BEECHCRAFT Bonanza Section VII
V35, V35A & V35B thru D-9947 Systems Description
WARNING HORN
With the landing 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 sub-
panel (right subpanel - V35, V35A; left subpanel - V358).
To set the parking brakes, pull control out and depress both
toe pedals until firm. Push the control in to release the
brakes.
CAUTION
The parking brake should be left off and wheel
chocks installed if the airplane is to be left un-
attended. Changes in ambient temperature can
cause the brakes to release or to exert ex-
cessive pressures.
MANUAL EXTENSION
The landing gear can be manually extended by operating a
handcrank at the rear of the front seats. This procedure is
described in the EMERGENCY PROCEDURES section.
January 1982
7-19
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