S 825-102

 (28)
 AIRPLANES WITH WASHERS BELOW THE UPSTOP ADJUSTMENT BOLT HEAD; Align the slats to be in plane with the distance between the adjacent slats to 0.00 to 0.03 inch at the slat leading edge.

 S 825-103

 (29)
 AIRPLANES WITH SHIMS BELOW THE UPSTOP ADJUSTMENT BOLT HEAD; Align the slats to be in plane with the distance between the adjacent slats to 0.00 to 0.06 inch at the slat leading edge.

 S 425-105

 (30)
 If the torsion rods are not installed, install the torsion rods (Fig. 506):

 (a)  Install the torsion rod through the auxiliary track support
 structure.
 (b)  Install the washers to the detent arm side.
 (c)  Align the index marks between the torsion rod and the detent
 arm.
 (d)  Adjust the torsion rod axially.
 1) BEJ B-2531 THRU B-2532;
 Add or remove the washers on the torsion rod until the
 detent arm centerline is 1.25 +/- 0.03 inch or 31.75 +/-
0.76 mm (dimension X) from the auxiliary track centerline
 (View H-H, Fig. 505).
 NOTE: The torsion rod must turn freely after the washer____
 adjustment.
 2) ALL EXCEPT BEJ B-2531 THRU B-2532;
 ON AIRPLANES WITH SHORTER TORSION ROD END LENGTHS (65C25690
 -3, -4) AND SLOTTED TRUNNION (65C25699-3);
 add or remove the washers on the torsion rod until the
 detent arm centerline is 1.16 +/- 0.03 inch or 29.46 +/-
0.76 mm from the auxiliary track centerline, as initial
 measurement before slat installation. Do the final
 adjustment of the detent arm after slat installation and
 make sure the detent arm is centered on the centerline of
 the detent arm roller (View H-H,Fig. 505).
 NOTE: The torsion rod must turn freely after the washer____
 adjustment.

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A 737-300/400/500MAINTENANCE MANUAL
 3)  Align the index marks again if it is necessary.
 (e)  Align the index marks to add the right plate assembly, washers,
 and torque shaft arm to the torsion rod end opposite of the
 detent arm.
 (f)  Remove or add the washers to make sure that the right plate
 assembly is correctly installed.
 NOTE:____ The torsion rod must turn freely after the washer
 adjustment.
 (g)  Tighten the nuts to 50-70 pound-inches.
 (h)  Connect the left and right plate assemblies with a trunnion,
 washer, and cotter pin.
 (i)  Move the plate assemblies up.
 (j)  Set the bushing in the position to hold the torsion rod as
 shown in Detail B-B.
 (k)  Install the plate assemblies to the structure with two plates,
 four bolts and nuts.
 (l)  Tighten the nuts to 20-25 pound inches.
 (m)  Install the torsion rod bolts through the trunnion and the
 torque shaft arm.

 S 035-106
 (31)
 Loosen the detent arm bolts.

 S 865-252

 (32)
 Move the flap control lever to the 10-unit detent to fully extend the leading edge slats.

 NOTE: Remove and install slat actuator locks and obey safety
____ warnings to prevent injury to persons or damage to equipment.
 S 435-107
 (33) Install the cam plate and the retainer plate.
 NOTE: It can be easier to do the detent arm adjustment with the
____ slats in the fully extended position.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-00
 ALL  ú ú 02 Page 542 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-253
 (34)
 Move the flap control lever to the 1-unit detent to extend the slats to the intermediate position.

 (a)  
Make sure the detent arm roller touches the bottom of the cam plate.