A320飞机维护手册 AMM 时间限制/维护检查 3(114)_航空信息_民用航空_通用航空

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After a flight crew report of a hard/overweight landing, you must do the
inspections that follow before the subsequent flight.
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific warning notices
No specific adjustable access platform 11 m (36 ft. 1 in.)

B. Referenced Information
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REFERENCE DESIGNATION
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05-56-00-200-001 Inspection/Check of the Leveling and Measurement
after Abnormal Operation of the Aircraft 07-11-00-581-001 Lifting for Aircraft Maintenance Operations 07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations 12-14-32-614-003 Check Charge Pressure of Main Landing Gear Shock
Absorber 12-14-32-614-004 Check Shock Absorber Charge Pressure 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-34-00-710-001 Operational Test of the Elevator and Hydraulic
Actuation
27-44-00-710-002 Operational Test of the Trimmable Horizontal Stabilizer Actuator with the Individual Hydraulic Systems
27-50-00-866-008 Extension of the Flaps on the Ground

R 31-37-00-200-001
R 32-00-00-481-001
R 32-11-00-200-004
R 32-11-00-200-005
32-11-00-200-006
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 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 Detailed Visual Inspection of the Transmission Assembly (Including Part of the Transmission in Zone 140)Operational Test of the Flap SystemExtension-Retraction of the Spoilers for MaintenanceExtending the Slats on the GroundAccess to the Fuel Tanks and the Work AreasPressure DefuelPut the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Check of the Load-Report Parameter after Hard/Overweight Landing or Excessive TurbulenceInstallation of the Safety Devices on the Landing Gears Detailed Inspection of Main Wheels Axle and Axle SleevesInspection of the MLG after the Aircraft has gone off the RunwayInspection of the MLG Axles 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 AccessInspection/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 Opening

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REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-22-00-410-001 32-31-00-720-002
R 32-31-22-000-001 32-31-22-400-001 32-31-46-000-001 32-31-46-400-001 32-33-00-720-001 32-41-00-210-002 32-41-12-000-001 32-41-12-000-002 32-41-12-400-001 32-41-12-400-002 54-51-17-000-001
54-51-17-000-002
54-51-17-200-001
54-51-17-200-002 54-51-17-400-001
54-51-17-400-002
R R R R R 55-10-00-210-001 55-16-00-200-001 55-30-00-200-001
55-36-00-210-001
R 71-00-00-000-042 71-00-00-400-042 71-00-00-710-008 71-13-00-010-040 71-13-00-010-040 72-00-00-200-008
78-31-00-710-042
　
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