(40)
 Close the electronic equipment access door No. 1201.

 (41)
 Supply hydraulic power (AMM 29-15-00/201).

 S 414-079-C01
 S 864-074-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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
S 714-085-C01
 (42) Do the Normal Operations Procedure to make sure the thrust levers are correctly installed (AMM 78-31-00/501).
 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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
THRUST LEVERS - REMOVAL/INSTALLATION
____________________________________
 TASK 76-11-01-904-001-C02
 1. Thrust Levers Removal and Installation
______________________________________
 A. General
 (1) Do not use this configuration.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
 76-11-01 STANDS WITH A TIE ROD THROUGH THE SPLINE ú CONFIG 2 SHAFT ú C01A Page 401
 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST LEVERS - REMOVAL/INSTALLATION
____________________________________
 1.  General
_______
 A.  This procedure has four tasks as follows:
 (1)  
Thrust Lever Removal Preparation

 (2)  
Thrust Lever Removal

 (3)  
Thrust Lever Installation

 (4)  
Put the Airplane to Its Usual Condition

 B.  For this procedure, the stabilizer trim splined control wheel shaft will be referred to as the spline shaft.
 TASK 76-11-01-844-001-C03
 2.  Thrust Lever Removal Preparation
________________________________
 A.  Equipment
 (1)  
Assembly - Rig Pin, F70207-11, Component of Rig
 Pin Kit F70207-93. Optional: MS20392-4C pin
 (or equivalent 0.311 +0.000/-0.002-inch
 diameter, 6-inch long rod or bolt)

 (2)  
Dowel Set - Thrust Lever, Control Stand,
 F80195-1

 (3)  
Hand Tool Set - Control Stand, C76002

 B.  References
 (1)  
AMM 12-31-11/201, Body Section Doors and Panels

 (2)  
AMM 27-09-14/201, Flight Control Cables

 (3)  
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby

 (4)  
AMM 76-11-04/201, Engine Control Cables

 C.  Access
 (1)  Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right
 202 Lower Nose Compartment
 205 Electronic Compartment

 D.  Procedure
 S 864-002-C03
 (1)  
Remove hydraulic power (AMM 29-15-00/201).

 (2)  
Put the thrust levers in the IDLE position.

 (3)  
Put the start levers in the CUTOFF position.

 (4)  
Put clamps on the start cables and the thrust cables.

 S 864-003-C03
 S 864-004-C03
 S 494-005-C03
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
　
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