-------------------------------------------------------------------------------
5. Close-up
________
1EFF : ALL 1 05-51-14Page 614 1 1 Nov 01/02R 1 1 1CES 1
R INSPECTION AFTER A TIRE BURST OR TREAD THROW OR WHEEL FAILURE
_____________________________________________________________ R INSPECTION/CHECK
________________
TASK 05-51-15-200-001
R Inspection after a Tire Burst or Tread Throw or Wheel Failure
WARNING : LET THE BRAKES AND THE WHEELS BECOME COOL BEFORE YOU GO NEAR THE
_______ LANDING GEAR. DO NOT APPLY A LIQUID OR GAS FIRE EXTINGUISHER DIRECTLY ON A HOT WHEEL OR BRAKE UNIT. THIS COULD CAUSE AN EXPLOSION.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific access platform 3 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-51-16-200-001 Inspection After Brake Overheat 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 27-14-00-710-001 Operational Test of the Aileron and Hydraulic
Actuation 27-50-00-866-008 Extension of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 27-80-00-866-004 Extending the Slats on the Ground 27-84-00-710-001 Operational Test of the Slat System 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-25-00-650-001 Pressure Defuel 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears 32-11-00-200-001 Inspection/Check of the Main Gear 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-30-00-867-001 Retraction of the Landing Gear for Maintenance 71-13-11-200-001 Visual Inspection of the Fan Cowl Doors 72-00-00-200-006 Inspection/Check of Foreign Objet Damage (FOD) (Bird
Strike Included)
78-31-00-710-042 Operational Test of the Thrust Reverser System
3. Job Set-up
__________
Subtask 05-51-15-481-050
A. Safety Precautions
R (1) Make sure that the safety devices are installed on the landing gears R (Ref. TASK 32-00-00-481-001).
Subtask 05-51-15-010-050
B. Get Access
(1)
Open the main gear doors and install the safety devices (Ref. TASK 32-12-00-010-001).
(2)
Open the nose gear doors and install the safety devices (Ref. TASK 32-22-00-010-001).
Subtask 05-51-15-866-050
C. Extension of the Flight Control Surfaces
(1)
Fully extend the flaps and the slats (Ref. TASK 27-50-00-866-008), (Ref. TASK 27-80-00-866-004).
(2)
Extend the spoilers (Ref. TASK 27-60-00-866-002).
Subtask 05-51-15-860-050
D. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
(2)
Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護(hù)手冊 AMM 時間限制/維護(hù)檢查 2(39)
