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时间:2011-03-31 16:18来源:蓝天飞行翻译 作者:航空
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5.  
TO CONVERT FIN STATION TO RUDDER STATION AT REAR SPAR. RUDDER STATION = (FIN STA - 187.1).

6.  
TO CONVERT FIN STATION TO LEADING EDGE STATION AT AUXILIARY SPAR (6%). LEADING EDGE STATION = (46 + FIN STA).


156.9 FIN
109.8
STA
FIN FIN
LE STA
563.2
86.3
STA STA
582.7 570 595 47.1
9.4
FIN FIN FIN FIN FIN FIN STA STA STA STA STA STA
40 345 370 395 420 470 520
FIN FIN FIN FIN FIN
STA STA STA STA STA

RUD 220 245 270 295 320
STA
RUD TRAILING UPPER 417.5
STARUDDERLEADING EDGE BEAM 382.4
EDGE RUD AUXILIARY HINGE POINTS STA SPAR 6% (EXAMPLE) 332.4
LE STA
CHORD  (11 LOCATIONS) RUD STA 282.5
204.7 RUD STA 257.54
FRONT RUDDER HINGE LE STA RUD STA 232.6
FIN STA  SPAR 70% CHORD
124.7
47.7
LE STA REAR RUD STA

8.6
53.5  SPAR 207.6
LE STA 0 7.9
RUD STA 157.7

FIN STA 0 LOWER RUDDER
A
8.9
RUD STA 132.7
FIN WL
E
C
D
F
25.2
RUD STA 107.8
RUD STA
B
FIN
27.7
RUD RUD RUD 82.8
FIN WL BWL 366.5
BWL 359.8
STA
144.4
STA STA8.1
STA 0 9.7
149.5
29 32.9
161.9
BODY 158
CROWN
264.4
LINE

323.1
461.5
B STA
2252.7

FWD
LEFT SIDE VIEW
____ ALL DIMENSIONS ARE IN INCHES.
NOTE:
Vertical Stabilizer and Rudder Station Diagram
Figure 1

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 06-31-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

HORIZONTAL STABILIZER AND ELEVATOR STATION DIAGRAM - DESCRIPTION AND OPERATION
1.
STABILIZER STATIONS ARE PERPENDICULAR TO REAR SPAR CENTERLINE.

2.
LEADING EDGE STATIONS ARE PERPENDICULAR TO LEADING EDGE.

3.
ELEVATOR STATIONS ARE PERPENDICULAR TO ELEVATOR HINGE.

4.
TO CONVERT STABILIZER STATION TO LEADING EDGE STATION AT LEADING EDGE. LE STA = (1.03) STAB STA.

5.
TO CONVERT STABILIZER STATION TO ELEVATOR STATION AT ELEVATOR HINGE. ELEV STA = STAB STA - 128.2. 6.STABILIZER BUTTOCK LINES ARE PARALLEL TO BODY BUTTOCK LINE 0.

 

ALL DIMENSIONS ARE IN INCHES
Horizontal Stabilizer and Elevator Station Diagram Figure 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 06-41-00
 ALL  ú ú 01 Page 1 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

WS _________________________________________ REF DWG
WING STATIONS - DESCRIPTION AND OPERATION
110U0001
0.0
90`
ACCESS DOOR
FUEL BAFFLE
(6 LOCATIONS)

BBL O WBL O
INBOARD FLAP
JACK
FUEL FILLER

POINT
NECK

WBL
128.45 WBL LANDING GEAR SUPPORT BEAM
150.00
BODY SKINLANDING GEAR TRUNNION
WS 294.62
INBOARD FLAP TRACK WBL 235.200
WS 338.00
TRAILING EDGE SUPPORT BEAM
SPOILERS
WS 411.420
INBOARD FLAP TRACK
WBL 353.000

KRUEGER FLAPS
(NO. 11 THRU 13)

BOOST PUMP ACCESS DOOR
2`
NACELLE WBL 470.00
INBOARD AILERON
ACCESS HOLES TANK END
(40 LOCATIONS)
OUTBOARD FLAP TRACK VARIABLE CAMBER FLAPS
WBL 584.977 (NO. 1E THRU 10)
OUTBOARD FLAP SPOILERS WS 934.00
WS 862.00
OUTBOARD FLAP TRACK WBL 743.828
FUEL FILLER NECK DRY BAY 1
REMOVABLE RIB SECTION WBL 834.00
WS 1056.00
NACELLE
FUEL TANK ACCESS DOOR STRUCTURAL ACCESS (17 LOCATIONS) DOOR (9 LOCATIONS)
2` OUTBOARD AILERON WS 1168.00
FUEL TANK ACCESS END OF MID SPAR
DOOR DRIP STICK TANK END
LOCATION JACK POINT
(5 LOCATIONS)
WS 1280.00 SURGE TANK
WS 1308.00 TANK END ERSS 1558.716
FWD
FUEL SURGE TANK ACCESS DOOR
JETTISON (2 LOCATIONS) ERSS LEFT WS 1485.00
1617.716 ERSS 1675.540
SURGE TANK END WBL 1241.00
WBL 1252.50 NOTE: REFER TO CHAPTER 57 FOR SECONDARY
STRUCTURE IDENTIFICATION.
 
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