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R Inspection Form Figure 001
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INSPECTIONS AFTER HARD/OVERWEIGHT LANDING - INSPECTION/CHECK
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R **ON A/C 001-003, 051-054,
TASK 05-51-11-200-004
Inspection After Hard/Overweight Landing
1. Reason for the Job
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A hard landing is defined as a landing with a vertical acceleration of more
than 2.6 g at the center of gravity or:
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a vertical speed (V/S) of more than 540 ft/min.
An overweight landing is defined as a landing at more than the maximum
landing weight with a vertical acceleration of more than 1.7 g at the center
of gravity or:
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a vertical speed (V/S) of more than 360 ft/min.
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 notice
No specific access platform 2 m (6 ft. 7 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 12-14-32-614-004 Check Shock Absorber Charge Pressure 23-71-00-710-001 Operational Test of the CVR and the CVR Channel
Recording 24-38-00-210-001 Visual Inspection of the Batteries (2PB1, 2PB2) 24-38-00-710-001 Operational Test of the Battery Charge Limiter (BCL),
(with the CFDS)
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REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002
27-50-00-866-008 27-50-00-866-009 27-54-00-200-001
27-54-00-710-001 27-60-00-866-002 27-64-00-710-001 27-80-00-866-004 27-80-00-866-005 28-10-00-910-002 28-25-00-650-001 29-00-00-864-001
29-22-00-720-001
31-33-00-710-005 31-33-00-710-007 32-00-00-481-001
32-11-00-200-001 32-11-13-000-001 32-12-00-010-001 32-12-00-410-001 32-12-00-710-002
32-21-13-000-001 32-22-00-010-001 32-22-00-410-001 32-31-00-720-002
32-41-00-210-002 32-69-00-740-001
R R R R 49-16-00-200-002 49-16-00-210-001
De-energize the Aircraft Electrical Circuits Supplied from the External PowerExtension of the Flaps on the GroundRetraction of the Flaps on the GroundDetailed 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 MaintenanceOperational Test of the Spoiler Hydraulic ActuationExtending the Slats on the GroundRetracting the Slats on the GroundAccess to the Fuel Tanks and the Work AreasPressure DefuelPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionOperational Check of RAT Manual Deployment, Functional Check of RAT using Ground Test Unit and Check of Filter IndicatorOperational Test of the QAROperational Test of the DFDRInstallation of the Safety Devices on the Landing GearsInspection/Check of the Main GearRemoval of the MLG Shock AbsorberOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessOperational Test of the Main Landing Gear (MLG) Doors Ground-Opening-MechanismRemoval of the NLG Shock Absorber AssyNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors ClosingFunctional Test of the Normal Extension and Retraction of the Landing GearInspection/Check of the Wheels and TiresBITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operative Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal (131-9(A)) Detailed Inspection of the Air Intake, Diffuser Elbow, Seals and Felt Metal (GTCP 36-300)
R 1EFF : 001-003, 051-054, 1 05-51-11Page 602 1 1 May 01/05 1 1 1CES 1
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REFERENCE DESIGNATION -------------------------------------------------------------------------------
54-51-17-000-001 Removal of the Pylon-to-Wing Forward Attach Fitting
at RIB4
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本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 3(100)
