Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 37
Normal takeoff distance – B95
Conditions:
Full power. Mixture leaned to appropriate fuel flow
Zero Flaps
Paved level dry runway
Retract gear at positive rate of climb
Cowl flaps open
Example:
Density altitude = 5000 ft.
Weight = 3500 lb.
Headwind = 20 Knots
Results:
Ground roll = 1700
Distance to 50 feet = 2110
NOTES: Produced by Selkirk College based on approved POH.
For use by Selkirk College Professional Aviation students and instructors only.
Distances calculated with this chart are based on pages 6-2 and 6-3 of the Beechcraft Travelair D95A Owners
Manual.
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