C. Put the aircraft back to its initial configuration.
 (1)
 Remove the warning notice(s).

 (2)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 INSPECTION AFTER ENGINE WINDMILLING (AFTER ENGINE IN-FLIGHT SHUT-DOWN)
______________________________________________________________________ INSPECTION/CHECK
________________
 TASK 05-51-34-200-001
 Inspection after Engine Windmilling (After Engine In-Flight Shut-Down)

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
72-00-00-100-007 Engine Dry-out and Relubrication
 3. Job Set-up
__________
 Subtask 05-51-34-860-050

 A. Not Applicable
 4. Procedure
_________ Subtask 05-51-34-210-050 R A. Do the engine dry-out and relubrication procedure after each IFSD or R ferry flight (Ref. TASK 72-00-00-100-007).

 INSPECTION AFTER OVERWEIGHT TAXIING - INSPECTION/CHECK
______________________________________________________
 TASK 05-51-41-200-001
 Inspection after Overweight Taxiing
 1. Reason for the Job
__________________
 Overweight taxiing is defined as taxiing at a weight that is more than the Maximum design Taxi Weight (MTW).
 NOTE : Before flight, you must decrease aircraft weight to that specified in
____ the Aircraft Flight Manual for takeoff. You must do this inspection if you taxi the aircraft at an overweight of more than 2% of the Maximum design Taxi Weight (MTW). You must do this inspection if you taxi an overweight aircraft (regardless of percentage over MTW) and have one of these conditions (or more):
 -high speed ground turn
 -sharp radius turn
 -heavy braking
 -taxi over rough pavement
 -pivot (sharp radius turn with brake on)
 -deflated tire.
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-11-00-200-006 Inspection of the MLG Axles after the Aircraft has
 gone off the Runway 32-11-13-000-003 Removal of the MLG Shock-Absorber Gland-Seals 32-11-13-400-003 Installation of the MLG Shock-Absorber Gland-Seals 32-11-16-000-001 Removal of the MLG Side-Stay Assembly 2505GM, 2506GM 32-11-16-400-001 Installation of the MLG Side-Stay Assembly 2505GM,
 2506GM 32-11-17-000-001 Removal of the MLG Lock Stay 32-11-17-400-001 Installation of the MLG Lock Stay 32-11-21-000-001 Removal of the MLG Lockstay Actuating Cylinder 32-11-21-400-001 Installation of the MLG Lockstay Actuating Cylinder 32-12-00-010-001 Open the Main Gear Doors for Access

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-00-410-001 Close the Main Gear Doors after Access 32-21-13-000-001 Removal of the NLG Shock Absorber Assy 32-21-13-400-001 Installation of the NLG Shock Absorber Assy 32-21-16-000-002 Removal of the NLG Drag Strut Assy (2528GM) 32-21-16-400-002 Installation of the NLG Drag Strut Assy (2528GM) 32-21-17-000-001 Removal of the NLG Lockstay Assy 32-21-17-400-001 Installation of the NLG Lockstay Assy 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-31-22-000-001 Removal of the NLG Actuating Cylinder (2527GM) 32-31-22-400-001 Installation of the NLG Actuating Cylinder (2527GM) 32-41-12-000-001 Removal of the NLG Wheel (2659GM,2660GM) 32-41-12-000-002 Removal of the Axle Sleeve 32-41-12-400-001 Installation of the NLG Wheel (2659GM,2660GM) 32-41-12-400-002 Installation of the Axle Sleeve
 3. Job Set-up
__________
 Subtask 05-51-41-481-050
 A. Safety Precautions
 (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
 Subtask 05-51-41-010-050
 B. Get Access
 (1)
 Open and safety the main gears doors (Ref. TASK 32-12-00-010-001).

 (2)
 Open and safety the nose gear doors (Ref. TASK 32-22-00-010-001).
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM 時間限制/維護(hù)檢查 4(126)