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Boeing 737-600 - Page 1748

Boeing 737-600
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A
B
2
A
A-A
1
1
1
3
B
1
2
3
FRAME, STRINGER AND SKIN STRUCTURE
(INSULATION BLANKET NOT SHOWN)
STRAP AND FRAME
FUSELAGE SECTION
FRAME AND SHEAR TIE
APPLY EPOXY PRIMER
ON FLANGE SURFACE
(TYPICAL)
APPLY EPOXY PRIMER
ON FLANGE SURFACE
(TYPICAL)
REINFORCING
ANGLE
SHEAR TIE
APPLY SEALANT BMS 5-95
ON STRINGER FLANGES
AND EDGES OF FRAMES
SKIN
FRAME
SKIN
STRAP
STRINGER
FRAME
APPLY BMS 3-23 TO ALL EXPOSED STRUCTURE
WHEN INSULATION BLANKETS ARE REINSTALLED, ENSURE THAT
OUTBOARD SURFACE OF UPPER BLANKET OVERLAPS LOWER BLANKET.
IN AREAS ABOVE THE WINDOW BELT BETWEEN STA 259.5 AND STA 1015
WHERE BLANKETS CONTACT STRINGER FLANGES AND EDGES OF FRAMES.
BETWEEN BODY STATIONS 540 AND 1016 WHERE STRINGER SOUND
DAMPING CAPS ARE USED, SEALANT IS NOT REQUIRED.
DISPLACING CORROSION
PREVENTIVE COMPOUND IN
ALL STRUCTURE IN BODY
UPPER LOBE ABOVE
WL 208.1 BETWEEN STA
260, AND STA 1040,
INCLUDING THE ENTIRE
FORWARD AND AFT FACE
OF STA 1016 BULKHEAD.
CARGO
DECK
STRINGER
S-10
WL
208.1
FRAME, STRINGER AND
SKIN STRUCTURE
J72219 S0000174884_V2
Crown Frames, Stringers and Skin
Figure 201/53-11-37-990-811 (Sheet 2 of 2)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-11-37
Page 205
D633A101-ILF Oct 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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