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Page 211
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Procedure
SUBTASK 27-81-00-860-007
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-81-00-860-008
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING EDGE
FLAPS AND SLATS, AND THE TRAILING EDGE FLAPS. THESE SURFACES WILL MOVE
AND CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(2) Move the ALTERNATE FLAPS ARM switch on the P5 panel to the ARM position.
SUBTASK 27-81-00-860-009
(3) Move the ALTERNATE FLAPS control switch to the DOWN position to extend the flaps and slats
as it is necessary.
NOTE: The leading edge flaps and slats will not retract with alternate control.
SUBTASK 27-81-00-860-010
(4) Move the ALTERNATE FLAPS control switch to the OFF position.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-81-00-860-011
WARNING: MAKE SURE THE POSITION OF THE FLAPS AND SLATS AGREES WITH THE POSITION
OF THE FLAP CONTROL LEVER. WHEN YOU PRESSURIZE THE HYDRAULIC SYSTEM
B, THE FLAPS AND SLATS WILL MOVE AUTOMATICALLY TO THE POSITION OF THE
FLAP CONTROL LEVER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(1) Move the ALTERNATE FLAPS control switch until the flaps and slats are in the same position as
the flap control lever or move the flap control lever to the position of the flaps and slats.
SUBTASK 27-81-00-860-012
(2) Move the ALTERNATE FLAPS control switch to the OFF position.
SUBTASK 27-81-00-860-013
(3) Move the ALTERNATE FLAPS ARM switch to the OFF position to disarm the alternate control
system.
------------------------- END OF TASK ---------------------------
TASK 27-81-00-860-803
6. Leading Edge Flaps and Slats Extension
A. 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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(Continued)
Zone Area
212 Flight Compartment - Right
B. Procedure
SUBTASK 27-81-00-860-014
(1) Do one of these tasks to extend the leading edge flaps and slats:
CAUTION: MAKE SURE THE INBOARD FAN DUCT COWL AND THE THRUST REVERSERS
ARE CLOSED OR REMOVED BEFORE YOU EXTEND THE LEADING EDGE FLAPS.
THERE IS NOT SUFFICIENT CLEARANCE FOR THE FLAPS TO EXTEND IF THE
INBOARD FAN DUCT COWL AND THE THRUST REVERSERS ARE IN THE OPEN
POSITION. THIS CAN CAUSE DAMAGE TO EQUIPMENT.
(a) To extend the flaps and slats with primary control, do this task: Leading Edge Flap and
Slat System Operation With Primary Control, TASK 27-81-00-860-801.
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.
(b) To extend the flaps and slats with alternate control, do this task: Leading Edge Flap and
Slat System Operation With Alternate Control, TASK 27-81-00-860-802.
------------------------- END OF TASK ---------------------------
TASK 27-81-00-860-804
7. Leading Edge Flaps and Slats Retraction
A. General
(1) The leading edge flaps and slats will not retract with alternate control.
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
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-81-00-860-015
(1) To retract the flaps and slats with primary control, do this task: Leading Edge Flap and Slat
System Operation With Primary Control, TASK 27-81-00-860-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
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Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-81-00-480-801
8. Leading Edge Flap and Slat Locks Installation
　
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