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A. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
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)
B. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
512 Left Wing - Krueger Flap No. 2
513 Left Wing - Krueger Flap No. 1
522 Left Wing - Slat No. 4
523 Left Wing - Slat No. 3
524 Left Wing - Slat No. 2
525 Left Wing - Slat No. 1
612 Right Wing - Krueger Flap No. 3
613 Right Wing - Krueger Flap No. 4
622 Right Wing - Slat No. 5
623 Right Wing - Slat No. 6
624 Right Wing - Slat No. 7
625 Right Wing - Slat No. 8
C. Leading Edge Flap and Slat Locks Installation
SUBTASK 27-81-00-480-002
(1) Install the lockout set, SPL-1734 to prevent retraction of the leading edge devices:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
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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.
(a) If the leading edge flaps and slats are not in the full extend (10-unit) position, do this task:
Leading Edge Flaps and Slats Extension, TASK 27-81-00-860-803.
WARNING: MAKE SURE TO INSTALL THE LEADING EDGE FLAP AND SLAT ACTUATORS
LOCKOUT SET TO PREVENT ACCIDENTAL OPERATION OF THE LEADING EDGE
FLAPS AND SLATS. THE LEADING EDGE FLAPS AND SLATS CAN MOVE
QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(b) Install the lockout set, SPL-1734 on the extended actuators of the leading edge flaps and
slats.
SUBTASK 27-81-00-480-003
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE
FLAPS AND SLATS. THE LEADING EDGE DEVICES OPERATE BY SYSTEMS B OR THE
POWER TRANSFER UNIT WITH SYSTEM A. THIS CAN CAUSE INJURY TO PERSONS
OR DAMAGE TO EQUIPMENT.
(2) Install the lock, SPL-1675 to prevent the extension of the leading edge devices by the standby
hydraulic system (Figure 202).
(a) Make sure the ALTERNATE FLAP ARM switch is in the OFF position.
(b) Attach the DO-NOT-OPERATE tag on the ALTERNATE FLAPS ARM switch.
(c) Disconnect the electrical connector from the leading edge standby drive shutoff valve.
(d) Make sure the override lever at the leading edge standby drive shutoff valve is in position
1.
WARNING: MAKE SURE TO INSTALL THE GROUND LOCK ON THE STANDBY HYDRAULIC
MODULE TO PREVENT ACCIDENTAL STANDBY SYSTEM OPERATION OF THE
LEADING EDGE FLAPS AND SLATS. THE LEADING EDGE FLAPS AND SLATS CAN
MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(e) Install the lock, SPL-1675 on the standby hydraulic module.
(f) Install the lockpin.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
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Hydraulic Module Lock Installation
Figure 202 (Sheet 1 of 2)/27-81-00-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Hydraulic Module Lock Installation
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(38)
