................................................................................. | A. Do not apply the corrosion | | | | | | | | | | preventative compound to areas | | | | | | | | | | which will be subsequently painted| | | | | | | | | | or sealed. | | | | | | | | | ................................................................................. | B. Shield or protect the control | | | | | | | | | | cables, pulleys, wire bundles, | | | | | | | | | | etc., to prevent the direct | | | | | | | | | | application of corrosion | | | | | | | | | | preventative compound to them. | | | | | | | | | ................................................................................. | C. Apply masking tape to the | | | | | | | | | | electrical connectors to prevent | | | | | | | | | | the application of the compound to| | | | | | | | | | electrical contacts. | | | | | | | | | ................................................................................. | D. Apply the compound before the | | | | | | | | | | installation of equipment (if | | | | | | | | | | applicable). | | | | | | | | | ................................................................................. | E. Do not apply corrosion | | | | | | | | | | preventative compound to teflon | | | | | | | | | | bearings, surfaces or joints, | | | | | | | | | | which are lubricated in other | | | | | | | | | | procedures. | | | | | | | | | ................................................................................. | F. The finished application of the | | | | | | | | | | corrosion preventive compound must| | | | | | | | | | be a continuous film, with no | | | | | | | | | | puddles. | | | | | | | | | ................................................................................. | G. Inspect the application each | | | | X | | | | | | 30-day cycle. | | | | | | | | |
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10-11-02
ALL ú ú 02 Page 233 ú Mar 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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| ................................................................................. | OXYGEN SYSTEM | | | | | | | | |
_____________ ................................................................................. | Short Term | | | | | | | | |
__________ .................................................................................
| When an airplane is put in storage for | | | | | | | | |
| time that is not more than 60 days, no | | | | | | | | |
| special precautions are necessary. | | | | | | | | |
| But, you must make sure that the high | | | | | | | | |
| pressure valves on the oxygen supply | | | | | | | | |
| cylinders are closed. These oxygen | | | | | | | | |
| cylinders are for the crew and the | | | | | | | | |
| passenger systems (AMM 12-15-08, AMM | | | | | | | | |
35-11-00).
................................................................................. | Long Term | | | | | | | | |
_________ ................................................................................. | The procedures that follow are for | | | | | | | | | | protection of the airplane for a | | | | | | | | | | time up to 2 years. | | | | | | | | | | Do the procedures that follow at | | | | | | | | | | the start of the storage cycle | | | | | | | | | | and at the specified intervals. | | | | | | | | |
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