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Reference Description
SPL-1734 Lockout Set - Leading Edge Slats and Krueger Flaps Actuators
(Part #: C27051-29, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
(Opt Part #: C27051-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
SPL-1739 Kit - Slat Rigging Tools
(Part #: C27045-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
C00528 Compound - Corrosion Preventive, Petroleum Hot
Application (Soft Film)
MIL-C-11796,
Class III
E. Location Zones
Zone Area
522 Left Wing - Slat No. 4
523 Left Wing - Slat No. 3
524 Left Wing - Slat No. 2
525 Left Wing - Slat No. 1
622 Right Wing - Slat No. 5
623 Right Wing - Slat No. 6
624 Right Wing - Slat No. 7
625 Right Wing - Slat No. 8
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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F. Slat Actuator and Main Track Downstop Adjustment
SUBTASK 27-81-00-860-026
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE
COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER.
THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) To pressurize hydraulic system B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-81-00-860-061
CAUTION: MAKE SURE THE INBOARD FAN DUCT COWL AND THE INBOARD AND OUTBOARD
THRUST REVERSERS ARE CLOSED OR REMOVED BEFORE YOU EXTEND THE
LEADING EDGE FLAPS AND SLATS. THERE IS NOT SUFFICIENT CLEARANCE FOR
THE FLAPS AND SLATS TO EXTEND IF THE INBOARD FAN DUCT COWL AND THE
INBOARD AND OUTBOARD THRUST REVERSERS ARE IN THE OPEN POSITION. THIS
CAN CAUSE DAMAGE TO EQUIPMENT.
(2) Move the flap control lever to the 10-unit position to extend the leading edge slats to the full
extend position.
SUBTASK 27-81-00-480-008
WARNING: MAKE SURE TO INSTALL THE LEADING EDGE SLAT ACTUATOR LOCKOUT SET TO
PREVENT ACCIDENTAL OPERATION OF THE LEADING EDGE SLATS. THE LEADING
EDGE SLATS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND
DAMAGE TO EQUIPMENT.
(3) Install the lockout set, SPL-1734 on the adjacent leading edge slats. To install the lockout set, do
this task: Leading Edge Flap and Slat Locks Installation, TASK 27-81-00-480-801.
SUBTASK 27-81-00-860-027
(4) Move the flap control lever to the 1-unit position to retract the leading edge slat to the extend
position.
NOTE: If the leading edge slat [31] is in the full extend position, the slat actuator [29] will be
preloaded against the leading edge slat [31].
SUBTASK 27-81-00-860-028
(5) To remove power from hydraulic system B, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
SUBTASK 27-81-00-020-004
(6) Remove the slat actuator door [39] from the slat actuator [40]:
(a) Remove the bolts [35], washers [36], washers [37], and nuts [38] that attach the slat actuator
door [39] to the slat actuator [40].
(b) Remove the bolts [32], washers [33] and nuts [34] that attach the slat actuator door [39] and
the bracket to the slat actuator [40].
(c) Remove the slat actuator door [39].
(d) Temporarily install the bolts [32], washers [33] and nuts [34] to attach the bracket to the slat
actuator [40].
SUBTASK 27-81-00-020-005
(7) Disconnect the slat actuator [40] from the leading edge slat [31]:
(a) Remove the bolts [46] and washers [47] that attach the bolt retainers [48] to the leading
edge slat [31].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 512
Jun 10/2004
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(b) Remove the bolt retainers [48] from the leading edge slat [31].
WARNING: MAKE SURE YOU HOLD THE LEADING EDGE SLAT IN ITS POSITION. THE
LEADING EDGE SLAT CAN FALL TO THE FULL EXTEND POSITION. THIS CAN
CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(c) Hold the leading edge slat [31] while you remove the nut [43], washer [42], bushing [41],
washer [49] and bolt [50].
SUBTASK 27-81-00-860-029
(8) Carefully let the leading edge slat [31] move down to the full extend position.
SUBTASK 27-81-00-860-030
(9) Use hydraulic power to extend the slat actuator [40] to the full extend position:
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT
　
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