Engine Failure During Take-Off Ground Roll; After Liftoffand In Flight - Beechcraft C23 SUNDOWNER 180 Pilot Operating Handbook

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Section III
BEECHCRAFT Sundowner
180
Emergency Procedures
C23
(M-1285 and After)
ENGINE FAILURE
DURING
TAKE-OFF
GROUND ROLL
1. Throttle
-
CLOSED
2. Braking
-
MAXIMUM
NOTE
Conduct
the
following
procedures
imme-
diately
if it
appears certain that
the
airplane
will run off
the
runway.
(Otherwise
conduct
these
procedures
at
the
pilot's
discretion.)
3.
Fuel
Selector Valve
-
OFF
4.
Battery Switch,
Alternator
Switch,
and
Fuel
Boost
Switch
-
OFF
5. Magneto/Start
Switch
-
OFF
AFTER LIFTOFF AND
IN FLIGHT
Landing
straight ahead is
usually
advisable. // sufficient
altitude
is available
for maneuvering,
accomplish
the
following:
1. Mixture
-
FULL
RICH, then LEAN as
required
2.
Fuel
Boost
Pump
-
ON
3.
Fuel
Selector Valve
-
SELECT OTHER
TANK (Check to
feel detent
and check visually)
4.
Magnetos
-
CHECK LEFT and RIGHT,
then
BOTH
NOTE
The
most
probable
cause
of engine
failure
would
be
loss
of fuel flow or
improper
functioning
of the
ignition
system.
3-4
Revised: April 1979

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