53-12-00
ALL ú ú 01 Page 5 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
B. The underwing keel beam consists of a pair of high strength aluminum alloy compression chords 18.0 inches apart stabilized by shear webs from the chords to T-chords attached to the lower surface of the center wing section. Additional stabilization is acquired by 0.25 inch thick diagonal tie braces from the compression chords to the T-chords. Horizontal stabilization is attained by a shear web attaching the two compression chords.
C. The keel beam from stations 1241 to 1480 consists of a pair of high strength aluminum alloy compression chords spliced to the keel beam chords from the underwing keel beam and stabilized by a rectangular box structure. The box structure consists of shear webs, stiffeners, and diaphragm bulkheads. A shear web containing stiffeners to prevent buckling is installed between the main deck floor and the top of the keel beam aft of the wing rear spar to station 1480.
7. Window Opening Reinforcements
_____________________________
A. The upper deck window openings in the skin are reinforced by doublers and high strength forged window frames. Extruded T-section stiffeners are attached to the upper and lower edges of the window frames.
B. The window opening reinforcements in sections 42, 44, and 46 on the main deck are basically the same. Doubler and window frame thickness increase with appropriate increases in stress level where adjacent to large cutouts or bulkheads.
8. Door Opening Reinforcements
___________________________
A. The main deck door openings are surrounded by doublers and skins machined from aluminum plate which are bonded or fay sealed and riveted together. Openings surrounding the cargo doors are similarly reinforced. A fay sealed doubler also surrounds the center electrical/electronic equipment access hatch.
B. Additional stringers, sills, straps, and frames have been added to these openings as required by local load conditions.
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53-12-00
ALL ú ú 05 Page 6 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
KEEL BEAM - INSPECTION/CHECK
____________________________
1. General_______
A. This procedure contains one task. The task is the inspection of the keel beam.
B. You get access to the keel beams through the wheel wells for the landing gear and the fuselage access panels.
TASK 53-12-01-206-001
2. The Keel Beam Inspection (Fig. 601)________________________
A. References
(1) 32-00-30/201, Landing Gear Door Locks
B. Access
(1)
Location Zone
135 Wing Landing Gear Well, Left
136 Wing Landing Gear Well, Right
137 Body Landing Gear Well, Left
138 Body Landing Gear Well, Right
129 Keel Beam
139 Keel Beam
149 Keel Beam
(2)
Access Panel
191GG Panel - Access - Keel Beam
191JJ Panel - Access - Keel Beam
191KK Panel - Access - Keel Beam
193J Panel - Access - Keel Beam
193K Panel - Access - Keel Beam
193L Panel - Access - Keel Beam
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