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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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