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时间:2011-04-21 07:59来源:蓝天飞行翻译 作者:航空
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 S 216-004
 (3)  Do the permanent repair procedure if the linings are not damaged more than these limits (AMM 25-50-09/801): (a) Slits that are 12-inches long, (b) "L" shaped tears that are 9-inches long on the two sides, (c) Holes that have a 1.5-inch diameter, (d) One damaged fastener, (e) Damaged zippers, (f) In the area of seams and fasteners, loose or damaged tape.
 S 906-005
 (4)  Replace the applicable fiberglass linings that have more than the above damage limits (AMM 25-50-01/401, AMM 25-50-02/401, or AMM 25-50-03/401).
 S 216-020
 (5)  Repair the rigid nomex honeycomb lining if it is necessary (AMM 25-00-00/801).

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 25-50-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 S 356-022
 (6)  If both rigid nomex honeycomb lining skins have been damaged, do this task: (AMM 25-50-09/801).
 TASK 25-50-00-206-028
 3.  Compartment Lining - Inspection/Check_____________________________________
 NOTE: This is a scheduled Maintenance Task.
____
 A. General
_______
 (1)  
This procedure is for the inspection and check of the cargo compartment lining. It gives instructions for the inspection of the fiberglass liners on the vertical and sloping sidewalls, bulkhead, and ceiling in the cargo compartment.

 (2)  
It is important that all of the fasteners, seams, and punctures are sealed correctly to keep the amount of oxygen in the compartment to a minimum.


 B. References
 (1)  
AMM 25-00-00/801, Equipment/Furnishings, Approved Repairs

 (2)  
AMM 25-50-01/401, Cargo Compartment Ceiling Lining

 (3)  
AMM 25-50-02/401, Cargo Compartment Sidewall Lining

 (4)  
AMM 25-50-03/401, Bulkhead Lining

 (5)  
AMM 25-50-09/801, Cargo Compartment Lining (Fiberglass)


 C. Access
 (1)  Location Zones
 121/122 Forward Cargo Compartment
 153/154 Aft Cargo Compartment
 161/162 Bulk Cargo Compartment

 D. Procedure
 S 216-029
 (1)  
Do a visual inspection of the forward, aft and bulk cargo compartment lining.

 S 346-030

 (2)  
Do the permanent repair procedure if the linings are not damaged more than these limits (AMM 25-50-09/801):

 (a)  
Slits that are 12-inches long,

 (b)  
"L" shaped tears that are 9-inches long on the two sides,

 (c)  
Holes that have a 1.5-inch diameter,

 (d)  
One damaged fastener,

 (e)  
Damaged zippers,

 (f)  
In the area of seams and fasteners, loose or damaged tape.

 


 S 966-034
 (3)  Replace the applicable fiberglass linings that have more than the above damage limits (AMM 25-50-01/401, AMM 25-50-02/401, or AMM 25-50-03/401).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 S 346-038
 (4)  Repair the rigid nomex honeycomb lining if it is necessary (AMM 25-00-00/801).
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 25-50-00
 ALL  ú ú 01 Page 604 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 CARGO COMPARTMENT - CLEANING/PAINTING
_____________________________________
 1.  General_______
 A.  This section contains one task. The task gives instructions to clean the cargo compartments.
 TASK 25-50-00-107-022
 2.  Clean the Cargo Compartment____________________________
 
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