Landing Gear System; Control Switch - Beechcraft Debonair 35-33 Pilot Operating Handbook

Section Vll
Systems Description
BEECHCRAFT
Debonair33
leading edge of the left flap. The intermediate positions are
reach ed when the marks are aligned with the trailing edge
of the wing.
Limit switches automatically turn off the electric motor
when the flaps reach the extremes of travel. lntermediate
flap positions can be obtained by placing the switch in the
~
OFF position as the flaps reach the desired position du ring
flap extension or retraction.
LANDING GEAR SYSTEM
~
CAUTION
Never taxi with a flat strut.
The landing gears are operated through adjustable linkage
connected to an actuator assembly mounted beneath the
front seats. The actuator assembly is driven by an electric
motor. The landi ng gears may be electrically retracted and
extended, and in an emergency may be extended
manually.
CONTROL SWITCH
The landing gear is controlled by a two-position switch on
the right side of the subpanel. The switch handle must be
pulled out of the safety detent before it can be moved to the
opposite position.
7-12
CAUT/ON
Do not change the position of the control
switch to reverse the direction of the landing
gear while the gear is in transit, as this could
cause damage to the retract mechanism.
April 1982