76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 402 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
SPEED BRAKE CONTROL LEVER
UPPER CONTROL ROD
LOWER CONTROL ROD
IDLER
LINK
CHECK NUT
FLOOR
SPEED BRAKE FORWARD DRUM
A
RIG PIN
Speed Brake Control Lever Adjustment
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 403 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
CONTROL WHEELS
STABILIZER
POSITION
INDICATOR
STABILIZER TRIM INDICATOR LINKAGECONNECTOR LINK
ARM SEE B
IDLER SPROCKET IDLER
STABILIZER TRIM SPROCKETINDICATOR CRANK
STABILIZER
AFT SUPPORT
TRIM BRAKE
LINK
INDICATOR
STABILIZER TRIM
FLEXIBLE SHAFT
CHAIN ASSEMBLY
CHAIN DEFLECTION 5-POUND CHAIN DEFLECTIONFORCE POINT DEFLECTION 0.25(|0.07) INCHSEE A
FORCE
A
FORWARD TRIM
MECHANISM
SPROCKET
4.5 (|1.0) INCHESFORWARD
A
SUPPORT LINK
FWD
TURNBUCKLE
FORWARD TRIM MECHANISM SPROCKET PIN
A
LINK
CONNECTOR LINK
B
Stabilizer Trim Chain Assembly Adjustment
Figure 402
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 404 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
1. RIGHT CONTROL
SHAFT NUT 2. STABILIZER
TRIM CONTROL
WHEEL SHAFT
16. HORN CUTOUT STAND FRAME3. RIGHT CONTROL
SWITCH
15. FIRE 4. KEY 5. UPPER RIGHT
CONTROL SIDE DOOR
MODULE
6. RIGHT STABILIZER
TRIM CONTROL
WHEEL
7. TIEROD NUT
(2 PLACES)
14. STABILIZER
TRIM CUTOUT
SWITCHES
13. BOLT
12. STABILIZER TRIM
INDICATOR LINK
11. RIGHT CONTROL
SHAFT
10. CONNECTOR 9. LOWER RIGHT 8. STABILIZER TRIM
LINK ACCESS PANEL CONTROL WHEEL
TIE ROD
FWD
Control Stand Access Installation
Figure 403
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 405 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-016-C01
(2) Pull the tie rod (8) from the right side of the control wheel.
NOTE: It is recommended that you discard the old tie rod nuts and
____
replace with new tie rod nuts.
S 034-017-C01
(3)
Remove the control wheel (6) from the wheel shaft (2).
S 014-018-C01
(4)
Remove the left and right upper side doors (5).
S 014-019-C01
(5)
Remove the lower right access panel (9).
S 864-020-C01
(6)
Disconnect the cutout switches (14).
S 034-021-C01 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 發(fā)動(dòng)機(jī)控制 ENGINE CONTROLS(20)
