(4)  
AMM 54-32-01/401, Forward Fairing

 (5)  
AMM 71-11-02/401, Fan Cowl Panels

 (6)  
AMM 76-11-00/501, Engine Control System

 (7)  
AMM 78-31-00/201, Thrust Reverser System

 C.  Access
 (1)  Location Zones
 303, Left Wing Leading Edge
 403, Right Wing Leading Edge
 507, Left Strut Area
 607, Right Strut Area

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 76-11-00
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)  Access Panels
 6301, Leading Edge Access Door, Eng. No. 1
 6401, Leading Edge Access Door, Eng. No. 2
 6302, Front Spar Access Panel, Eng. No. 1
 6402, Front Spar Access Panel, Eng. No. 2
 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

 D. Prepare for the Examination
 S 046-033-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 EQUIPMENT.
 (1)  Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
 S 046-034-C00
 WARNING: REFER TO AMM 27-81-00/201 FOR THE INSTALLATION OF THE LOCK FOR
_______ THE LEADING EDGE FLAP. THE FLAPS CAN MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
 (2)  Extend the leading edge flaps and install the flap locks
 (AMM 27-81-00/201).

 NOTE: You must extend the leading edge flaps to get access to the
____ engine control cables between the fuselage and the strut.
 S 016-036-C00
 (3)  Open the access door, 1103L, to get to the thrust lever and the start lever drums that are below the control stand.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 016-035-C00
 (4)  
Open the access door, 1201L, to get access to the forward fuselage
 turnbuckles and the two autothrottle mechanisms that are above the
 electronic equipment shelves.

 S 016-037-C00

 (5)  
Go into the forward cargo compartment, through the forward cargo
 door, 4404R, to get access to the aft fuselage turnbuckles through
 the cargo compartment ceiling.

 S 016-038-C00

 (6)  
Remove the ceiling lining in the forward cargo compartment
 (AMM 25-52-65/401).

 S 016-039-C00

 (7)  
Remove the left fan cowl panel (AMM 71-11-02/401).

 S 016-040-C00

 (8)  
Remove the access panel, 6301 or 6401, from the upper aft surface of the strut (AMM 12-31-71/201).

 S 016-061-C00

 (9)  
Remove the access panel, 6302 or 6402, from the leading edge
 (AMM 12-31-71/201).

 S 016-041-C00

 (10)
 Remove these access doors from the upper and side surfaces of the
 strut (AMM 12-31-91/201).

 (a)  
ON ENGINE NO. 1; remove the access doors, 5726, 5727, 5728, 5729 and 5731.

 (b)  
　
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