V1: engine failure recognition speed
- abort the take-off and bring the aircraft to a stop on the runway plus stopway OR
- continue and be at V2 at 35 feet above the departure end of the runway
- increases with weight
V2: take-off safety speed
- a referenced airspeed obtained after the aircraft lifts off and at which the required OEI climb performance can be achieved
Vmca: aim minimum control speed
- lowest calibrated airspeed at which control of an aircraft can be maintained following the failure of the critical engine with the remaining engine(s) operating at take-off power
- determined at gross weight with the C of G at the aft limit, flaps in take-off position, landing gear retracted, and the propeller windmilling if no autofeathering system is installed
Va: maneuvering speed
- maximum speed at which full deflection of the primary flight controls will not cause overstressing of the aircraft
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