Beechcraft Baron 58 - Page 136

Section V
Performance
BEECHCRAFTBaron58
SerialTH
773 and After
Enter the Accelerate-Stop graph at 15°C, 5650 feet pres-
sure altitude,
5400 pounds, and 9.5 knots headwind
component:
Accelerate-Stop Distance
3960 ft
Engine Failure Speed
86 kts
NOTE
Since
3960 feet is less than the available field
length (10,010 ft), the accelerate-stop pro-
cedure can be performed at any weight.
Take-off at 5400lbs can be accomplished. How-
ever, if an engine failure occurs before be-
coming airborne, the accelerate-stop pro-
cedure
must be performed.
The
following example assumes the airplane is loaded so
that the take-off weight is 4850 pounds.
Although not required by regulations, information has been
presented to
determine the take-off weight, field require-
ments and take-off flight path assuming an engine failure
occurs during the take-off procedure. The following
illustrates the use of these charts.
Enter the Accelerate-Go graph at 15°C,
5650 feet pressure
altitude,
4850 pounds, and 9.5 knots headwind component:
Ground Roll 1775 ft
Total Distance Over 50 ft Obstacle 8071 ft
Lift-off Speed 86 kts
50 Foot Speed
94 kts
5-6 October 1976