55-10-00
 ALL  ú ú B01 Page 2 ú Oct 20/83
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
REAR SPAR
ELEV STA
24.90
ELEV STA
39.02
ELEV STA
66.54
ELEV STA
94.07
ELEV STA
121.59
ELEV STA
REAR SPAR
149.12
CLOSURE

ELEV STA
RIB INTERCOSTAL 176.64
STAB BLFRONT ELEV STA 215.28
SPAR 195.00
ELEV STA
213.32
STAB STA
67.54
STAB
STA

STAB
83.50
STA STAB
101.90
STA STAB
120.30
STA STABSTAB 138.70
STA STABSTA STAB 157.10
STA
92.70  STAB
STA STAB 175.50
STA
111.10  STAB
STA STAB 193.90
STA
129.50  STAB
STA STAB
212.30
STA
147.90  STAB
STA STAB 230.70
STA STA BL
166.30  STAB
STA STABLE STA
249.10  249.81
STA
184.70  STAB
STA56.01
STAB
267.50
STA203.10
LE STA
STA
STAB 285.90
69.93
221.50
STA  CLOSURE RIB
STABLE STALE STA 239.90
STA
86.66  STAB
78.29 LE STA 258.28
STA STAB INBDLE STA 105.26
LE STA 276.50
95.96  STA
LE STA 123.85
LE STA 295.10
114.55
LE STA 142.45  FWD
LE STA
133.15
LE STA 161.04
LE STA
151.75
179.64
LE STA LE STA
170.34 LE STA 198.23
LE STA
188.94
LE STA 216.83
INBD  LE STA
207.53
235.43
LE STA LE STA
226.13 LE STA 254.02
LE STAFWD 244.72
LE STA 272.62
LE STA
263.30
291.21
LE STA
281.91
LE STA
300.51
Horizontal Stabilizer Structure
Figure 2

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 55-10-00
 ALL  ú ú B01 Page 3 ú Jun 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 THRUST BRACE LINKS - REMOVAL/INSTALLATION
_________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the thrust brace links.
 B.  The thrust brace links are located at the rear spar of the horizontal stabilizer center section.
 C.  There are four thrust brace links, two on each side.
 TASK 55-10-10-004-001-B00
 2.  Thrust Brace Links Removal__________________________
 A.  Standard Tools and Equipment
 (1)  Use suitable wood beams (approximately a 4-inch by 4-inch cross-section) to support the center section of the thrust brace link assembly at any approximately horizontal position (Fig. 402).
 B.  References
 (1)  IPC 55-10-00-12, Horizontal Tail Center Section Assembly
 C.  Access
 (1)  
Location Zone
 700 Empennage

 (2)  
Access panel
 3701 Left Stabilizer Trim Access Door

 D.  Prepare for the Removal
 S 494-009-B00
 (1)  Install suitable wood beams to support the center section at any approximately horizontal position (Fig. 402).
 E.  Remove the thrust brace links
 S 024-002-B00
 (1)  Disconnect the upper inboard end.
 (a)  
Remove the cotter pin (2) and nut (3).

 (b)  
Remove washer (4), bolt (7) and bushing (6).

 (c)  
Disconnect the thrust brace link (1) from the center section fitting.

 S 024-003-B00
 (2)  Disconnect the lower inboard end.
 (a)  
Remove the cotter pin (14) and nut (15).

 (b)  
Remove washer (16), bolt (22) and bushing (21).

 (c)  
Disconnect the thrust brace link (27) from the center section fitting.

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