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时间:2011-04-21 07:57来源:蓝天飞行翻译 作者:航空
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 NOTE: Use this procedure to repair panels that have more than
____ 0.5 inch of damage but no core damage.
 S 348-018
 (1)  
Remove the damaged part of the panel skin.

 S 348-019

 (2)  
Rub the area and 2 inches more on all the sides of the area with abrasive paper until the area is not glossy.


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 S 118-020
 (3)
Clean the area with a cheesecloth that is soaked with naphtha.

 S 118-021

 (4)  
Dry the area with a clean cheesecloth.

 S 348-022

 (5)  
Follow the manufacturer's instructions to mix the BMS 8-201 resin and hardener.

 S 348-023

 (6)  
Apply glass fabric that is soaked with the mixed adhesive and make an overlap of approximately 1/2-inch.


 NOTE: Use 50 percent more glass fabric than the initial skin.
____
 S 348-024
 (7)  
Let the glass fabric and adhesive cure for 24 to 36 hours at 75 to 90°F, or for 3 to 4 hours at 140 to 160°F.

 S 348-025

 (8)  
If this is a decorative panel, do the procedure to repair the decorative surface.


 J. Repair Panels that have Core Damage
 NOTE: Use this procedure to repair panels that have
____
 more than 0.5 inch of damage and damaged core.

 There are two procedure for this repair.
 S 348-113
 (1)  
Remove the damaged skin until you can see at least 0.5-inch of core that does not have damage.

 (2)  
Remove the damaged part of the core.


 S 348-026
 NOTE: Make sure 0.5 inch of core without damage is shown
____
 on all sides of the damaged area.

 S 118-027
 (3)
Clean the area with a cheesecloth that is soaked with naphtha.

 (4)  
Dry the area with a clean cheesecloth.


 S 118-028
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 ALL  ú ú 01 Page 811 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 S 348-029
 (5)  Repair Procedure I
 (a)  
Mix (by weight) 109 parts of EC 3532A/B resin part A to 100 parts of part B.

 (b)  
Bond a piece of foam with the adhesive mixture to the area where the damaged core was removed.


 NOTE: The foam thickness must be the same thickness as the
____ honeycomb core that was removed from the damaged area.
 (c)  
Let the repair cure for 2 hours at 75°F, or for 45 minutes at 160°F.

 (d)  
Repair the skin with the steps given before for panels that do not have core damage.


 S 348-030
 (6)  Repair Procedure II
 (a)  
Use the manufacturer's instructions to mix the Epocast 1618A/B.

 (b)  
Fill the damaged area with the adhesive mixture.

 (c)  
Let the repair cure for 3 hours at 75°F.

 (d)  
Repair the skin with the steps given before for panels that do not have core damage.


 K. Repair Potted Inserts
 S 348-031
 (1)  
Remove the damaged skin and approximately 1/2-inch more on all sides of the damage.

 S 118-032

 (2)
Clean the area with a cheesecloth that is soaked with naphtha.

 (3)  
Dry the area with a clean cheesecloth.

 S 348-034

 (4)  
Cut around the insert from the back side of the panel with a hole saw or an equivalent tool.

 

 S 118-033
 NOTE: Be careful not to cut the front side of the panel.
____
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