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SUBTASK 27-51-00-860-004
WARNING: KEEP PERSONS AND EQUIPMENT 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 INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT.
(2) Supply system B hydraulic power, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-51-00-860-005
WARNING: MOVE ALL PERSONS AND EQUIPMENT AWAY FROM THE TRAILING EDGE FLAPS,
AND THE LEADING EDGE FLAPS AND SLATS. THESE SURFACES WILL MOVE AND
CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(3) Move the flap control lever to the applicable detent position.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-00-860-006
(1) Move the flap control lever to the UP position to retract the flaps and slats.
SUBTASK 27-51-00-860-007
(2) Remove system B hydraulic power, do this task: Hydraulic System A or B Power Removal,
TASK 29-11-00-860-805.
------------------------- END OF TASK ---------------------------
TASK 27-51-00-860-802
5. Trailing Edge Flap System Operation With Alternate Control
(Figure 201)
A. General
(1) The alternate control system uses electrical power to move the flaps.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Procedure
SUBTASK 27-51-00-860-008
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-00-860-009
WARNING: MOVE ALL PERSONS AND EQUIPMENT AWAY FROM THE TRAILING EDGE FLAPS,
AND THE LEADING EDGE FLAPS AND SLATS. 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 arm the alternate control system.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-51-00-860-010
(3) Move the flap control lever to the 40-unit position.
NOTE: This will decrease the load on the flap electric motor. You can move the lever past
where you will move the flaps to.
SUBTASK 27-51-00-860-011
CAUTION: WAIT A MINIMUM OF 15 SECONDS AFTER THE FLAPS STOP BEFORE YOU USE THE
ALTERNATE SYSTEM TO MOVE THE FLAPS AGAIN. YOU CAN CAUSE DAMAGE TO
THE FLAP ALTERNATE MOTOR.
(4) Move the ALTERNATE FLAPS control switch to UP or DOWN to extend or retract the flaps as it is
necessary.
NOTE: The leading edge flaps and slats will not retract with alternate control.
SUBTASK 27-51-00-860-012
(5) Move the ALTERNATE FLAPS control switch to the OFF position.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-00-860-013
WARNING: MAKE SURE THE POSITION OF THE FLAPS AGREES WITH THE POSITION OF THE
FLAP CONTROL LEVER. WHEN YOU SUPPLY HYDRAULIC POWER, 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 are in the same position as the flap
control lever or move the flap control lever to the position of the flaps.
SUBTASK 27-51-00-860-014
(2) Move the ALTERNATE FLAPS control switch to the OFF position.
SUBTASK 27-51-00-860-015
(3) Move the ALTERNATE FLAPS ARM switch to the OFF position to disarm the alternate control
system.
------------------------- END OF TASK ---------------------------
TASK 27-51-00-980-801
6. Trailing Edge Flap System Manual Operation
(Figure 203)
A. General
(1) Use this task to manually operate the trailing edge flap system without airplane power.
B. References
Reference Title
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
C. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00467 Fluid - Landing Gear Shock Strut BMS3-32, Type
II
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
4 Cover 27-51-55-02-110 GUN 001-028, 101-121,
155-157, 201-999
　
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