76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 412 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
D.  Remove the short control shaft, the flap lever, and the stabilizer trim indicator:
 S 864-026-C03
 (1)  
Make the crimped tab straight on the two control shaft cup washers with a lockwasher removal tool.

 S 034-027-C03

 (2)  
Remove the nut and the cup washer from the right end of the short control shaft with the control shaft wrench and the control shaft nut wrench.

 S 034-028-C03

 (3)  
Remove the flap lever, the stabilizer trim indicator, the spacer, and the short control shaft as a unit.

 S 434-029-C03

 (4)  
Install the cup washer and the nut on the end of the short control shaft, finger tight.

 E.  Remove the thrust lever:
 S 024-031-C03
 (1)  To remove the left thrust lever, remove the following pins from connectors DO8313J and DO8315J (Figs. 405 and 406):
 (a)  
Connector DO8313J:

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

 (b)  
Connector DO8315J:

 1)  Pins Wire No. 1 011 No. 2 012 No. 3 013 No. 4 014 No. 5 015 No. 6 016
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 413 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S114 
S829 
S787 (INBOARD) S272  S77  CONDUIT S564 S566  SEE  A 
(OUTBOARD) S149  2 8  3  4  S819 
R384  S113 
1  7 CONDUIT  S828 S786 
FWD  RIGHT SIDE  4  3  2  S651 S650 
A 
S823 S815 S825 S824 S822 S814  6  8 S827 S826 7  D2487J  6 1 
5  LEFT SIDE A 5 D8315J D8313J D3524J  D5148J  FWD D5150J 
Figure 405 Thrust Lever Wire Bundle Installation 

F13998
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
(2)  S 024-032-C03To remove the right thrust lever, remove the following pins from 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
 (3)  S 024-033-C03Separate the left (right) thrust reverser wire bundle from other wire bundles that do not require removal.
 (4)  S 024-034-C03Remove the clamps for the wire bundle.
 (5)  S 034-035-C03Remove the cable from the thrust lever cable drum.
 (6)  S 864-036-C03Make the crimped tab straight on the long control shaft right cup washer with the lockwasher removal tool.
 (7)  S 034-037-C03Remove the right control shaft nut and the cup washer from the long control shaft. (a) Use the control shaft wrench and the control nut wrench.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 415 ú Mar 12/02
　
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