76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 411 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
A
1. NO. 2 THRUST LEVER (SHOWN REMOVED FOR CLARITY)
6. NO. 1 THRUST LEVER SEE A
4. NO. 1 START LEVER STAND 2. CONTROL
5. DOWEL
3. NO. 2 START LEVER FWD
Thrust Lever Installation
Figure 406
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 412 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
2) No. 2 start lever 3) No. 2 thrust lever 4) No. 1 thrust lever 5) No. 1 start lever 6) Speed brake crank, and if it is necessary, a spacer on each
side
7) Stabilizer trim indicator with spacer.
CAUTION: MAKE SURE THAT THE TWISTED LOCKWIRE ENDS DO NOT EXTEND
_______
MORE THAN THE WIDTH OF THE DRUM. INTERFERENCE WITH
ADJACENT COMPONENTS CAN OCCUR.
(b)
Install the cable to the drum.
1) Put the ball terminal in the relieved area and install lockwire.
(c)
Put the spacers in the positions they were at before the
removal.
NOTE: Make sure that the spacers are in the thrust lever
____
assemblies.
(d) Move the left control shaft from the right to the left while
you put the levers and the spacers in position.
S 434-043-C01
(2) Complete the installation of the left control shaft as follows:
(a) Push the left control shaft against the dowel (5).
CAUTION: DO NOT LET THE SPACERS FALL WHEN YOU PUSH THE DOWEL
_______ FROM THE CONTROL STAND. THE SPACERS WILL BE DIFFICULT TO GET BACK.
(b)
Push the dowel with the left control shaft to the left until
the dowel is clear of the control stand.
(c)
The left control shaft should extend 0.25 +0.06/-0.07 inch
through the frame of the left control stand.
S 434-044-C01
(3)
Put the key (9, Fig. 404) into the shaft and the frame of the left control stand.
S 434-045-C01
(4)
Install the nut (3) on the left control shaft and tighten the nut to 100-150 inch-pounds.
(5)
Install lockwire on the nut and the frame.
S 434-046-C01
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 413 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 414-083-C01
(6)
Open the access door No. 1201 to the electronic equipment bay (AMM 12-31-11/201).
S 424-084-C01
(7)
To install the left thrust lever, install the following pins into 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
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