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 1)  Make sure the pin/bolt, end caps, bolt, nut, and washers turn together as an assembly. a) If it is necessary, you can tighten the castelated nut
 on the pin/bolt assembly to a maximum torque of 200 pound-inches (22.6 N.m) until the assembly turns. 2) You can adjust the chain hoists to more accurately find the correct load.
 NOTE: When you remove the load correctly, the pin/bolt
____ (that you will remove) will turn easily.
 G.  Remove the Applicable Pin/Bolt.
 S 024-027-B00
 CAUTION:_______MAKE SURE YOU USE A BRASS SLUG TO PUSH OUT THE ATTACH PIN. IF YOU DO NOT USE A BRASS SLUG, THE CLEVIS MAY NOT STAY ALIGNED WITH THE LUG. DAMAGE TO THE BUSHINGS OR THE STRUCTURE CAN OCCUR.
 CAUTION: MAKE SURE ALL THE UPPER LINK PINS AND MIDSPAR FUSE BOLTS ARE
_______
 INSTALLED. DAMAGE TO THE STRUCTURE CAN OCCUR.

 (1)  Remove the forward pin from the diagonal brace (Figure 402,
 Detail F).

 (a)  If you remove the diagonal brace, do these steps:
 1)  Look for markings on the brace that identify the airplane, the strut position, and the center-to-center distance.
 NOTE: If the brace is marked with this data, it is an
____ optional (custom fitted) diagonal brace.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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A

737-300/400/500
MAINTENANCE MANUAL

STRUT
UPPER LINK  FUSE PIN SEE D  SEE  B  C 
STRUT  PIN SEE  E  FUSE BOLT (QTY 2) 
STA 194.24 

1 SLING ATTACH POINT SEE  A  H  SEE PIN  F  DIAGONAL BRACE  FUSE PIN SEE G 
FWD 
1  PERMITTED WHEN FITTING NEW DIAGONAL BRACE FOR DRILLING MEASUREMENT 0-3000 POUNDS UP OR DOWN PERMITTED TO FIT THIS POINT. 1500 |100 POUNDS UP LOAD DIAGONAL BRACE APPLIED TO SLING FITTING AT 
Nacelle Strut Installation Figure 402 (Sheet 1) 

E37009
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
UPPER LINKASSEMBLY
MID SPAR 
ATTACH FITTING 
SIDE LINK 
ASSEMBLY 
LOWER SPAR 
MID SPAR  ATTACH FITTING 
ATTACH FITTING 
FWD  DIAGONAL 
BRACE 
A 
WING ATTACH 
FITTING 
NACELLE STRUT 
0.400 (OUTBOARD)0.520 
0.180 0.060 (INBOARD) 
2 

B 2
MEASUREMENT AFTER STRUT INSTALLATION
WITH NO UP OR DOWN LOAD AT STA 194.24

Nacelle Strut Installation Figure 402 (Sheet 2)
E37168
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
NUT
WING FITTING MIDSPAR ATTACH WING-CENTER (2 LOCATIONS)
WASHER (2 LOCATIONS)

6
(2 LOCATIONS) (2 LOCATIONS) (2 LOCATIONS)

WING FITTING
UPPER LINK FUSE PIN (VIEW IN THE AFT DIRECTION)

D 0.020-0.060 INCH (0.50-1.52 mm) PERMITTED AFTER INSTALLATION OF SIDE LINK ASSEMBLIES
0.020-0.105 INCH (0.50-2.67 mm) PERMITTED AFTER INSTALLATION OF SIDE LINK ASSEMBLIES
CORROSION PREVENTIVE COMPOUND MIL-C-11796,
0.050 INCH (1.27 mm) THICK

6
OPTIONAL TO REMOVE AND NOT REINSTALL
WASHER AT THIS LOCATION.

Nacelle Strut Installation Figure 402 (Sheet 3)
E37169
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