(7)
Cut the lockwire and remove the nut (1).
S 034-022-C01
(8)
Remove the fire control module (15) from the aft electronic panel (AMM 26-21-51/401).
S 034-023-C01
(9)
Remove the forward and aft cover tie straps (4 and 2, Fig. 404).
S 034-024-C01
(10)
Remove the forward and aft cover angles (6 and 8).
S 034-025-C01
(11)
Remove the horn cutout switch (16, Fig. 403).
(12)
Lift the cover assemblies (5, Fig. 404) from the control stand.
(13)
Remove the frame (3, Fig. 403).
(14)
Remove the key (4) from the slot in the right control shaft (11).
(15)
Replace the nut (1) from the right control shaft (11).
S 034-026-C01
S 034-027-C01
S 034-028-C01
S 434-029-C01
NOTE: This will permit the spacer, stabilizer trim indicator,
____
spacer and flap handle to be removed as a unit.
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 406 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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. LEFT STABILIZER TRIM CONTROL WHEEL
3. LEFT CONTROL SHAFT NUT
2. AFT TIE STRAP
9. KEY
8. AFT COVER ANGLE
4. FORWARD TIE STRAP
5.
COVER ASSEMBLIES
6.
FORWARD COVER ANGLE
7.
STABILIZER TRIM CONTROL WHEEL SHAFT
Control Stand Center Components Installation
Figure 404
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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
S 034-030-C01
(16)
Remove the bolt (13) and then disconnect the indicator link (12) from the stabilizer trim indicator.
S 034-031-C01
(17)
Remove the right control shaft (11) with the nut, spacer, trim indicator, spacer, and flap handle as a unit.
S 864-032-C01
(18)
Turn the trim wheel (1, Fig. 404) until you can remove the connector link (10, Fig. 403).
S 034-033-C01
(19)
Remove the connector link (10, Fig. 403).
S 034-034-C01
(20)
Remove the chain from the sprocket and safety the chain in the bottom of the control stand.
S 034-035-C01
(21)
Remove the left control wheel (1, Fig. 404) from the control wheel shaft (7).
S 034-036-C01
(22)
Remove the control wheel shaft (7) and the sprocket from the right side of the control stand.
S 014-080-C01
(23)
Open the access door No. 1201 to the electronic equipment bay (AMM 12-31-11/201).
S 024-084-C01
(24)
To remove the left thrust lever, remove the following pins from connectors DO8313J and DO8315J (Figs. 405 and 406):
(a) Connector DO8313J:
1) Pins Wire
No. 1 001
No. 2 002
No. 3 003
No. 4 004
No. 5 005
No. 6 006
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 408 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發動機控制 ENGINE CONTROLS(21)
