(3)
AMM 20-30-82/201, Airplane Structure Cleaning Solvents (Series 82)
(4)
AMM 20-30-88/201, Airplane Structure Cleaning Solvents (Series 88)
(5)
AMM 20-41-01/201, Static Grounding
(6)
AMM 28-11-00/201, Fuel Tank Entry
(7)
AMM 28-11-00/601, Fuel Tank
(8)
AMM 28-11-00/801, Fuel Tank
(9)
AMM 28-11-01/401, Center Tank Access Door
(10)
AMM 28-11-02/401, Main and Reserve Tank Access Door
(11)
AMM 28-11-03/401, Surge Tank Access Door
(12)
AMM 28-26-00/201, Fuel Tank Defueling
(13)
SOPM 20-30-81, Cleaning Solvents (Series 81)
(14)
SOPM 20-30-82, Cleaning Solvents (Series 82)
(15)
SOPM 20-30-88, Cleaning Solvents (Series 88)
C.
Equipment
(1)
Blower - Air, Explosion Proof, 90-100 cubic feet per minute, includes sufficient hose to reach all areas of fuel tanks (commercially available)
(2)
Brush - Paint (commercially available)
(3)
Fan - Exhaust, Centrifugal, Explosion Proof, 125-150 cubic feet per minute, includes 75 feet of 3-inch suction hose and sufficient delivery hose to carry air out of work area (commercially available)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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747-400
MAINTENANCE MANUAL
180
TEMPERATURE - `F (`C)
(82.222)
160
(71.111)
140
(60)
120
(48.888)
100
(37.778) 1 2 3
TIME (HOURS)
Bostik-Finch (BMS 10-20 Type II) Compound
Cure Time Versus Temperature
Figure 702
L48090
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400
MAINTENANCE MANUAL
120
(48.888)
110
(43.333)
100
(37.777)
90
(32.222)
80
(26.666)
70
(21.111)
60
(15.555)
50
(10)
20% RH FUEL RESISTANT CURE
45% RH 60% RH
90% RH
TEMPERATURE - `F (`C)
0 5 101520253035
TIME (HOURS)
DeSoto (MIL-C-27725) Compound Fuel Resistant Cure Time
Versus Temperature and Relative Humidity (RH)
Figure 703
L48101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
140
(60)
130
(54.444)
120 (48,888)
110
(43.333)
100
(37.777)
90
(32.222)
80
(26.666)
TEMPERATURE - `F (`C)
TIME (HOURS)
Desoto (MIL-C-27725) Compound Full Cure Time
Versus Temperature and Relative Humidity (RH)
Figure 704
L48241
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
% RELATIVE TEMPERATUR E - `F (`C)
HUMIDITY (RH) 20 65 (18.333) 392 70 (21.111) 228
45 376 212
65 344 184
90 240 124
(23.888)
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