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Maneuvering speed : ウィキペディア英語版 | Maneuvering speed In aviation, the maneuvering speed of an aircraft is an airspeed limitation selected by the designer of the aircraft. At speeds close to, and faster than, the maneuvering speed, full deflection of any flight control surface should not be attempted because of the risk of damage to the aircraft structure.〔Federal Aviation Administration, (Advisory Circular 23-19A, ''Airframe Guide for Certification of Part 23 Airplanes'', Section 48 (p.27) ) Retrieved 2012-01-06〕 The maneuvering speed of an aircraft is shown on a cockpit placard and in the aircraft's flight manual but is not commonly shown on the aircraft's airspeed indicator. In the context of air combat manoeuvring (ACM), the maneuvering speed is also known as corner speed or cornering speed.〔(CNATRA P-821 (Rev. 01-08) "Flight Training Instruction, Advanced Naval Flight Officer (T-45C)". ) ''Department of the Navy'', 2008.〕 ==Implications==
It has been widely misunderstood that flight below maneuvering speed will provide total protection from structural failure. In response to the destruction of American Airlines Flight 587, a CFR Final Rule was issued clarifying that "flying at or below the design maneuvering speed does not allow a pilot to make multiple large control inputs in one airplane axis or single full control inputs in more than one airplane axis at a time". Such actions "may result in structural failures at any speed, including below the maneuvering speed."〔Federal Aviation Administration, (14CFR §25.1583 Final Rule ) Retrieved 2012-01-06〕
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