-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
| | |(2) Examine internally the pylon box | | | X | | |
| | | (all the items you can see) for | | | | | |
| | | distortion, cracks, defective | | | | | |
| | | attachment or other damage: | | | | | |
| | | - lower and upper spars, | | | | | |
| | | - ribs, | | | | | |
| | | - side panels, | | | | | |
| | | - fire protection system (specially| | | | | |
| | | extinguishing bottles | | | | | |
| | | attachments), | | | | | |
| | | - electrical cables | | | | | |
| | | - hydraulic and fuel pipes, | | | | | |
| | | - air-bleed system components. | | | | | |
| | |(3) Remove the engine | | | X | | |
| | | (Ref. TASK 71-00-00-000-042). | | | | | |
| | |(4) Do an inspection of the attach | | | X | | |
| | | fittings at the head of rib 1 | | | | | |
| | | pyramid and under rib 3. | | | | | |
| | | Make sure that there are no signs | | | | | |
| | | of distortion, damage to the | | | | | |
| | | structure (cracks, rupture and | | | | | |
| | | signs of oxydation or burning). | | | | | |
| | |(5) Remove the center fillets at the | | | X | | |
| | | pylon-to-wing junction. | | | | | |
| | |(6) Remove the pylon-to-wing attach | | | X | | |
| | | fittings | | | | | |
| | | (Ref. TASK 54-51-17-000-001) | | | | | |
| | | (Ref. TASK 54-51-17-000-002) | | | | | |
| | |(7) Do a detailed visual inspection of:| | | X | | |
| | | - the forward attach fitting at | | | | | |
| | | at Rib 4 | | | | | |
| | | (Ref. TASK 54-51-17-200-001), | | | | | |
| | | - the spigot between ribs 4 and 5, | | | | | |
| | | - the rear attach fitting at rib 10| | | | | |
| | | (Ref. TASK 54-51-17-200-002). | | | | | |
| | | If there are signs of damage: | | | | | |
| | | (a) Defuel the wing | | | X | | |
| | | (Ref. TASK 28-25-00-650-001). | | | | | |
| | | (b) Get access to the internal | | | | | |
| | | structure adjacent to ribs 7 | | | X | | |
| | | and 8 | | | | | |
| | | (Ref. TASK 28-10-00-910-002). | | | | | |
| | | (c) Examine the rear face of the | | | X | | |
R 1EFF : ALL 1 05-51-11Page 662 1 1 Nov 01/01 1 1 1CES 1
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
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(12)