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时间:2011-04-02 05:47来源:蓝天飞行翻译 作者:航空
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A
737-300/400/500MAINTENANCE MANUAL
 (c)  To increase the relative humidity, let moist, warm air, at a temperature of less than 120°F (49°C), flow on the repair area.
 NOTE: In hot, dry weather, put a pan of water in the fuel
____ tank adjacent to the repair area to increase the humidity.
 (d)  
Make sure the water added to the air contains less than 100 parts per million of total solids and less than 10 parts per million of chlorides.

 (e)  
If warm, moist air, at a temperature of less than 120°F (48.9°C), flows on the sealant, it decreases the cure time.


 S 398-219
 (6)  If you increase the temperature of the tank structure, but not more than 120°F (48.9°C), it decreases the cure time.
 (a)  If there is fuel in the tank adjacent to the repair area, you can defuel that tank to increase the temperature of the repair area.
 S 398-220
 CAUTION: MAKE SURE THE TEMPERATURE OF THE TANK SURFACE TO WHICH YOU
_______ APPLY THE SEALANT IS AT A TEMPERATURE MORE THAN THE AMBIENT TEMPERATURE. CONDENSATION CAN OCCUR AND THE SEALANT WILL NOT DRY CORRECTLY.
 (7)  For BMS 5-26 Type II sealant, if you keep the humidity constant, the times, shown in Fig. 801, change by these quantities:
 (a)  
The tack-free times are approximately one-half as long for each 20°F (11.1°C) increase in temperature.

 (b)  
The tack-free times are approximately double for each 20°F (11.1°C) decrease in temperature.


 TASK 28-11-00-398-240
 5. Repair of Sealant Leaks in the Fuel Tank Structure
__________________________________________________
 A. General
 (1)  This task has instructions to do a permanent repair of a damaged seal on the internal surface of an integral fuel tank. You must apply a new seal if you do not find a seal. These primary steps are necessary:
 (a)  Prepare to go into the tank.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEALANT  CLASS  HOURS TIME (MINIMUM) APPLICATION 1  HOURS TIME TACK-FREE (MINIMUM) 1  HOURS OUT LIFE (MINIMUM) SQUEEZE-1  HOURS TIME CURING (MINIMUM) 1 
PROSEAL 860 3  B-1/6  1/6  1.5 2  -- 4 
PR-1828 PR-1826 64 4  B-1/4  1/4  1  -- 2
B-1/2  1/2  2.5  -- 3 
BMS 5-45, TYPE II  B-1/2 7  1/2  8  -- 24 
B-2  2  24  6  48 
BMS 5-26, TYPE II  A-2 (Grade 1)  2  36  -- 72 
A-2 (Grade 2)  2  24  -- 48 
B-1/2 7  1/2  6  -- 24 
B-2  2  24  6  48 
C-24 5  8  -- 24  168 
C-48 5  12  -- 48  336 
C-168 5  48  -- 168  1,344 


AT 77`F (25`C) AND 50% RELATIVE HUMIDITY AMBIENT CONDITIONS. OTHER TEMPERATURE AND RELATIVE HUMIDITY CONDITIONS WILL CHANGE THE TIMES.
DO NOT LET FUEL TOUCH THE SEALANT UNTIL IT IS NOT TACKY FOR A MINIMUM OF 2 HOURS.
WHEN YOU USE PROSEAL 860, DO NOT USE A PRECOAT. PROSEAL 860 IS RECOMMENDED FOR SMALL REPAIRS ONLY,
DUE TO ITS SHORT APPLICATION TIME. AVAILABLE FROM COURTAULDS AEROSPACE, GLENDALE, CALIFORNIA.

USED TO REPAIR FILLET SEALS OF BMS 5-26 OR BMS 5-45. AVAILABLE FROM COURTAULDS AEROSPACE,
GLENDALE, CALIFORNIA.
USED WITH FAYING SURFACE SEALS THAT HAVE A LONG SQUEEZE-OUT LIFE

THIS SEALANT IS WHITE. THUS, IT IS EASY TO SEE THE REPAIRED AREA.
MIX BMS 5-26 OR BMS 5-45, TYPE II, CLASS B-2 SEALANT WITH A 20:100 ACCELARATOR/BASE RATIO BY
WEIGHT OR GET THIS SEALANT PRE-MIXED.

Sealant Usable Time
Figure 801

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 (2)

(3)

(4)


A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Remove the corrosion protection finish (topcoat) if it is necessary to get access to sealant that you must repair
 
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