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时间:2011-02-11 09:59来源:蓝天飞行翻译 作者:admin
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32-11-00-200-006 
R R  32-11-00-220-004 32-11-11-000-001 32-11-11-400-001 32-11-13-000-001 32-11-13-400-001 32-11-16-000-001 32-11-16-400-001 
32-11-17-000-001 32-11-17-400-001 32-11-21-000-001 32-11-21-400-001 32-12-00-010-001 32-12-00-410-001 

Inspection After Brake OverheatInspection/Check of the Leveling and Measurement after Abnormal Operation of the AircraftLifting for Aircraft Maintenance OperationsLifting of the Aircraft at Forward Jacking Point, MLG Wheels on the GroundLowering of the Aircraft at Forward Jacking Point, MLG Wheels on the GroundLowering of the Aircraft for Maintenance Operations Check Shock Absorber Charge PressureDe-energize the Aircraft Electrical Circuits Supplied from the External PowerExtension of the Flaps on the GroundRetraction of the Flaps on the GroundAccess to the Fuel Tanks and the Work AreasPressure DefuelPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionInstallation of the Safety Devices on the Landing GearsCheck the Charge Pressure of the Main Landing Gear Shock AbsorberInspection of the MLG after the Aircraft has gone off the RunwayInspection of the MLG Axles after the Aircraft has gone off the Runway Inspection of the MLG Side Stay Attachment Lug(s) after the Aircraft has gone off the RunwayRemoval of the MLG Leg AssemblyInstallation of the MLG Leg AssemblyRemoval of the MLG Shock AbsorberInstallation of the MLG Shock AbsorberRemoval of the MLG Side-Stay Assembly 2505GM, 2506GMInstallation of the MLG Side-Stay Assembly 2505GM, 2506GMRemoval of the MLG Lock StayInstallation of the MLG Lock StayRemoval of the MLG Lockstay Actuating CylinderInstallation of the MLG Lockstay Actuating CylinderOpen the Main Gear Doors for AccessClose the Main Gear Doors after Access


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REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-21-00-200-005 32-21-00-200-006 32-21-11-000-002 32-21-11-400-002 32-21-13-000-001 32-21-13-400-001 32-21-16-000-002 32-21-16-400-002 32-21-17-000-001 32-21-17-400-001 32-22-00-010-001 32-22-00-410-001 32-31-00-720-002
32-31-00-720-003
32-31-22-000-001 32-31-22-400-001 32-31-46-000-001 32-31-46-400-001 R 32-33-00-720-001 32-41-12-000-001 32-41-12-000-002 32-41-12-400-001 32-41-12-400-002 71-00-00-000-042 71-00-00-400-042 71-13-00-010-040 71-13-00-410-040 72-00-00-200-006
78-31-00-710-042 78-36-00-010-040 78-36-00-410-040 05-51-24-991-002 05-51-24-991-003 05-51-24-991-004 Detailed Inspection/Check of the NLGInspection/Check of the Barrel/Drag struct connectionRemoval of the NLG Leg Assy (2526GM)Installation of the NLG Leg Assy (2526GM)Removal of the NLG Shock Absorber AssyInstallation of the NLG Shock Absorber AssyRemoval of the NLG Drag Strut Assy (2528GM)Installation of the NLG Drag Strut Assy (2528GM)Removal of the NLG Lockstay AssyInstallation of the NLG Lockstay AssyNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors ClosingFunctional Test of the Normal Extension and Retraction of the Landing GearFunctional Test of the Normal Extension and Retraction of the Nose Landing GearRemoval of the NLG Actuating Cylinder (2527GM)Installation of the NLG Actuating Cylinder (2527GM)Removal of the MLG Actuating CylinderInstallation of the MLG Actuating Cylinder Functional Check of Free-Fall ExtensionRemoval of the NLG Wheel (2659GM,2660GM)Removal of the Axle SleeveInstallation of the NLG Wheel (2659GM,2660GM)Installation of the Axle SleeveRemoval of the Power PlantInstallation of the Power PlantOpening of the Fan Cowl DoorsClosing of the Fan Cowl DoorsInspection/Check of Foreign Objet Damage (FOD) (Bird Strike Included)Operational Test of the Thrust Reverser SystemOpening of the Thrust Reverser DoorsClosing of the Thrust Reverser DoorsFig. 601Fig. 602Fig. 603


 3. Job Set-up__________
 Subtask 05-51-24-481-050 
R  A. Safety Precautions 
R R  (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
 (2) Put the warning notices in the cockpit to tell persons not to operate the aircraft systems.
 Subtask 05-51-24-860-050
 B. Aircraft Maintenance Configuration
 (1) Make sure that the Hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
 (2) Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
 Subtask 05-51-24-010-050
 C. Get Access
 (1) Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-001).
 (2) Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-001). 
R  (3) Put an access platform in position.
 Subtask 05-51-24-866-050
 D. Extension of the Flaps
 (1) Fully extend the flaps (Ref. TASK 27-50-00-866-008).


 
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