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 the stabilizer trim sprocket (AMM 27-51-94/401).
 4)  Remove the knob for the horn cutout switch.
 5)  Remove the three screws from the lightplate for the flap
 lever cover.
 6)  Turn the lightplate for the flap lever cover to get access
 to the screws on the flap lever cover.
 7)  Remove the four screws from the flap lever cover.
 8)  Remove the electrical cable clamps, as necessary, to get
 wire slack.
 9)  Remove the flap lever cover and lightplate.
 10) Put the masking tape on the surface of the lightplate to
 protect the surface. 11) Let the flap lever cover and lightplate hang by the electrical cable near the forward edge of control stand. 12) Attach the flap lever cover and lightplate to the control stand to prevent movement of the lightplate.
 (i)  Stabilizer trim CUTOUT switches. 1) Remove the four screws from the CUTOUT switch plate. 2) Put the masking tape on the surface of the CUTOUT switch
 plate to protect the surface.
 3)  Remove the electrical cable clamps, as necessary, to get
 wire slack.
 4)  Remove the CUTOUT switch plate.
 5)  Let the CUTOUT switch plate hang by the electrical cable
 near the aft right edge of the control stand. 6) Attach the CUTOUT switch plate to the control stand to prevent movement of the switch plate.
 (j)  Side panels. 1) Remove the side panels on the control stand.
 F.  Remove the Splined Shaft, the Stabilizer Trim Sprocket, and the Chain Guard.
 S 024-016-C03
 (1)  Disconnect the right linkage arm for the stabilizer trim indicator.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
 76-11-02 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 407
 ú  Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
STABILIZER TRIM 
CHAIN GUARD 
FLAP LEVER 
CABLE DRUM 
STABILIZER TRIM SPLINED 
CONTROL WHEEL SHAFT  STABILIZER 
(BEARINGS AND SPACERS  TRIM 
NOT SHOWN) CRANK INDICATOR 

STABILIZER TRIM  STABILIZER TRIM 
CHAIN GUARD  INDICATOR CRANK 
STABILIZER TRIM 
CHAIN SPROCKET 
SEE  A 

STABILIZER TRIM CHAIN SPROCKET
SEE B
FLAP LEVER CABLE DRUM
STABILIZER TRIM CHAIN SPROCKET INSTALLATION STABILIZER TRIM CHAIN SPROCKET
AB
Control Shaft Components Installation Figure 404 (Sheet 1)
F14067
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú

 76-11-02
 STANDS WITHOUT A TIE ROD THROUGH THE ú CONFIG 3 SPLINE SHAFT ú C01 Page 408 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
A
A
FWD
STABILIZER RIGHT TRIM CHAIN STABILIZER
LEFT STABILIZER
GUARD TRIM WHEEL TRIM CONTROL
STABILIZERNO. 1 NO. 2 TRIM CHAINTHRUST
START
STABILIZER

WHEEL SPROCKET
LEVER CONTROLBEARING LEVER STAND
TRIM SPLINED (3 LOCATIONS)
CONTROL SHAFT

NO. 1 NO. 2 FRAME
BUSHING
SPACER START THRUST FLAP LEVER (4 LOCATIONS) LEVER LEVER
AND CABLE DRUM
SHIM  SHIM 
BUSHING LONG CONTROL SHAFT  SHORT CONTROL SHAFT LONG CONTROL SHAFT NUT AND CUP WASHER SHIM CONTROL STAND FRAME SHIM (3 PLACES) CONTROL STAND FRAMEFRAME CONTROL STAND SHIM A-A SHIM (2 LOCATIONS)  BUSHING  WASHER SHORT CONTROL SHAFT NUT AND CUP 
Control Shaft Components Installation Figure 404 (Sheet 2) 

F14068
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú

 76-11-02
　
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