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时间:2011-03-25 17:53来源:蓝天飞行翻译 作者:admin
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

 Carefully remove the secondary hinged fairing (2). If necessary, use a wedge - non metallic to loosen the seal to release the secondary hinged fairing.

 (5)
 Loosely attach the nuts (5) and (9) and the bolts (7) and (10) to the secondary hinged fairing (2).


 1EFF : ALL 1 32-12-13Page 408 1 1 Aug 01/05 1 1 1CES 1 TASK 32-12-13-400-001


 Installation of a Replacement Secondary Hinged Fairing
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific ground hydraulic cart
 No specific safety barriers
 No specific warning notice
 No specific access platform 2.5 m (8 ft. 2 in.)
 No specific access platform 3 m (9 ft. 10 in.)

R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft)
 1EFF : ALL 1 32-12-13Page 409 1 1 May 01/05 1 1 1CES 1 B. Consumable Materials


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire, corrosion resistant steel, 0.8mm
 (0.032in.)
 Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A
 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (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)
 Material No. 19-005
 WAX CRAYON (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 cotter pin 52-81-11 01A-010 4 cotter pin 52-81-11 01L-010 R 4 cotter pin 52-81-11 01M-010 8 cotter pins 52-81-11 01A-010 8 cotter pins 52-81-11 01L-010 R 8 cotter pins 52-81-11 01M-010
 1EFF : ALL 1 32-12-13Page 410 1 1 May 01/05 1 1 1CES 1 D. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001 Lifting for Aircraft Maintenance Operations 07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations 20-28-00-912-004 Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action 29-10-00-864-001 Depressurize the Green Hydraulic System 32-00-00-481-001 Installation of the Safety Devices on the Landing
 Gears 32-00-00-481-002 Installation of the Safety Devices on the Landing Gear Doors 32-00-00-860-002 Ground Configuration after Flight Configuration with
 Electrical Power 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-12-14-400-001 Installation of the MLG Fixed Fairing Assembly (That
 was Removed For Access Only)
 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening
 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing
 32-31-00-720-002 Functional Test of the Normal Extension and

 Retraction of the Landing Gear
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 32-12-13-991-001 Fig. 401
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 32-12-13-991-001-A Fig. 401A
 1EFF : ALL 1 32-12-13Page 411 1 1 Aug 01/05 1 1 1CES 1

 **ON A/C ALL


 3. Job Set-up
__________
 Subtask 32-12-13-941-053
 A. Safety Precautions
 
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