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BEECHCRAFT
Debonair33
SectionVll
Systems Description
Switches on
the
right
and left subpanels operate landing
gear, flaps,
exterior
lighting,
and
radios. Attached to the
lower
center section
of the
subpanel
are the powerplant
controls
and interior
li~hti
ng rheostats. Flap indicator
lights
are to
the left of the control column and landing gear
indicator lights to the
right.
GROUND CONTROL
Steering is accomplished by use of the
rudder
pedals
through
a
linkage arrangement which connects the nose
strut
to
the rudder
pedal shaft. Nose wheel straightening is
accomplished by engagement
of
a roller with
a
track as
the
nose wheel is retracted. The steering link attaches to the
steering mechanism
on the
nose strut
with a swivel
connect ion which
permits the
mechanism to disengage
when the nose gear is retracted
and
operation of the
rudder
pedals will have no tendency to turn the
nose
wheel with the gear retracted
.
The minimum wing
tip turning radius,
using full
steering,
one brake and partial power, is 26
feet
4
inches.
WING FLAPS
The wing flaps are
controlled
by
a three-position
switch,
UP, OFF and DOWN, located on the
subpanel
to the
left
of
the
center
console.
The control must be pulled out
of
detent before it can be repositioned.
The flap position lights on the left side of the control
~
console show green for the up position and red for the full-
down landing position- intermediate 20-degree and
10-
degree positions are indicated by lines painted on the
April 1982
7-11
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