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| 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.<ref name=AC23-19A>[[Federal Aviation Administration]], [http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/d1a4060f22939f36862572eb0061ca3f/$FILE/AC%2023-19A.pdf Advisory Circular 23-19A, ''Airframe Guide for Certification of Part 23 Airplanes'', Section 48 (p.27)] Retrieved 2012-01-06</ref>
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| It has been widely misunderstood that flight below maneuvering speed will provide total protection from [[structural failure]]. See [[American Airlines Flight 587]]. Due to this accident a CFR Final Rule was issued effective October 15, 2010 clarifying this misconception.<ref name=faa>Federal Aviation Administration, [http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgFinalRule.nsf/0/395c3f064247018a862577b200495b5a!OpenDocument 14CFR §25.1583 Final Rule] Retrieved 2012-01-06</ref>
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| 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]].
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| In the context of [[air combat manoeuvring]] (ACM), the maneuvering speed is also known as '''corner speed''' or '''cornering speed'''.<ref>[https://www.cnatra.navy.mil/pubs/folder5/NFO_SNFO/P-821(2).PDF CNATRA P-821 (Rev. 01-08) "Flight Training Instruction, Advanced Naval Flight Officer (T-45C)".] ''Department of the Navy'', 2008.</ref>
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| ==Design maneuvering speed V<sub>A</sub>==
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| V<sub>A</sub> is the design maneuvering speed and is a [[calibrated airspeed]]. Maneuvering speed cannot be slower than <math>V_s \sqrt{n}</math> and need not be greater than V<sub>c</sub>.<ref>[http://www.ecfr.gov/cgi-bin/retrieveECFR?gp=1&SID=0eb6ca22ab5efa94f23f757d30af7726&h=L&n=14y1.0.1.3.10&r=PART&ty=HTML#14:1.0.1.3.10.3.70.9 14 CFR §23.335(c)(2)] Definition of Maneuvering Speed</ref>
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| ==Maximum operating maneuvering speed V<sub>O</sub>==
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| Some aircraft have a maximum operating maneuvering speed V<sub>O</sub>. The concept of maximum operating maneuvering speed was introduced to the USA [[Type certificate|type-certification]] standards for light aircraft in 1993.<ref name=AC23-19A/><ref>[http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf/0/2A0AA756267EFE8F85256687007232CC?OpenDocument USA 14CFR §23.1557] Retrieved 2012-01-06</ref> The maximum operating maneuvering speed is selected by the aircraft designer and cannot be faster than <math>V_s \sqrt{n}</math>, where V<sub>s</sub> is the [[Stall (flight)|stalling]] speed of the aircraft, and ''n'' is the maximal allowed positive [[load factor (aeronautics)|load factor]].
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| At airspeeds slower than <math>V_s \sqrt{n}</math> the aircraft will stall before the structure is subjected to its limiting aerodynamic load. The maneuvering speed or maximum operating maneuvering speed depicted on a cockpit placard is calculated for the maximum weight of the aircraft. Some [[Pilot's Operating Handbook]]s also present safe speeds for weights less than the maximum.
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| The formula used to calculate a safe speed for a lower weight is <math>\scriptstyle V_A \sqrt{W_2 \over W_1}</math>, where V<sub>A</sub></sub> is maneuvering speed (at maximum weight), W<sub>2</sub> is actual weight, W<sub>1</sub> is maximum weight.<ref>{{Cite book | title=Jeppesen Instrument/Commercial Manual |year=2000 |ISBN=0-88487-274-2}}</ref>
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| == See also ==
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| * [[V speeds]]
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| == References ==
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| {{Reflist}}
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| == External links ==
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| * {{CodeFedReg|14|23|335}} "Design airspeeds"
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| {{DEFAULTSORT:Maneuvering Speed}}
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| [[Category:Airspeed]]
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| [[Category:Aerodynamics]]
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