(2)
AMM 27-81-00/201, Leading Edge Flaps and Slats
(3)
AMM 54-32-01/401, Forward Fairing
(4)
AMM 71-11-02/401, Fan Cowl Panels
(5)
AMM 76-11-00/501, Engine Control System
B. Access
(1)
Location Zones
5700, Engine No. 1 (Left)
5800, Engine No. 2 (Right)
(2)
Access Panels 5726L, Strut Access Door, Eng. No. 1 - left 5727L, Strut Access Door, Eng. No. 1 - top 5728L, Strut Access Door, Eng. No. 1 - top 5729L, Strut Access Door, Eng. No. 1 - top 5731L, Strut Access Door, Eng. No. 1 - right 5746L, Fan Cowl Panel, Eng. No. 1 - left 5826R, Strut Access Door, Eng. No. 2 - left 5827R, Strut Access Door, Eng. No. 2 - top 5828R, Strut Access Door, Eng. No. 2 - top 5829R, Strut Access Door, Eng. No. 2 - top 5831R, Strut Access Door, Eng. No. 2 - right 5846R, Fan Cowl Panel, Eng. No. 2 - right
C. Remove the start control (push-pull) cable (Fig. 401).
S 044-002-C00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE THRUST REVERSER TO
_______ PREVENT THE OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT.
(1) Do the deactivation procedure for the thrust reverser (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-09
ALL ú ú C01 Page 401 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
START CONTROL CABLE
STRUT ACCESS PANELS
1
SEE C
CLAMP
SEE C
BLOCKS CLAMP
SEE B BLOCKS CLAMP
QUICK-RELEASE CLAMPCLAMPS
START CONTROL CABLE
SEE D 1
ENGINE NO. 1
A
SEE B QUICK-RELEASE CLAMPS
SEE D
1 FOR THESE THREE CLAMP BLOCKS ONLY, AS AN OPTIONAL METHOD, YOU CAN
ENGINE NO. 2
INSTALL THE CABLES LIKE THE OPPOSITE ENGINE.
A
Start Control Push-Pull Cable Installation Figure 401 (Sheet 1)
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ALL ú ú C01 Page 402 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FAN COWLPENETRATION
SUPPORT BEAM
FITTING
START CONTROL CABLE
B
RETAINER PIN
WASHER (ENG NO. 1)
CABLE RETAINER (ENG NO. 2)
BUSHING
FUEL SHUTOFF ASSEMBLY
QUADRANTSTART SUPPORT
CONTROL BRACKET
CABLE
JAMNUTS
FWD
NOTE: ENGINE NO. 1 INSTALLATION SHOWN ENGINE NO. 2 INSTALLATION SIMILAR.
C
Start Control Push-Pull Cable Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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ALL ú ú C01 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
BOLT
WASHER
WASHER START CONTROL CABLE SUPPORT CABLE START CONTROL CABLE
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