(b)  
Install the lower end of the control cable through the bearing in the cable support plate on the MEC control box.

 (c)  
Install the second tabwasher and jamnut below the cable support plate.

 (d)  
Do not install the lockwire on the jamnut at this time.

 (e)  
Install the end fitting and the checknut on the control cable.

 (f)  
Connect the end fitting to the MEC shutoff lever with the bolt, the washer below the bolthead, and the nut. 1) Install the bolt with the bolthead toward the engine

 centerline.

 (g)  
Do not install the aft cover on the MEC.

 S 414-017-C00
 (5)  
Install the strut access doors No. 5726 through 5729 and 5731 for the left strut (AMM 12-31-91/201).

 S 414-018-C00

 (6)  
Install the strut access doors No. 5826 through 5829 and 5831 for the right strut (AMM 12-31-91/201).

 S 414-019-C00

 (7)  
Do not install the access panel No. 6301 or 6401 at the fuel shutoff assembly.

 S 824-020-C00

 (8)  
Do the procedure to adjust the start control push-pull cable (AMM 76-11-00/501).

 S 214-021-C00

 (9)  
Make sure the cable casing is not in tension or compression with the penetration fitting (Fig. 401).

 S 394-022-C00

 (10)
 Put the sealant around the casing where it goes through the penetration fitting.

 S 414-027-C00

 (11)
 Install the access panel No. 6301 or 6401 at the fuel shutoff assembly (AMM 12-31-91/201).

 (a)  Apply the sealant from the inside the fan cowl support beam.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-09
 ALL  ú ú C01 Page 410 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 414-023-C00
 (12)
 Install the forward fairing (AMM 54-32-01/401).

 S 414-024-C00

 (13)
 Install the fan cowl panel (AMM 71-11-02/401).

 S 444-025-C00

 (14)
 Do the activation procedure for the leading edge flaps (AMM 27-81-00/201).

 S 444-026-C00

 (15)
 Do the activation procedure for the thrust reverser (AMM 78-31-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 76-11-09
 ALL  ú ú C01 Page 411 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ENGINE START LEVER SWITCHES - REMOVAL/INSTALLATION
__________________________________________________
 1.  General
_______
 A.  This procedure is for the removal and installation of the start lever switches.
 TASK 76-11-10-004-001-C00
 2.  Remove the Start Lever Switches
_______________________________
 A.  Access
 (1)  
Location Zones
 101 Left Control Cabin
 102 Right Control Cabin

 (2)  
Access Panels S1012L Control Stand Forward Access Covers S1012R Control Stand Forward Access Covers

 B.  Procedure (Fig. 401)
 S 864-002-C00
 (1) Open these circuit breakers and attach a DO-NOT-CLOSE tag:
 (a)  P6 Load Control Center
 1) L IGN
 2) R IGN

 S 014-003-C00
 (2)  Remove the forward, bottom panel on the two sides of the pilot's control stand.
 NOTE: The switches are found between the two brackets in the
____
 pilot's control stand.

 S 034-004-C00
 (3)  
Remove the middle brace found behind the forward, bottom panel.

 S 034-005-C00

 (4)
Disconnect the electrical leads from the four switches.

 (a)  Identify the leads to help in the installation.
 S 034-006-C00
 (5)  Remove the mounting screws from each switch.
　
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(81)