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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
R | | | self-blanking unions and bleed | | | | | |
R | | | screws. | | | | | |
R | | | (b) Clean the piston housing with | | | | | |
| | | a cloth and make sure it is in | | | | | |
| | | the correct condition (no | | | | | |
| | | separation, no blisters). | | | | | |
R | | | (c) Make sure that the heat pack is| | | | | |
| | | serviceable: | | | | | |
| | | - carbon integrity | | | | | |
| | | - free movement of the rotor | | | | | |
R | | | discs | | | | | |
| | | - cracks or signs of oxidation | | | | | |
R | | | on the part of the rotor | | | | | |
R | | | discs you can see. | | | | | |
R | | | NOTE: Be careful with the | | | | | |
| | | discs to prevent damage| | | | | |
| | | to the protective | | | | | |
| | | finish (anti-oxidation | | | | | |
R | | | paint). | | | | | |
| | |If you find damage: | | | | | |
R | | |- Remove the damaged brake unit for | | X | | | |
R | | | overhaul | | | | | |
R | | | (Ref. TASK 32-42-27-000-001). | | | | | |
R | | | (Refer to the manufacturer's | | | | | |
R | | | instructions for the overhaul | | | | | |
R | | | procedure). | | | | | |
| | |(3) Installation of the removed | | | | | |
| | | components | | | | | |
R | | | (a) Install serviceable components:| | | | | |
| | | - for the wheels | | | | | |
| | | (Ref. TASK 32-41-11-400-006) | | | | | |
| | | - for the brakes | | | | | |
R | | | (Ref. TASK 32-42-27-400-001). | | | | | |
| | | | | | | | |
R | B.| |Inspection after the melting of the | | | | | |
R | | |183 deg.C (361.4 deg.F) or 300 deg.C | | | | | |
R | | |(572 deg.F) fuse plug(s) and/or the | | | | | |
R | | |reported cockpit indication of the | | | | | |
R | | |brakes temperature equal to or more | | | | | |
R | | |than 900 deg.C (1652 deg.F) | | | | | |
| | | | | | | | |
| | |(1) Remove the related wheel for | X | | | | |
| | | overhaul | | | | | |
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本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 4(38)
