A320飞机维护手册 AMM LANDING GEAR 起落架1(125)_航空信息_民用航空_通用航空

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28 washer 32-11-11 66D-100
28 washer 32-11-11 66F-100
30 laminated shims 32-11-11 66F-095
31 O-ring 32-11-05 02 -140
31 O-ring 32-11-05 02A-140
31 O-ring 32-11-05 02B-140
32 laminated shims 32-11-11 66F-095
34 cotter pin 32-11-11 66A-070
34 cotter pins 32-11-11 66A-070
34 cotter pin 32-11-11 66D-070
34 cotter pins 32-11-11 66D-070
34 cotter pin 32-11-11 66F-070
34 cotter pins 32-11-11 66F-070
36 O-ring 32-11-05 02 -140
36 O-ring 32-11-05 02A-140
36 O-ring 32-11-05 02B-140
36 cotter pins 32-11-11 66A-070
36 cotter pins 32-11-11 66D-070
36 cotter pins 32-11-11 66F-070
38 O-ring 32-11-05 06B-140
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------

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07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations 11-00-00-400-012 Installation of the Labels on Landing Gear 12-12-32-611-004 Check Fluid Level of Main Landing Gear Shock Absorber 12-22-32-640-001 Lubrication of the MLG and Doors 20-21-11-911-001 Tightening Torques for Standard Threaded Fasteners 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
1EFF : ALL 1 32-11-11Page 436 1 1 Aug 01/05R 1 1 1CES 1

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REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
27-54-45-400-004 Installation of the Torque Shaft 6208CM(6258CM)
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
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-23-00-860-002 Connection of the Isolation Coupling of the Power
Transfer Unit (PTU)
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
32-00-00-860-001 Flight Configuration Precautions with Electrical
Power
32-00-00-860-002 Ground Configuration after Flight Configuration with
Electrical Power
32-11-16-400-001 Installation of the MLG Side-Stay Assembly 2505GM,
2506GM
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
32-12-13-000-001 Removal of the Secondary Hinged Fairing
32-12-13-400-002 Installation of the Secondary Hinged Fairing (That
was Removed for Access Only)
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
32-31-46-400-001 Installation of the MLG Actuating Cylinder
32-33-00-720-001 Functional Check of Free-Fall Extension
32-42-00-710-001 Operational Check of the Normal Braking System
32-42-00-720-002 Functional test of the tachometers
32-42-00-870-001 Bleeding of the Normal Braking at the Brake Units
32-42-27-400-001 Installation of the Brake
(2641GM,2642GM,2643GM,2644GM)
32-43-00-710-001 Operational Check of Alternate Braking System