C.  
Consumable Materials

 (1)
D00015 Grease - Corrosion Preventive, BMS 3-24

 (2)
A00626 Sealant, Environmental Pressure, Chromate Type, BMS 5-95

 D.  
References

 (1)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 (2)
AMM 27-81-41/401, Leading Edge Slat Actuator

 (3)
AIPC 27-81-41 thru AIPC 27-81-41-10, LE Slat Actuator Installation

 (4)
CMM 27-81-47, LE Slat Hydraulic Actuator Assembly

 E.  
Access

 (1)  
Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 302 Wing Outboard Leading Edge with Slats, LH 303 Wing Inboard Leading Edge with Slats, LH 402 Wing Outboard Leading Edge with Slats, RH 403 Wing Inboard Leading Edge with Slats, RH

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL INSTALLATION ROD END BSEE  LE SLAT 2 LE SLAT 3  LE SLAT 1 
SEE  A 
FWD  INBD 
END ATTACHMENT ACTUATOR ROD CSEE  A  ACTUATOR LE SLAT 
PISTON INNER 
NUT 
SPRING  SLEEVE 
SLIDE RETAINER  SPRING SLIDE BUSHING  ROD END EDGE SLAT LEADING PISTON OUTER  ACTUATOR 
LOCK  B ROD END INSTALLATION ROD END  ROD END BOLT  ELECTRICAL CONNECTOR ACTUATOR ROD END ATTACHMENT LOCKNUT ACTUATOR SWITCH LEAD C 
Figure 401 Leading Edge Slat Actuator Rod End Installation 

M10327
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ROD END  ACTUATOR  LOCATING PIN 
SEE  A  NAMEPLATE 
RIG PIN  SLIDE  AND STRAP 

THUMB SCREWS
STARWHEEL
INDEX PIN
ROD END TOOL (MIT65C38058-1)
SPRING
LOCK
SLEEVE
NUT
INNER PISTON
ROD END
(BEFORE THE CHANGE)

A
ROD END
BUSHING
LOCK  SPRING
SLEEVE
NUT
INNER PISTON
ROD END
(AFTER THE CHANGE)

A
Replacement of the Rod End (Non-Reed Switch) Figure 402
L62510
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 F. Procedure
 S 864-048
 (1)  Pressurize hydraulic system B (AMM 27-81-00/201).
 S 864-049
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING
_______ EDGE FLAPS AND SLATS. THE LEADING EDGE FLAPS AND SLATS WILL EXTEND. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  Move the flap control lever to the 10-unit detent to fully extend the flaps and slats.
 S 494-050
 WARNING: CAREFULLY INSTALL THE LEADING EDGE SLAT LOCKOUT SET TO PREVENT
_______ ACCIDENTAL OPERATION OF THE LEADING EDGE SLATS. THE LEADING EDGE SLATS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (3)  
Install the leading edge slat actuator lockout set on the actuators of the leading edge slats (AMM 27-81-00/201).

 S 024-051

 (4)
Remove the slat actuator door from the actuator (AMM 27-81-41/401).

 S 014-052

 (5)  
Remove the access door of the rod end seal to get access to the electrical connector and the rod end bolt.

 S 864-053

 (6)  
Move the flap control lever to the FLAP UP detent.

 S 864-054

 (7)  
When the LE slat is half between the fully extended and the intermediate positions, release pressure from hydraulic system B (AMM 27-81-00/201).
　
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