Aircraft instruments and avionics pdf
Aircraft Instruments, Engines and Systems - WikiversityBohemia, New York nician training program. The descriptions, drawings Flight Dynamics Inc. Portland, Oregon and graphics in this book are for instructional pur- Piper Aircraft Corp. Excerpts from Federal Aviation Regula- Inc. Longueuil, Quebec, Canada tions and other sources have been paraphrased and The Canadair drawings which appear throughout simplified in order to save space and time.
Aircraft Instruments and Avionics.pdf
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There are two parts to any instrument system—the sensing mechanism and the display mechanism. Information is relayed from the sensors to the indicators via electricity, or direct pressure sensing via pneumatic or oil-filler tubes. There are also miscellaneous gauges and indicators that provide information that do not fall into these classifications, especially on large or complex aircraft. The most common arrangement is referred to as a T arrangement, with Airspeed, Artificial Horizon, and Altimeter across the top and heading indicator at the bottom. The other two instruments are the turn coordinator and vertical speed indicator.
A pitot-static system is a system of pressure-sensitive instruments that is most often used in aviation to determine an aircraft's airspeed , Mach number , altitude , and altitude trend. A pitot-static system generally consists of a pitot tube , a static port, and the pitot-static instruments. Errors in pitot-static system readings can be extremely dangerous as the information obtained from the pitot static system, such as altitude, is potentially safety-critical. Several commercial airline disasters have been traced to a failure of the pitot-static system. The pitot-static system of instruments uses the principle of air pressure gradient. It works by measuring pressures or pressure differences and using these values to assess the speed and altitude. The static pressure is used in all measurements, while the pitot pressure is used only to determine airspeed.