Hint | Answer | % Correct |
---|---|---|
Minimum speed in the takeoff, following a failure of the critical engine at VEF, at which the pilot can continue the takeoff and achieve the required height above the takeoff surface within the takeoff distance. | V1 | 91%
|
The maximum speed in the takeoff at which the pilot must take the first action to stop the airplane within the accelerate-stop distance. | V1 | 91%
|
Rotation speed | VR | 88%
|
Takeoff safety speed | V2 | 82%
|
Speed for best rate of climb | VY | 56%
|
Design cruising speed | VC | 53%
|
Speed for best angle of climb | VX | 53%
|
Design maneuvering speed | VA | 50%
|
Design flap speed | VF | 50%
|
Never-exceed speed | VNE | 50%
|
Reference landing speed | VREF | 41%
|
Design speed for maximum gust intensity | VB | 32%
|
Maximum structural cruising speed | VNO | 32%
|
Design diving speed | VD | 29%
|
Maximum flap extended speed | VFE | 24%
|
Maximum speed in level flight with maximum continuous power | VH | 24%
|
Maximum landing gear operating speed | VLO | 24%
|
The stalling speed or the minimum steady flight speed obtained in a specific configuration | VS1 | 24%
|
Maximum landing gear extended speed | VLE | 18%
|
Stalling speed or the minimum steady flight speed in the landing configuration | VS0 | 18%
|
Minimum control speed with the critical engine inoperative | VMC | 15%
|
Speed at which the critical engine is assumed to fail during takeoff | VEF | 12%
|
Maximum operating limit speed | VMO/MMO | 12%
|
Reference stall speed | VSR | 9%
|
Lift-off speed | VLOF | 6%
|
Takeoff safety speed for a Category A rotorcraft | VTOSS | 6%
|
Minimum unstick speed | VMU | 3%
|
Minimum takeoff safety speed | V2MIN | 0%
|
Demonstrated flight diving speed | VDF/MDF | 0%
|
Maximum speed for stability characteristics | VFC/MFC | 0%
|
Final takeoff speed | VFTO | 0%
|
Reference stall speed in a specific configuration | VSR1 | 0%
|
Speed at which onset of natural or artificial stall warning occurs | VSW | 0%
|
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