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 407
ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
5) Let the stabilizer trim CUTOUT switch plate hang by the aft right edge of the control stand by the electrical cable. 6) Attach the stabilizer trim CUTOUT switch plate to the control stand to prevent movement of the switch plate.
(j) Remove the side panels.
C. Remove the splined shaft, the stabilizer trim sprocket, and the chain guard (Fig. 404).
S 034-018-C03
(1)
Disconnect the right stabilizer trim indicator linkage arm.
S 034-019-C03
(2)
Hold the stabilizer trim sprocket with one hand, and remove the
spline shaft, bearings, and spacers from the left end of the two
hollow control shafts.
S 864-020-C03
(3)
Saftey the sprocket and the chain in the bottom of the control
stand.
S 034-021-C03
(4)
Remove the aft chain screw with a 90 degree No. 2 Phillips bit
screwdriver.
NOTE:____Get access to the aft screw of the stabilizer trim chain guard through the stabilizer trim cutout switch hole.
S 034-022-C03
(5) Remove the two screws from the stabilizer trim chain guard.
NOTE: Get access to the other two screws of the stabilizer trim
____
chain guard through the side of the control stand.
S 864-023-C03
(6)
Cut the lockwire on the nylon flap lever cam.
(7)
Remove the nylon flap lever cam.
(8)
Remove the stabilizer trim chain guard.
S 034-024-C03
S 034-025-C03
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 408 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 POSITION
NOT SHOWN) INDICATOR
STABILIZER
STABILIZER TRIM POSITION
CHAIN GUARD INDICATOR
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)
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(29)