BEECHCRAFT
SectlonX
Safety Information
in the shortest possible time, and is based on the
following criteria:
- critical engine inoperative, and its propeller
in
the minimum drag position.
- operating engine set
at
not more than maximum
continuous
power.
- landing gear retracted.
- wing flaps in the
most favorable (i.e., best
lift/drag ratio position).
-
cowl flaps
as
required for engine cooling.
- aircraft
flown at recommended bank angle.
Drag caused by a windmilling propeller, extending
landing gear,
or
flaps
in
the landing position, will
severely
degrade
or
destroy single engine climb
performance. Since engine climb performance varies
widely with type
of
airplane, weight, temperature,
altitude,
and
airplane
configuration,
the
climb
gradient (altitude gain
or
loss per mile) may be
marginal
-
or
even negative - under some_conditions.
Study
the
Information Manual for your specific
airplane and know what performance to expect with
one-engine out.
BEST
SINGLE
ENG/NE
ANGLE-OF-CLIMB
AIRSPEED (Vxse)
Vxse is used only
lo
clear obstructions during initial
March,
1981
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