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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
______________________
 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
 -------------------------------------------------------------------------------
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

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REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-54-00-200-001
27-54-00-710-001 27-60-00-866-002 27-80-00-866-004 28-10-00-910-002 28-25-00-650-001 29-00-00-864-001

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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