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

 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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C02 Page 419 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 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.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發動機控制 ENGINE CONTROLS(33)