(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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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