Originally Posted by
AirRabbit
First, V1 is the maximum speed at which the rejected takeoff maneuver can be initiated and the airplane stopped within the remaining field length under the conditions and procedures defined in the FAR’s. It is the latest point in the takeoff roll where a stop can be initiated.
For an engine failure scenario, only if at field limited weight and no remaining reverse is used(on a dry runway, wouldn't you say.