Download Ace the Technical Pilot Interview by Gary Bristow PDF

By Gary Bristow

* A entire research advisor supplying pilots the solutions they should excel on their technical interview
* beneficial properties approximately a thousand capability questions (and solutions) that could be requested through the technical interview for pilot positions
* extensive scope--ranges from gentle plane via heavy jet operations
* Culled from interviewing practices of best airways around the world
* contains interviewing suggestions and strategies

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Extra info for Ace the Technical Pilot Interview

Sample text

Speed instability is the second consequence of poor lift at lower speeds for the swept-wing aircraft. Speed is unstable below minimum drag speed (VIMD) because the aircraft is now sliding up the back end of the jet drag curve, where power required increases with reducing speed. This means that despite the higher coefficient of lift (C L ) associated with lower speeds, the drag penalty increases faster than the lift; therefore, the lift-drag ratio degrades, and the net result is a tendency to progressively lose speed.

Stall warner's and stick pushers. Stall warners are either an artificial audio warning and/or a stick shaker, which usually are activated at or just before the onset of the prestall buffet. Stick pushers are normally used only on aircraft with superstall qualities and usually activate after the stall warning but before the stall, giving an automatic nose-down command. Both systems normally receive a signal from an incidence-measuring probe. Instability What is Dutch roll? Dutch roll is an oscillatory instability associated with swept-wing jet aircraft.

Stalling speed is increased. 3. Maneuverability is reduced. 4. Wear on tires and brakes is increased. 5. Structural safety margins are reduced. Describe center of gravity. The center of gravity (C ofG, CG) is the point through which the total weight of a body will act. Describe a component arm. The definition of a component arm is the distance from the datum to the point at which the weight of a component acts (center of gravity point). By convention, an arm aft of the datum, which gives a nose-up moment, is positive, and an arm forward of the datum, which gives a nose-down moment, is negative.

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