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F/O Electrical System Panel, P6-2
Row Col Number Name
A 7 C00210 FLIGHT CONTROL FLAP SHUTOFF VALVES
SUBTASK 27-81-00-480-001
(4) Install the lock, SPL-1675 on the standby hydraulic module to prevent LE devices extension by
the standby hydraulic system. To install the lock, do this task: Leading Edge Flap and Slat
Locks Installation, TASK 27-81-00-480-801.
H. Deactivate the Leading Edge Flaps and Slats in the Full Extend Position
SUBTASK 27-81-00-480-006
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.
(1) Install the lockout set, SPL-1734 on the extended actuators of the leading edge flaps and slats. To
install the locks, do this task: Leading Edge Flap and Slat Locks Installation,
TASK 27-81-00-480-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Leading Edge Cruise Depressurization Valve
Figure 201 (Sheet 1 of 4)/27-81-00-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Leading Edge Cruise Depressurization Valve
Figure 201 (Sheet 2 of 4)/27-81-00-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Feb 10/2007
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Leading Edge Cruise Depressurization Valve
Figure 201 (Sheet 3 of 4)/27-81-00-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Feb 10/2007
D633A101-GUN
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Leading Edge Cruise Depressurization Valve
Figure 201 (Sheet 4 of 4)/27-81-00-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-81-00-440-801
3. Reactivate the Leading Edge Flaps and Slats
A. General
(1) If you do the deactivation procedure with the leading edge flaps and slats in the retract position,
then do the steps to reactivate the leading edge flaps and slats in the retract position.
(2) If you do the deactivation procedure with the leading edge flaps and slats in the full extend
position, then do the steps to reactivate the leading edge flaps and slats in the full extend
position.
B. 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)
SPL-1746 Tool - Lockout, LE Shutoff Valves
(Part #: C27038-6, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. 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
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
E. Reactivate the Leading Edge Flaps and Slats In the Retract (UP) Position
SUBTASK 27-81-00-080-001
(1) Remove the lock, SPL-1675 from the standby hydraulic module. To remove the lock, do this task:
　
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