57-26-13-991-001-A  Fig. 401 
R  **ON A/C ALL 
R  Post SB  57-1104 For A/C 051-052, 
R  57-26-13-991-001  Fig. 401A 
R  **ON A/C ALL
 
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