-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
| | | (Ref. TASK 28-25-00-650-001). | | | | | | | | | (2) Get access to the internal | | | | | | | | | structure adjacent to rib 7 and | | | | | | | | | rib 8 | | | | | | | | | (Ref. TASK 28-10-00-910-002). | | | | | | | | | Do a full inspection for: | | | | | | | | | - cracks, damage, damage paint and | | | | | | | | | sealant and the correct condition| | | | | | | | | of all fasteners and safety | | | | | | | | | devices | | | | | | | | | in the following areas: | | | | | | | | | - the rear face of the front spar, | | | | | | | | | inboard of rib 7 and outboard of | | | | | | | | | rib 8, | | | | | | | | | - the front face of the rear spar | | | | | | | | | inboard of rib 7 and outboard of | | | | | | | | | rib 8, | | | | | | | | | - the pylon rear attachment, | | | | | | | | | - rib 7 and rib 8, | | | | | | | | | - the stringers and the brackets. | | | | | | | | | | | | | | | | | | If you find damage: | | | X | | | | | | - do an alignment check | | | | | | | | | (Ref. TASK 05-56-00-200-001). | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 05-51-26-420-050
A. Installation of the Power Plant
(1) Install the power plant (Ref. TASK 71-00-00-400-042).
Subtask 05-51-26-942-050
B. Put the aircraft back to the serviceable condition.
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Remove the warning notice(s).
1EFF : ALL 1 05-51-26Page 606 1 1 Nov 01/00R 1 1 1CES 1
(3) Remove the access platform(s).
1EFF : ALL 1 05-51-26Page 607 1 1 Nov 01/00R 1 1 1CES 1
R INSPECTION AFTER IMPACT ON ENGINE COWLS - INSPECTION/CHECK
__________________________________________________________
TASK 05-51-27-200-001
1. Reason for the Job
R Inspection after Impact on Engine Cowls __________________ Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific adjustable access platform
No specific warning notices
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
71-00-00-000-042 Removal of the Power Plant
71-00-00-400-042 Installation of the Power Plant
71-13-00-010-040 Opening of the Fan Cowl Doors
71-13-00-410-040 Closing of the Fan Cowl Doors
78-36-00-010-040 Opening of the Thrust Reverser Doors
78-36-00-410-040 Closing of the Thrust Reverser Doors
3. Job Set-up
__________
Subtask 05-51-27-941-050
A. Safety Precautions
(1) Put the warning notices in the cockpit to tell persons not to operate the systems related to the engines.
中国航空网 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(117)
