(b)  
Connector DO8315J:

 1)  Pins Wire
 No. 1 001
 No. 2 002
 No. 3 003
 No. 4 004
 No. 5 005
 No. 6 006

 S 424-086-C01
 (8)  To install the right thrust lever, install the following pins into connectors DO8313J and DO8315J (Figs. 405 and 406):
 (a)  
Connector DO8313J:

 1)  Pins Wire
 No. 19 031
 No. 20 032
 No. 21 033
 No. 22 034
 No. 23 035
 No. 24 036

 (b)  
Connector DO8315J:

 1)  Pins Wire
 No. 19 021
 No. 20 022
 No. 21 023
 No. 22 024
 No. 23 025
 No. 24 026

 S 424-085-C01
 (9)  
Connect the left (right) thrust reverser wire bundle to other wire bundles as necessary.

 (10)
 Install the clamps for the wire bundle.

 S 424-087-C01
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 414 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 434-048-C01
 (11) Install the control wheel shaft (7, Fig. 404) for stabilizer trim and the sprocket in the left control shaft.
 NOTE: Install with a long spacer and a bearing at the left end.
____
 S 434-049-C01
 (12)
 Put the stabilizer trim chain on the sprocket.

 S 434-075-C01

 (13)
 Install the connector link (10, Fig. 403).

 S 434-050-C01

 (14)
 Install the control wheel (1, Fig. 404) for left stabilizer trim on the control wheel shaft (7).

 S 434-051-C01

 (15)
 Install the right control shaft (11, Fig. 403) with the levers on the control wheel shaft (2).

 (a)  Assemble the right control shaft with the cranks put in
 sequence from left to right:  flap handle, spacer, stabilizer
 trim indicator, spacer, and nut.
 (b)  Make sure that the spacers are installed between the bearings
 on the flap handle.
 (c)  Put the assembly on the control wheel shaft (2).
 NOTE:____ Make sure that the two bearings and the spacer are
 correctly seated and that the flap switch lever enters
 the cam on the flap drum.

 S 434-052-C01
 (16) Connect the indicator link (12) to the stabilizer trim indicator with bolt (13).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
 76-11-01 STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 415
 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-053-C01
 (17)
 Remove the nut (1) from the right control shaft (11).

 S 434-054-C01

 (18)
 Attach the right control stand frame (3) to the control stand.

 S 434-055-C01

 (19)
 Connect the cutout switches (14).

 S 434-056-C01

 (20)
 Install the key (4) in the right control shaft and the right frame.

 S 434-057-C01

 (21)
 Install the nut (1).

 (a)
Tighten the nut to 100-150 inch-pounds.

 (b)
Install lockwire on the nut and the frame.

 S 434-076-C01
 (22)
 Install lockwire on the nut and the frame.

 S 434-058-C01

 (23)
 Install the cover assemblies (5, Fig. 404) on the control stand.

 S 434-059-C01

 (24)
 Install the horn cutout switch (16, Fig. 403).

 S 434-060-C01

 (25)
 Install the forward and aft cover angles (6 and 8, Fig. 404) on the control stand.
　
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