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 12-22-71
 ALL  ú ú 01 Page 303 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 D. Procedure
 S 863-005
 (1)  
Pressurize hydraulic system B (Ref 27-81-00/201).

 S 863-006

 (2)  
Move the flap control lever to the 10-unit detent to extend the leading edge slats.

 S 863-007

 (3)
Release pressure from hydraulic system B (Ref 27-81-00/201).

 S 643-003

 (4)
Lubricate the leading edge slat track rollers (Fig. 301).

 S 863-009

 (5)  
Pressurize hydraulic system B (Ref 27-81-00/201).

 S 863-008

 (6)  
Move the flap control lever to the FLAP UP detent to retract the leading edge slats.

 S 863-010

 (7)
Release pressure from hydraulic system B (Ref 27-81-00/201).

 TASK 12-22-71-603-019
 3.  Leading Edge Slat Track Lubrication___________________________________
 A. Consumable Materials
 (1)  D00015 Grease - BMS 3-24
 B. References
 (1) 27-81-00/201, Leading Edge Flap and Slat Control System
 C. Access
 (1)  Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 302 Wing Outboard Leading Edge with Slats, LH 402 Wing Outboard Leading Edge with Slats, RH
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-71
 ALL  ú ú 01 Page 304 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  Access Panels
 6213 Slat Access Panel
 6217 Slat Access Panel
 6219 Slat Access Panel Removable
 6224 Slat Access Panel Removable
 6227 Slat Access Panel Removable
 6232 Slat Access Panel Removable
 6233 Slat Access Panel Removable
 6513 Slat Access Panel
 6524 Slat Access Panel Removable
 6527 Slat Access Panel Removable
 6532 Slat Access Panel Removable
 6533 Slat Access Panel Removable
 6536 Slat Access Panel Removable
 6539 Slat Access Panel Removable

 D. Procedure
 S 863-020
 (1)  
Pressurize hydraulic system B (Ref 27-81-00/201).

 S 863-021

 (2)  
Move the flap control lever to the 10-unit detent to extend the leading edge slats.

 S 863-022

 (3)  
Release pressure from hydraulic system B (Ref 27-81-00/201).

 S 643-023

 (4)  
Apply large quantity of grease to all roller and rub strip surfaces on the slat main tracks and auxiliary tracks after the adjustment.

 NOTE: Grease must be on these areas at all times except for the
____
 short periods after you clean the tracks.

 S 863-024
 (5)  
Pressurize hydraulic system B (Ref 27-81-00/201).

 S 863-025

 (6)  
Move the flap control lever to the FLAP UP detent to retract the leading edge slats.

 (7)  
Release pressure from hydraulic system B (Ref 27-81-00/201).

 S 863-026
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-71
 ALL  ú ú 01 Page 305 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 12-22-71-603-011
 4.  Leading Edge Krueger Flap Seal Door Lubrication_______________________________________________
 A. Consumable Materials
 (1)  
D00633 Grease - BMS 3-33 (Recommended)

 (2)  
D00013 Grease - MIL-G-23827 (Alternate)

 (3)  
D00569 Grease - MIL-G-21164

 B. References
　
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