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时间:2011-04-15 08:32来源:蓝天飞行翻译 作者:航空
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 53-11-00
 ALL  ú ú 04 Page 1 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

STA 520 
CREW COMPARTMENT 
OVERHEAD HATCH 
SEE  C 
STA 
PRESSURE  140 
BULKHEAD 
SEE  B 
RADOME 
SEE  A 
STATION 240 
CANTED BULKHEAD  FLOOR-TO-SKIN 
SHEAR TIES 
SEE  D 
FWD 
STA 140 
NOSE LANDING 
GEAR WHEEL WELL 
STRINGER 
ATTACHMENT 
(EXAMPLE)  STATION 340 
BULKHEAD 
AFT RING  STATION 400  STA 520 
BULKHEAD 
ELECTRICAL/ 
ELECTRONICS 
ACCESS DOOR 
FORWARD 
RING  A 
FLAT WEB 
FWD 
PRESSURE BULKHEAD 

Nose Section, Section 41 
Figure 1 (Sheet 1) 

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 ALL  ú ú 01 Page 2 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL 
UPPER DECK 307.5 WL  520 STA 
MAIN DECK 199.8 WL  REINFORCEMENT DOOR 
(EXAMPLE) STRINGERS 
FRAME  STRINGER  BEAM FLOOR C  (2 LOCATIONS) MAIN ENTRY DOOR FWD 
SHEAR TIES FLOOR-TO-SKIN 

Figure 1 (Sheet 2) Nose Section, Section 41 

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 ALL  ú ú 01 Page 3 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE A
FRAME 
SKIN 
B  FAIL-SAFE STRAP 
STRINGER 
CUTOUT 

FORMED CHORD 
REINFORCING 
ANGLE 
B-B 

Frame and Stringer - Section 41 (Example)
Figure 2 

STRINGER
STRINGER CLIP
LOCAL CHORD REINFORCING
C
L
STA

BASIC
FRAME
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 ALL  ú ú 01 Page 4 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 5.  Floor-to-Skin Shear Ties (Fig. 1)
________________________
 A.  The floor-to-skin shear ties extend along both sides of the fuselage, level with the floor at each deck. Two types of shear ties are used. A punched and formed sheet metal type is most common but a truss-type is used where decompression venting provisions are required. The shear ties are attached to fuselage skin stringers, floor beams, and body frame.
 6.  Flight Compartment Window Opening Reinforcements (Fig. 3)
________________________________________________
 A.  The flight compartment window and windshield posts form a truss tied to the body frames. The forward and aft of the aft window is part of a reinforced portion of body station 320 and 340 frames. The portion of the body frame at station 320 that separates the forward and aft side windows is known as No. 3 post. No. 2 post separates the windshield from the forward side window and No. 1 post separates the left and right windshields (detail A, sheet 2).
 B.  All posts are of two-piece fail-safe construction so that, should one member fail, the remaining member can safely carry the load. Upper and lower sill chords of the side windows are extrusions. All sill chords and posts are aluminum alloy extrusions except the windshield lower sills and the No. 1 post. The windshield lower sills are machined aluminum forgings and the No. 1 post is a machined extrusion of aluminum alloy. The posts are continuous beams, splicing to and continuing through the sills to effect maximum rigidity with least visual blocking. The upper sill is a torque box extending around the entire window pattern from station 340 bulkhead, left to right side. The main lower sill is a continuous beam extending forward and below the windshield aft to station
 
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