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Beechcraft Duchess 76 - Page 183

Beechcraft Duchess 76
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BEECHCRAFT
Duchess 76
section
VII
Systems Description
WARNING HORN SILENCE
BUDON
An optional gear warning horn silence button allows
the
pilot
to
manually silence the warning horn with either
throttle retarded, the landing gear retracted, and the flaps
retracted above approximately 16°. The push-to-silence
button is located next to the landing gear control switch
and is placarded
"GEAR
HORN SILENCE". A red light
in
the button illuminates when the gear horn silence system
is
activated.
When either throttle is retarded sufficiently to activate the
gear
warning horn, the horn may be silenced with the
button.
If
the other throttle is then retarded, the warning
hom
will again sound and cannot be silenced. After a
single throttle has
been
retarded and the resulting warning
horn silenced with the button, readvancing the throttle
resets the warning
horn
and it will again sound when either
throttle
is
retarded.
The
warning horn is also reset when
the landing gear are lowered. When the flaps are extended
beyond approximately 16°, the button will not silence
the
warning horn.
CIRCUIT BREAKER
The
landing GEAR
MOTOR
circuit breaker and the landing
GEAR CONTROL circuit breaker are located on the right
subpanel. The circuit breakers are the pull-and-reset type
and will pop out under overload conditions.
EMERGENCY EXTENSION
The
landing gear can
be
manually extended by turning the
hydraulic pressure
bypass
valve 90° counterclockwise. The
valve is located under
the
access door on the floor in front
of
the pilot's seat. When
the
system pressure is released, the
gear will fall into the down-and-\ocked position.
The
emer-
gency extension procedure is outlined in the EMERGENCY
PROCEDURES section.
August,
1980
7-12A

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