(b)  
Make sure you can freely install the rig pin through the forward drum on the speed brake into the structure in the lower nose compartment. If you cannot freely install the rig pin, do these steps: 1) Disconnect the top end of the bottom control rod from the

 idler link.
 2)  Loosen the checknut and adjust the rod end until you can install the rod end bolt freely with the rig pin installed.
 3)  Install the rod end bolt with the washer under the bolthead. a) Install the washer and locknut on the rod end bolt.
 4) Tighten the checknut on the rod end. 5) Make sure you can see the rod end through the inspection hole in the control rod. 6) Remove the rig pin.
 S 864-022-C01
 (8)  Pressurize the A and B hydraulic systems and resevoirs (AMM 29-15-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-02
 STANDS  ú CONFIG 1 ú C02 Page 414 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
START LEVERS - REMOVAL/INSTALLATION
___________________________________ ú
 TASK 76-11-02-904-001-C02
 1. Start Levers Removal and Installation
_____________________________________
 A. General
 (1) Do not use this configuration.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
 76-11-02 STANDS WITH A TIE ROD THROUGH THE SPLINE ú CONFIG 2 SHAFT ú C01A.1 Page 401
 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
START LEVERS - REMOVAL/INSTALLATION
___________________________________
 1.  General
_______
 A.  This procedure has two tasks. The first task removes the start levers. The second task installs the start levers.
 B.  For this procedure, the stabilizer trim splined control wheel shaft will be referred to as the spline shaft.
 TASK 76-11-02-004-001-C03
 2.  Remove the Start Levers
_______________________
 A.  Equipment
 (1)  
Rig Pin Assembly - F70207-11.
 Component of Rig Pin Kit
 F70207-1, -2, -61 or -78.
 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)  
Wrench Kit - Control Stand, C76002

 (4)  
Screwdriver - 90 degree No. 2 Phillips bit

 B.  References
 (1)  
AMM 12-31-11/201, Body Section 41 Access Doors and Panels

 (2)  
AMM 26-21-51/401, Engine and APU Fire Control Module

 (3)  
AMM 27-09-14/201, Flight Control Cables

 (4)  
AMM 27-51-94/401, Flap 40 Unit Switches

 (5)  
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby

 (6)  
AMM 76-11-04/201, Engine Control Cables

 C.  Access
 (1)  
Location Zones
 101/102 Control Cabin
 202 Lower Nose Compartment
 205 Electronic Compartment
 208 Forwrad Cargo Compartment

 (2)  
Access Panels
 1103L Forward Access Door
 1201L Forward Equipment Access Door
 4404R Forward Cargo Door

 D.  Prepare to Remove the Start Levers
 S 864-002-C03
 (1) Depressurize the hydraulic systems A and B (AMM 29-15-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS REINFORCED CONTROL ú
　
中國航空網 m.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(42)