Short-Field Takeoff, No Obstacle (25° Flaps) Short-Field Takeoff, Obstacle Clearance (25° Flaps) Operational Speeds Operation Normal Takeoff (0° Flaps) Do not exceed this speed under any circumstances. Range of speed at which the aircraft should be operated only in smooth air, and then only with caution. Range of speed at which the aircraft is normally operated.
What Is It? Range of speed at which flaps may be fully extended.
CESSNA 172P V SPEEDS KNOTS FULL
Maximum crosswind component during which the aircraft has been landed by the manufacturer test pilot.Īirspeed Indicator Markings Range Full Flap Operating Maximum speed at which to close a door in flight should it inadvertently open. Maximum speed at which to perform the emergency landing gear extension procedure. Maximum speed at which the landing gear may be raised. Maximum speed at which the landing gear may be in the extended position. Maximum speed at which the landing gear may be lowered. Do not exceed this speed except in smooth air. Reduce speed to this value when in rough air. Maximum speed at which full, abrupt deflection of the controls can be made without causing structural damage. Maximum speed at which flaps may be fully extended. In a glide it provides the maximum distance traveled forward with the minimum altitude lost. In a climb it provides increased forward visibility and engine cooling. In a climb it provides the maximum gain in altitude per unit of time traveled. In a climb it provides the maximum gain in altitude for the distance traveled forward. The speed at which the nosewheel is lifted from the runway during takeoff. Stall speed or minimum steady flight speed in the clean configuration (flaps fully retracted). What Is It? Stall speed or minimum steady flight speed in the landing configuration (flaps fully extended). PA-28R-201 ARROW III SPEEDS NOTE: All airspeeds shown are expressed in Knots Indicated Airspeed (KIAS) and are based on the aircraft at maximum gross weight unless otherwise noted.ħ0 KIAS, 0° Flaps 60 KIAS, 25° Flaps 72 KIAS, G.
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