................................................................................. | 2. Remove the water filters and | X | | | | | | | | | do not install them during the | | | | | | | | | | storage time, (AMM 38-10-00-2). | | | | | | | | | ................................................................................. | 3. Remove all of the coffeemakers and | X | | | | | | | | | water boilers from airplane. Store | | | | | | | | | | them at temperatures that do not | | | | | | | | | | freeze. | | | | | | | | | ................................................................................. | FIRE EXTINGUISHING SYSTEMS | | | | | | | | |
__________________________ ................................................................................. | Short and Long Term | | | | | | | | |
___________________ ................................................................................. | The procedure that follows is for | | | | | | | | | | protection of the airplane for a | | | | | | | | | | time up to 2 years. | | | | | | | | | | Do the procedure that follows at | | | | | | | | | | the start of the storage cycle, | | | | | | | | | | and at the specified intervals | | | | | | | | | | (AMM 26-21-00/0). | | | | | | | | |
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10-11-02
ALL ú ú 02 Page 236 ú Jun 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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| ................................................................................. | 1. Make sure that the discharge | X | | | | | | | | | squibs stay installed on all fire | | | | | | | | | | extinguisher bottles. Also make sure| | | | | | | | | | the squibs are connected to their | | | | | | | | | | correct electrical supply. | | | | | | | | | | | | | | | | | | | | NOTE:____The fire extinguisher bottles | | | | | | | | | | must stay in the airplane | | | | | | | | | | in a charged, and in a | | | | | | | | | | serviceable condition. | | | | | | | | | ................................................................................. | POWER PLANT AND APU | | | | | | | | |
___________________ ................................................................................. | 1. Refer to AMM 71-00-03 for the | | | | | | | | | | maintenance procedures that are | | | | | | | | | | applicable to engine storage. | | | | | | | | | ................................................................................. | 2. Refer to AMM 49-11-00 for the | | | | | | | | | | procedures that are applicable to APU| | | | | | | | | | storage. | | | | | | | | | 2.........................................….........…...…...…...…...…...…...…...1
TASK 10-11-02-632-002
3. Put the Airplane Back to a Serviceable Condition After Storage
______________________________________________________________
A. Consumable Materials
(1)
D00012 Grease - Aeroshell No. 5
(2)
G00009 Corrosion Preventive Compound - BMS 3-23, Type II
(3)
D00013 Grease - MIL-G-23827
(4)
E00118 Remover - Ardrox 302N (water base)
B. References
(1)
AMM 07-11-01/201, Jacking Airplane
(2)
AMM 07-11-03/201, Jacking Airplane Axle
(3)
AMM 09-11-00/201, Towing
(4)
AMM 12-11-01/301, Pressure Fueling
(5)
AMM 12-12-01/301, Hydraulic System
(6)
AMM 12-14-01/301, Potable Water System
(7)
AMM 12-15-01/301, Main Gear Shock Strut
(8)
AMM 12-15-02/301, Nose Gear Shock Strut
(9)
AMM 12-15-03/301, Landing Gear Tires
(10)
AMM 12-15-04/301, Parking Brake Accumulator
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