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Date/Time Thumbnail Dimensions User Comment; current: 16:18, 7 September 2008: 581 × 581 (85 KB): Dhaluza {{Information |Description={{en|1=Figure 3-10. A true airspeed indicator allows the pilot to correct indicated airspeed for nonstandard temperature and pressure.}} |Source=Instrument Flying Handbook, page 3-7 |Author=U.S. Federal Aviation Adminstration |D
The actual speeds represented by these designators are specific to a particular model of aircraft. They are expressed by the aircraft's indicated airspeed (and not by, for example, the ground speed), so that pilots may use them directly, without having to apply correction factors, as aircraft instruments also show indicated airspeed.
The diagram on the right shows a very simplified plot which shall be used to explain the general shape of the plot. The outer edges of the diagram, the envelope, show the possible conditions that the aircraft can reach in straight and level flight.
V A is the design maneuvering speed and is a calibrated airspeed.Maneuvering speed cannot be slower than and need not be greater than V c. [4]If is chosen by the manufacturer to be exactly the aircraft will stall in a nose-up pitching maneuver before the structure is subjected to its limiting aerodynamic load.
An airspeed indicator for an aeroplane. Indicated airspeed is displayed on the black background (in this case both in knots (kn) and miles per hour (mph)). The pilot sets the pressure altitude and air temperature in the top window using the knob. Based on that, the white background scale in the lower left window moves to give true airspeed.