EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.ú
06-32-00
ALL úú 01 Page 202 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
NOTE:
1.
THE FIN STATIONS ARE PERPENDICULAR TO THE 55% LINE
2.
THE LEADING EDGE STATIONS ARE PERPENDICULAR TO THE LEADING EDGE
34.10
3.
THE RUDDER STATIONS ARE PERPENDICULAR TO THE 75% LINE
4.
THE VERTICAL STABILIZER RIBS FROM FIN STATION 81.10 6.20
TO FIN STATION 292.70 ARE ON 9.2 INCH CENTERS LE STA 311.12
5.
TO CONVERT THE FIN STATION AT THE FRONT SPAR
FIN STA 299.15
(10%) LE STA = FIN STA 1.01756521 +
FIN STA 292.70
3.59150051
FIN STA 283.50
6. TANGENT A = 0.52293481
FIN STA 265.10
TANGENT B = 0.78884390
FIN STA 237.50
TANGENT C = 0.84793481
BALANCE WEIGHT (EXAMPLE)
FIN STA 209.90
RUDDER LE FIN STA 182.30
25% CHORD LINE FIN STA 154.70 REAR SPAR 55% CHORD
FRONT SPAR 10% CHORD
FIN STA 127.10
BWL 378.218
FIN STA 99.50
TANGENT POINT
FIN STA 90.30
FIN STA 81.10
FIN STA 69.44
FIN STA 57.77
FIN STA 46.10
FIN STA 9.50
6.50 A
LE STA 0
C
FIN STA 0
35`
B
20.0
20.0
20.5
B STA 1016.00
FIN
THRUST
20.0
19.5
STA
B STA 1085.56
RIB
52.248 FIN
19.5
CONNECTION
STA
19.5
POINTS
56.57
1.65
132.617
BODY STA BODY STA 1007.65
1126.56
BODY
112.75
STA
153.75
840.193
205.00
62.00
46.50
PIVOT POINT (EXAMPLE)
8.00
1.00
FWL
230.25 RUD STA
237.64
RUD STA
233.09
RUD STA
233.09
RUDDER SPAR RUD STA
196.46
FWL 161.0
RUD STA
174.12
242.00
RUD STA 141.52
FWL
112.356 RUD STA 121.64
RUDDER HINGE 75% LINE
RUD STA 86.59
RUD STA
60.15
RUD STA
31.65
RUD STA 23.27
RUD STA
13.33
FIN WL 0 (BWL 300.50)
BODY CROWN LINE
FIN STA 67.70
RUD STA 0.00
BODY STA 1177.81
A
737-300/400/500MAINTENANCE MANUAL
HORIZONTAL STABILIZER AND ELEVATOR STATION DIARGAM - MAINTENANCE PRACTICES
__________________________________________________________________________
1. General_______
A. The horizontal stabilizer and elevator station diagram gives the location of the structural components on the horizontal stabilizer and elevator.
TASK 06-42-00-202-001
2. Horizontal Stabilizer and Elevator Station Diagram (Fig. 201)__________________________________________________
A. Procedure
S 222-002
(1) See Fig. 201 for the horizontal stabilizer and elevator station diagram.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
06-42-00
ALL ú ú 02 Page 201 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
LE STA 0STAB STA 0
BODY STA 1093.417
FRONT SPAR
(CENTER)
AIRPLANE (SYM)
NOTE:HORIZONTAL STABILIZER RIBS FROM STA 83.50TO 295.10 HAVE 9.20 INCH CENTERS
STAB SEMI SPAN 252.10 INCHES
Horizontal Stabilizer and Elevator Station Diagram
Figure 201
A 737-300/400/500MAINTENANCE MANUAL
06-42-00
Page 202
Nov 12/01
A
737-300/400/500MAINTENANCE MANUAL
WING STATION DIAGRAM - MAINTENANCE PRACTICES
____________________________________________
1. General_______
A. The wing station diagram gives the location of the structural components on the wing.
TASK 06-52-00-202-002
2. Wing Station Diagram (Fig. 201)____________________
A. Procedure
S 222-001
(1) See Fig. 201 for the wing station diagram.
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