-
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
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
 No specific brush
 No specific safety barriers
 No specific warning notices

R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-001  USA MIL-S-8802 TYPE I CLASS A
 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)

 Material No. 09-002  USA MIL-S-8802 TYPE I CLASS B
 FUEL TANK SEALANTPOLYSULFID(NO LONGER AVAILABLE
 (Ref. 20-31-00)

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

 Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING 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)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 20-28-00-912-002 Electrical Bonding of Components With Conductive Bolts and Screws in 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 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank
R  28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank 28-42-00-740-001 Status Report (BITE) 28-46-00-740-001 Functional (BITE) Test 57-27-11-000-001 Removal of the Access Panel (540AB, 540BB, 540CB,
 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB) 57-27-11-000-005 Removal of the Access Panel 521AZ(621AZ), 521BZ(621BZ), 521CZ(621CZ)

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
57-27-11-400-001  Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
 57-27-11-400-005 Installation of the Access Panel 521AZ(621AZ),
 521BZ(621BZ), 521CZ(621CZ)
 57-27-11-991-008 Fig. 406

 3. Job Set-up
__________
 Subtask 57-27-11-941-066

 A. Safety Precautions WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
R (1) You must obey the fuel safety procedures when you do work in a fuel R tank, (Ref. TASK 28-10-00-910-001) and (Ref. TASK 28-10-00-910-002).
 (2)
 Make sure the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed correctly on the flap/slat control lever.

 (3)
 Make sure that the safety barriers are in position.

 (4)
 Make sure the warning notices are in position in the cockpit to tell persons not to operate the flaps or slats.

 (5)
 Make sure the access platform is in position below the wing fuel tank, zone 540(640).

 Subtask 57-27-11-860-069
 B. Aircraft Maintenance Configuration
 (1)
 Make sure the aircraft has been defuelled (Ref. TASK 28-25-00-650-001).

 (2)
 Make sure the applicable fuel tank(s) have been drained (Ref. TASK 28-25-00-650-003).

 (3)
 Make sure the access panel 540BB(640BB) has been removed (Ref. TASK 57-27-11-000-001).

 (4)
 Make sure the access panels 521AZ(621AZ), 521BZ(621BZ) and 521CZ(621CZ) have been removed (Ref. TASK 57-27-11-000-005).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼2(83)