78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 202 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST DRUM
MOUNTING SCREW TOP
CAM FOLLOWER
LOWER MOUNTING SCREW CSEE SWITCH-AND-BRACKET ASSEMBLY ENGINE NO. 1 BRACKET ASSEMBLY SWITCH-AND- ENGINE NO. 2 BRACKET ASSEMBLY SWITCH-AND-
B
S815
S822 S823
S814 SWITCH ACTUATORS
SWITCH MOUNTING SCREW S827 STOW SWITCH, ARM SWITCH, S826
SWITCH ADJUSTMENT SCREW STOW SWITCH, S825
ARM SWITCH, S824
FWD C ADJUSTMENT SCREW SLOT
Thrust Reverser Arm and Stow Switches Installation
Figure 201 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 203 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
PUSH-PULL CABLE
ROD END
UPPER (LOCKING) ACTUATOR
BELLCRANK
A
Thrust Reverser Feedback Cable Connections
Figure 202
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 204 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C36507
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
REVERSE
REVERSE THRUST LEVER
Reverse Thrust Lever Protractor
Figure 203
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 205 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C36516
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
D5148
D5150
A
Control Stand Electrical Plugs
Figure 204
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RAKE ACTUATED ú
78-34-05
ARM AND STOW SWITCHES ú CONFIG 1 ú C01 Page 206 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C36519
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(3) S 032-006-C01Remove the tie rod nut from the left stabilizer trim wheel (Fig. 201). (a) Remove the trim wheel.
(4) S 032-007-C01Pull the right stabilizer trim wheel with the tie rod from the right side of the control stand.
(5) S 012-008-C01Remove the upper mechanism doors. (a) Disconnect the lightplate electrical connections while you remove the doors. (b) Attach a tag to the connections for easier installation. (c) Prevent the lightplates from possible damage.
(6) S 012-009-C01Remove the lower doors from the control stand.
(7) S 032-010-C01Remove the control lever bracket for stabilizer trim.
(8) S 032-011-C01Remove the upper and lower mounting screws (Fig. 201). (a) Disengage the switch and bracket assembly from the mounting brackets and the cam follower.
(9) S 032-012-C01If you will remove the cam followers, remove the switch bracket.
S 032-013-C01
(10) Disconnect the leads from the applicable switch.
(a) Make a note of the location of the lead connections to the switch terminals.
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 EXHAUST(171)
