S 424-046-C03
(5)
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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STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C02 Page 418 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b) Connector DO8315J:
1) Pins Wire
No. 1 011
No. 2 012
No. 3 013
No. 4 014
No. 5 015
No. 6 016
S 424-047-C03
(6) To install the right thrust lever, install the following pins into connectors DO8313J and DO8315J (Figs. 405 and 406):
(a)
Connector DO8313J:
1) Pins Wire
No. 19 031
No. 20 032
No. 21 033
No. 22 034
No. 23 035
No. 24 036
(b)
Connector DO8315J:
1) Pins Wire
No. 19 021
No. 20 022
No. 21 023
No. 22 024
No. 23 025
No. 24 026
S 424-048-C03
(7)
Connect the left (right) thrust reverser wire bundle to other wire bundles as necessary.
(8)
Install the clamps for the wire bundle.
S 424-049-C03
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
76-11-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-050-C03
(9)
Turn the long control shaft until the keyway is at the top.
S 434-051-C03
(10)
Install the cup washer.
NOTE: Align the key tab on the cup washer with the keyway on
____
the long control shaft.
S 434-052-C03
(11)
Install the right control shaft nut on the long control shaft.
S 864-053-C03
(12)
Tighten the control shaft nut to 100-150 inch-pounds.
S 864-054-C03
(13)
Bend the cup washer flange with a lockwasher break tool to hold the control shaft nut.
D. Install the short control shaft, the flap lever and the stabilizer trim indicator.
S 034-055-C03
(1)
Remove the nut and the cup washer from the right end of the short control shaft.
S 434-056-C03
(2)
Install the flap lever, the stabilizer trim indicator, the spacer, and the short control shaft as a unit.
S 434-057-C03
(3)
Install the cable on the flap lever drum.
(4)
Turn the short control shaft until the keyway is at the top.
S 864-058-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 C02 Page 420 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 434-059-C03
(5) Install the cup washer.
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