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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
Nose Gear Doors - Ground Doors ClosingFunctional Test of the Normal Extension and Retraction of the 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 ExtensionInspection/Check of the Wheels and TiresRemoval of the NLG Wheel (2659GM,2660GM)Removal of the Axle SleeveInstallation of the NLG Wheel (2659GM,2660GM)Installation of the Axle SleeveRemoval of the Pylon-to-Wing Forward Attach Fitting at RIB4Removal of the Pylon-to-Wing Aft Attach Fitting at RIB10Inspection of the Pylon-to-Wing Forward Attach-FittingInspection of the Pylon-to-Wing Aft Attach-FittingInstallation of Pylon-to-Wing Forward Attach Fitting at RIB4Installation of the Pylon-to-Wing Aft Attach Fitting at RIB10 Detailed Inspection of Horizontal Stabilizer Internal Structure of Torque Box Inboard of Fuselage Fairings Detailed Inspection of Horizontal Stabilizer Rear Support Fittings, Upper and Lower Attach Fittings and Surrounding External Structure, LH/RHDetailed Visual Inspection of Vertical Stabilizer Center Box Internal Structure as far as Visible, Front Spar FWD Face Upper Closing Rib Upper SurfaceDetailed Visual Inspection of the Vertical Stabilizer Attach Fittings Including the Load Introduction Area at the Skin PanelsRemoval of the Power PlantInstallation of the Power PlantPower Assurance CheckOpening of the Fan Cowl Doors Opening of the Fan Cowl DoorsInspection/Check After the Engine has Exceeded the Operational LimitsOperational Test of the Thrust Reverser System -------------------------------------------------------------------------------
REFERENCE DESIGNATION ------------------------------------------------------------------------------- 78-36-00-010-040 Opening of the Thrust Reverser Doors R 78-36-00-010-040 Opening of the Thrust Reverser Doors 79-00-00-281-002 Check of the Electrical Master Chip Detector for Particles 05-51-11-991-015 Fig. 611 05-51-11-991-016 Fig. 612 3. Job Set-up __________ Subtask 05-51-11-210-090 A. Hard/Overweight Landing Inspection Requirements (Ref. Fig. 611/TASK 05-51-11-991-015, 612/TASK 05-51-11-991-016) (1) Definitions There are several categories of hard/overweight landing:
(a) Hard landing A hard landing is a landing with an aircraft weight less than the Maximum landing Weight (MLW) and:
- a vertical acceleration (VertG) equal to or more than 2.6 g and less than 2.86 g at aircraft Center of Gravity (CG) or,
- a vertical speed (Vs) equal to or more than 10 ft/s and less than 14 ft/s.
(b) Severe hard landing A severe hard landing is a landing with an aircraft weight less than the Maximum landing Weight (MLW) and:
- a vertical acceleration (VertG) equal to or more than 2.86 g at aircraft Center of Gravity (CG) or,
- a vertical speed (Vs) equal to or more than 14 ft/s.
(c) Overweight landing An overweight landing is a landing with an aircraft weight more than the Maximum landing Weight (MLW) and:
- a vertical acceleration (VertG) equal to or more than 1.7 g and less than 2.6 g at aircraft Center of Gravity (CG) or,
- a vertical speed (Vs) equal to or more than 6 ft/s and less than 13 ft/s.
(d) Severe overweight landing A severe overweight landing is a landing with an aircraft weight more than the Maximum landing Weight (MLW) and:
- a vertical acceleration (VertG) equal to or more than 2.6 g at aircraft Center of Gravity (CG) or,
- a vertical speed (Vs) equal to or more than 13 ft/s.
(e) High pitch-rate landing A high pitch-rate landing is a landing during which the pitch rate is more than 10 Deg/sec.
(2) Hard/overweight landing confirmation
(a) It is the responsibility of the flight crew to make a report if they think there was a hard/overweight landing. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 2
