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_______ 4 MINUTES OPERATION AND 25 MINUTES OFF. FAILURE TO DO THIS CAN CAUSE DAMAGE TO THE DRIVE UNIT.
 (g)  
Set the FLT CONTROL A or B switch on the forward overhead panel (P5) to STDBY RUD. 1) Make sure the STANDBY HYD LOW PRESSURE light comes on. 2) Make sure that the standby hydraulic pump starts. 3) Make sure the STANDBY HYD LOW PRESSURE light goes off.

 (h)  
Monitor the leading edge flaps and slats for 60 seconds.

 (i)  
Make sure that the flaps and slats do not extend.

 NOTE: The leading edge flaps can slowly extend because of
____
 gravity.

 (j) Put the FLT CONTROL switch back to the ON position.
 TASK 27-81-00-825-018
 4. Leading Edge Flaps and Slats - Adjustment/Test
______________________________________________
 A. General
 (1)  
The adjustment of the trailing edge flap system must be correct before you adjust the leading edge flap and slat system. The rigging of the leading edge flap and slat system contains these parts:

 (a)  
The adjustment of the leading edge flap and slat control valve.

 (b)  
The adjustment of the flap nose linkage on each leading edge flap.

 (c)  
The adjustment of each leading edge slat to the aligned position.

 (2)  
You can adjust the leading edge flaps and slats with the airplane on or off the jacks. You can also adjust the leading edge flaps and slats when the airplane has fuel or no fuel in the tanks. You must get the same adjustment tolerances no matter what condition the airplane is in, when you rig the slats.

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 27-81-00
 ALL  ú ú 01 Page 513 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SLAT 1
SEE A
SLAT 2
SEE F
SLAT 3
UPSTOP (4 LOCATIONS EACH SLAT)
WING FIXED LE STRUCTURE SLAT 4
SLAT 5
SLAT 6
M  DOWNSTOP 
SEE  C  D  FOLLOWER BEARING AUXILIARY TRACK 
M 
A  K 
D 
B  LEADING EDGE 
SLAT ACTUATOR 

LEADING UPSTOP
EDGE SLAT
UPSTOP
C
AUXILIARY SLAT TRACK ARM ANTI-ICING
(INSTALLED THIS DUCT DOOR
LOCATION ON SLATS
A
1 AND 6 ONLY)
MAIN SLAT B MAIN SLAT
TRACK TRACK
OUTBD AUXILIARY
SLAT TRACK C  UPSTOP
SLAT 1 SHOWN) FWD
K
THERMAL ANTI-ICING
A
TELESCOPE DUCT
L
NEGATIVE MISMATCH OUTBD (AIRFLOW) AUXILIARY SLAT TRACK ARM
L
SLAT OR
FIXED LE

SEE B
SLAT OR WING FIXED
STRUCTURE LE STRUCTURE
F
Leading Edge Slat Adjustment
Figure 505 (Sheet 1)

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 27-81-00
 ALL  ú ú 01 Page 514 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
ROLLERS
FIXED LEADING EDGE  SEE E
MAIN TRACK COVER PLATE
ADJUSTMENT BOLTS

SLAT
SEE D CLEARANCE BETWEEN THE SLAT LOWER TRAILING EDGE AND THE
CLEARANCE BETWEEN FIXED LEADING EDGE PANEL
THE MAIN TRACK COVER PLATE AND THE BOTTOM SURFACE OF THE LEADING EDGE
(SLAT SHOWN RETRACTED) A-A
FRONT NOMINAL
SPAR POSITION ROLLERS
1B (4 LOCATIONS)
E
DOWNSTOP
FIXED LEADING EDGE
MAIN TRACK
F
MAIN TRACK SLAT
COVER PLATE
F E
(SLAT SHOWN FULLY EXTENDED) A-A
FIXED LEADING EDGE 1A AIRPLANES WITHOUT ADJUSTABLE DOWNSTOPS
1B AIRPLANES WITH THE THREE-WAY ADJUSTABLE DOWNSTOPS
Leading Edge Slat Adjustment Figure 505 (Sheet 2)
FRONT SPAR
1A
DOWNSTOP
HOLE IN SUPPORT RIB (FOR INSTALLATION OF THE DOWNSTOP)
E
FRONT SPAR
DOWNSTOP
1A
HOLE IN SUPPORT RIB
(FOR INSTALLATION OF
THE DOWNSTOP)

E
FRONT SPAR
DOWNSTOP
1B
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