Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 40
Accelerate Stop dist. – B95
Conditions:
Normal takeoff procedure and conditions.
Gear extended throughout takeoff and landing
Immediate reduction in power and landing following
engine failure at 89 KIAS.
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 an estimate based on the assumption that the airplane is at 35’agl at
89KIAS, a 3 second reaction time is assumed with no change in altitude. The stopping distance is then based
on the normal landing distance chart from 35 feet. Data was taken from pages 6-2, 6-3, 6-20 and 6-21 of the
Beechcraft Travelair D95A Owners Manual.
Vr, all weights – 74 KIAS
Vgo, all weights – 89 KIAS
Chart gives estimated distance to
89KIAS at 35 feet agl then land
and stop.
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