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 404 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F14056
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
STABILIZER TRIM CONTROL WHEELSSTABILIZER POSITION INDICATOR
CONNECTOR LINK
SEE B
IDLER
IDLER SPROCKET CRANK SPROCKET
STABILIZER AFT SUPPORT
TRIM BRAKE LINK
CHAIN ASSEMBLY STABILIZER TRIM FLEXIBLE SHAFT INDICATOR
ASEE FORCE POINT CHAIN DEFLECTION FORCE DEFLECTION 5-POUND 0.25(|0.07) INCH CHAIN DEFLECTION
A
FORWARD TRIM
SPROCKET MECHANISM (|1.0) 4.5
INCHES
FORWARD A
SUPPORT LINK
FWD
TURNBUCKLE
FORWARD TRIM MECHANISM SPROCKET
PIN
A
LINK
CONNECTOR LINK
B
Stabilizer Trim Chain Assembly Adjustment Figure 402
F14057
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 405 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SCREW
(9 LOCATIONS) THRUST LEVER COVERS AND SEALS
COVER LIGHT PLATE SPEED BRAKE LEVER LEVER COVER SPEED BRAKE SCREW LEVER STOP FORWARD THRUST (4 LOCATIONS)
SCREW (8 LOCATIONS)
AFT THRUST LEVER STOP
AND LIGHT PLATE STABILIZER TRIM COVER HORN CUTOUT SWITCH KNOB SCREW (3 LOCATIONS) SCREW SCREW (8 LOCATIONS) (2 LOCATIONS) SCREW FLAP LEVER COVER LIGHT PLATE FLAP LEVER COVER DETENT QUADRANT FLAP LEVER (4 LOCATIONS)
TRIM CUTOUT SWITCH PLATE STABILIZER SCREW (4 LOCATIONS) SCREW (2 LOCATIONS) STABILIZER TRIM INDICATOR LIGHT PLATE STABILIZER TRIM COVER WHEEL SHAFT SPLINED CONTROL STABILIZER TRIM
COVER AND SEALS START LEVER
AFT GUARD PLATE SCREW
SCREW (2 LOCATIONS) FWD STABILIZER TRIM CONTROL WHEEL
Control Stand Access Installation
Figure 403
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 406 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F14059
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
5) Let the right cover and lightplate hang by the electrical cable near the control stand. 6) Attach the right cover and lightplate to the control stand to prevent movement of the lightplate.
(h) Flap lever detent, cover, and lightplate. 1) Remove four screws from the flap lever detent. 2) Remove the flap lever detent. 3) Remove the flap 40 unit switches from the chain guard for
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(44)
