Warning Horn; Brakes; April 1982 - Beechcraft Debonair 35-33 Pilot Operating Handbook

SectionVll
BEECHCRAFT
Debonair33
Systems Description
WARNING HORN
With the landi ng gear retracted, if the throttle is retarded
below approximately 12 in. Hg manifold pressure, a
warning horn will sound intermittently.
BRAKES
The brakes on the main landing gear wheels are operated
by applying toe pressure to the rudder pedals.
CAUTION
Continuous brake application of either the
pilot's or copilot's brake pedals in conjunction
with an overriding pumping action from the op-
posite brake pedals could result in the loss of
braking action on the side which continuous
pressure is being applied .
The parking brake push-pull control is located on the right
subpanel. To set the parking brakes, pull control out and
depress both toe pedals until firm. Push the control in to
release the brakes.
7-14
CAUTION
The parking brake should be left oft and wheel
chocks installed if the airplane is tobe left un-
attended. Changes in ambient temperature can
cause the brake to release or 'to exert ex-
cessive pressures.
April 1982