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时间:2011-04-01 19:06来源:蓝天飞行翻译 作者:航空
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 S 432-023
 S 412-024
 S 412-025
 TASK 25-11-21-302-026
 6.  Flight Compartment Insulation Approved Repairs (Fig. 202)______________________________________________
 A. General
 (1)  Repair with patches or damaged blankets to keep the insulation dry.
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 25-11-21
 ALL  ú ú 02 Page 205 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  Replace immediately all the damage blankets that soaked with the oil.
 NOTE: If the damage area is more than 25 percent of the total
____ blanket area, you must replace the blanket.
 B. Consumable Materials
 (1)  
B00148 Solvent - Methyl Ethyl Ketone TT-M-261

 (2)  
A00153 Adhesive - BMS 5-30

 (3)  
G00087 Insulation - Covering, BMS 8-142, Type 1


 C. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

 D. Procedure
 S 112-027
 (1)  Clean the damaged area with MEK, isopropyl alcohol, or ethyl alcohol.
 NOTE: Permit the cleaned fabric to dry until you smell no solvent.
____
 S 352-028
 (2)  
Cut a patch of the fabric to put covers on the area.

 S 352-029

 (3)  
Apply a large quantity of the adhesive to the area and to the patch.

 (4)
When the adhesive is tacky, push the patch tightly on the area.


 S 352-030
 TASK 25-11-21-002-031
 7. Flight Compartment Drip Pan Removal (Fig. 203)
___________________________________
 A. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

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 25-11-21
 ALL  ú ú 01 Page 206 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 B.  Procedure S 012-032
 (1)  
Remove the overhead instrument panels. S 012-033

 (2)  
Remove the adjacent lining panels (par. 1). S 012-034

 (3)  
Remove the structure which holds the panels.


TRIM FABRIC
(APPLIED LAYER
TUBE
SPONGE TYPE PLASTIC SHEET

Flight Compartment Drip Pan Installation
Figure 203

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 25-11-21
 ALL  ú ú 01 Page 207 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 032-035
 (4)  
Remove the wire supports and the clips.

 S 032-036

 (5)  
Disconnect the wire where it is necessary.

 S 032-037

 (6)  
Loosen the wire bundles where it is necessary.

 S 012-038

 (7)  
Disconnect the drain line.

 S 022-039

 (8)  
Remove the remaining fasteners.

 S 022-040

 (9)
Push the wire bundles out of the holes to remove the drip pan.

 S 212-041

 (10)
 Examine for loose insulation and for damaged insulation pads.


 TASK 25-11-21-402-042
 8. Flight Compartment Drip Pan Installation (Fig. 203)
________________________________________
 A. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

 B. Procedure
 S 422-043
 (1)  
Put the drip pan into its position and install it with the bolts.

 S 412-044

 (2)  
Connect the cooling and drain lines.

 S 432-045

 (3)  
Put the wire bundles into their correct positions and attach the bundles where it is necessary.
 
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