Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 41
Single Engine Rate of Climb
Single Engine Climb Gradient
Conditions:
Climb on single engine
Airspeed at Vyse
Propeller on failed engine feathered
Approximately 5 degrees bank toward operating engine
Note:
This chart is based on page 6-9 of the Beechcraft Travelair D95A Owners Manual
All IFR departure procedures require a minimum of 200 ft/Nm climb gradient. Some procedures require
more than 200 ft/Nm. Transport Canada regulations do NOT require single engine climb gradients for legal
IFR departures but the lack of such climb gradients should cause pilots to prepare alternate plans of action
in the event of an engine failure below MEA.
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