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| 6. Make sure all doors and hatches are | X | | | | | | | X |
| closed when they are not used. | | | | | | | | |
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| 7. Put aluminum foil tape or other | X | | | | | | | |
| reflective material (such as | | | | | | | | |
| aluminized mylar) over the | | | | | | | | |
| outside of the control cabin windows | | | | | | | | |
| and windshields. Do not put | | | | | | | | |
| material that will permit heat | | | | | | | | |
| to build up on the windshield. | | | | | | | | |
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| 8. Examine the structural drain holes | X | | | | | X | | |
| each 90-day cycle (AMM 51-41-00/201).| | | | | | | | |
| Make sure they are open. | | | | | | | | |
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| WING LEADING EDGE, TRAILING EDGE, AND |
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| _____________________________________
| EMPENNAGE |
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| _________
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| 1. Lubricate all flap tracks, carriages | X | | | | | X | | |
| and rollers with MIL-C-16173, | | | | | | | | |
| Grade 2. Do it again each 90-day | | | | | | | | |
| cycle (AMM 12-21-09). | | | | | | | | |
.................................................................................
| 2. Put a layer of MIL-C-16173, Grade 2 | X | | | | | | | |
| on all steel parts that are not | | | | | | | | |
| painted. | | | | | | | | |
.................................................................................
| 3. Lower (or open) all of the flaps | X | | | | | X | | |
| (both leading and trailing edge) and | | | | | | | | |
| the spoilers, and examine them for | | | | | | | | |
| corrosion. When completed, put all | | | | | | | | |
| of the flaps in the up (closed) | | | | | | | | |
| position. Do this each 90-day | | | | | | | | |
| cycle. | | | | | | | | |
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
10-11-02
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ú 03 Page 209
ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
~............................................................................... | | Procedures Repeat Intervals (Days) | | ....................................... | | | | | | | | | As| | Item | Initial | 7 | 14| 30| 60| 90|180|Rqd| ................................................................................. | 4. Examine the structural drain holes | X | | | | | X | | | | and make sure they are open. Do | | | | | | | | | | this again each 90-day cycle. | | | | | | | | | ................................................................................. | | | | | | | | | | .................................................................................
| 5. Before the airplane goes into | X | | | | | | | |
| storage, spray the front and rear | | | | | | | | |
| spar cavities with corrosion | | | | | | | | |
| preventative compound. | | | | | | | | |
................................................................................. | 6. Put a layer of MIL-L-7870 on the fuel| X | | | X | | | | | | pump parts that are external to the | | | | | | | | | | fuel tanks. Examine the fuel pump | | | | | | | | | | parts each 30-day cycle and apply | | | | | | | | | | a new layer (AMM 28-21-00-0). | | | | | | | | | ................................................................................. | 7. Make a visual spot check of the front| | | | | | x | | | | and rear spars for corrosion. (You | | | | | | | | | | will have to remove some access | | | | | | | | | | panels in Zones 512, 524, 525, 612, | | | | | | | | | | 624, and 625 (AMM 06-44-00/201) | | | | | | | | | | which are aft of the slats, to | | | | | | | | | | examine the front spar.) | | | | | | | | | ................................................................................. | EQUIPMENT/FURNISHINGS | | | | | | | | | 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 AMM 飛機維護手冊 PARKING, MOORING, STORAGE & RETURN TO S(12)
