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NOTE:____The 0.10 inch clearance adjustment is done with ú three way adjustable downstops only. ú
 (b)  If you find that the required 0.10 inch minimum clearance is
 not there or can not be adjusted, do one of these tasks: ú 1) Inspect the auxiliary tracks and its support fittings for ú damage and adjust the 0.10 inch clearance with the ú downstops following the procedure "Do a check of the ú clearance between the slat upper trailing edge to the fixed ú leading edge" (AMM 27-81-00/501 "Leading Edge Flap and ú Slats - Adjustment/Test").
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 27-81-41
 ALL  ú ú 02.1 Page 401 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SLAT ACTUATOR 
SLAT 6 (RIGHT WING) SLAT 1 (LEFT WING)  SEE  B 
SLAT 2 (LEFT WING) 
SLAT 5 (RIGHT WING) 
SLAT 3 (LEFT WING) 
SLAT 4 (RIGHT WING) 
HYDRAULIC  SUPPORT 
LINES  FITTING 
A 
A 

LEADING EDGE SLAT ACTUATOR DOOR SLAT ACTUATOR MOUNTING LUG FOR DOOR INSTALLATION
SEE B
LEADING
EDGE SLAT
INBOARD RIB
LOWER CHORD

OUTER
LEADING EDGE
PISTON
SLAT ACTUATOR SUPPORT
B
INNER PISTON
B
SLAT ACTUATOR A
Leading Edge Slat Actuator Installation
Figure 401 (Sheet 1)

A55138
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 27-81-41
 ALL  ú ú 03 Page 402 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

SLAT ACTUATOR DOOR

 

A-A
B-B
ON LEFT WING SLATS, INSTALL NUT ON THE
INBOARD SIDE OF SUPPORT FITTING.
ON RIGHT WING SLATS, INSTALL NUT ON THE
OUTBOARD SIDE OF SUPPORT FITTING.

Leading Edge Slat Actuator Installation Figure 401 (Sheet 2)
A55151
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 27-81-41
 ALL  ú ú 03 Page 403 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 27-81-41-004-054
 2.  Leading Edge Slat Actuator Removal (Fig. 401)__________________________________
 A. Special Tools and Equipment
 (1)  
C27012-1 - Leading Edge Slat Actuator Lockout Set

 B.
References

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

 (2)  
29-09-00/201, Hydraulic Reservoir Pressurization System

 (3)  
IPC 27-81-41-02 thru 27-27-81-41-10, LE Slat Actuator Installation

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

 C.
Access

 (1)  
Location Zone 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

 (2)  
Access Panel
 6215 Slat Access Panel, LH
 6222 Slat Access Panel, LH
 6230 Slat Access Panel, LH
 6534 Slat Access Panel, RH
 6522 Slat Access Panel, RH
 6530 Slat Access Panel, RH

 D.
Prepare for Removal

 S 014-001
 (1)  
Remove the inboard and outboard access panels adjacent to the actuator.

 (2)  
Pressurize hydraulic system B (Ref 27-81-00/201).

 S 864-003

 (3)  
Move the flap control lever to the 10-unit detent to extend the slats.

 S 864-002
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