Get Airplane Flying Handbook: FAA-H-8083-3A PDF

By Federal Aviation Administration

ISBN-10: 156027557X

ISBN-13: 9781560275572

The basic abilities and crucial info precious for piloting airplanes are brought during this starting aviator's consultant. Pilots wishing to enhance their flying talent and aeronautical wisdom, flyers getting ready for extra certificate or scores, and flight teachers engaged within the guideline of either scholars and certified pilots will enjoy the info during this pilot source. The legitimate FAA reference for the aviator-in-training, many attempt questions for the FAA wisdom assessments for pilots come without delay from this advisor.

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Extra resources for Airplane Flying Handbook: FAA-H-8083-3A

Sample text

This leads to a cardinal rule of airplane flying that a student pilot must understand and appreciate: The pilot must never attempt to “stretch” a glide by applying back-elevator pressure and reducing the airspeed below the airplane’s recommended best glide speed. Attempts to stretch a glide will invariably result in an increase in the rate and angle of descent and may precipitate an inadvertent stall. When the approximate gliding pitch attitude is established, the airspeed indicator should be checked.

Trim is also a very important consideration during a climb. After the climb has been established, the airplane should be trimmed to relieve all pressures from the flight controls. If changes are made in the pitch attitude, power, or airspeed, the airplane should be retrimmed in order to relieve control pressures. 3-14 To enter the climb, simultaneously advance the throttle and apply back-elevator pressure to raise the nose of the airplane to the proper position in relation to the horizon. As power is increased, the airplane’s nose will rise due to increased download on the stabilizer.

Best rate of climb. qxd 7/13/04 11:08 AM Page 3-14 Absolute Ceiling When performing a climb, the power should be advanced to the climb power recommended by the manufacturer. If the airplane is equipped with a controllable-pitch propeller, it will have not only an engine tachometer, but also a manifold pressure gauge. Normally, the flaps and landing gear (if retractable) should be in the retracted position to reduce drag. Service Ceiling As the airplane gains altitude during a climb, the manifold pressure gauge (if equipped) will indicate a loss in manifold pressure (power).

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Airplane Flying Handbook: FAA-H-8083-3A by Federal Aviation Administration

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