Difference between revisions 1205724 and 1205923 on sqwiki

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{|{{Infobox Aircraft Begin
  |name = Model 210 Centurion
  |image = Image:cessna.210.centurion.d-ebws.arp.jpg
  |caption = A Cessna 210 Centurion
}}{{Infobox Aircraft Type
  |type = light aircraft
  |national origin=[[United States]]
(contracted; show full)xtended outboard, from Wing Station 100 to Wing Station 122, which allowed a lower landing speed (FAA certification regulations state that a single-engine aircraft must have a flaps-down, power-off stall speed no greater than 70 miles/hour).  To compensate for the reduced aileron span, the aileron profile was changed and its chord enlarged.  The 1964 model 210D introduced a {{convert|285|hp|abbr=on}} engine and 2 small child seats, set into the cavity which contained the mainwheels aft of the passengers.


InNe 1967 the modeli 210G introduced afuti nje krah [[cantilever#In aircraft|cantilever]] wingduke replacing the strut-braced wing.  Its planform changed to a constant taper from root chord to tip chord.  In 1970 the 210K became the first full 6-seat model. This was achieved by replacing the flat leaf-springs used for the retractable main landing gear struts (undercarriage) with tapered tubular steel struts of greater length. This allowed the tires to be nested farther to the rear of the fuselage, making room for the full size rear seats.  In 1979 the 210N model eliminated the folding doors which previously covered the two retracted main wheels. The tubular spring struts retract into shallow channels along the bottom of the fuselage and the wheels fit snugly in closed depressions on the underside of the fuselage.  Some models featured de-icing boots as an option.

The aircraftAvioni was offered in a normally aspirated version, designated the model  '''210''', as well as the [[turbocharged]] '''T210''' and the [[cabin pressurization|pressurized]] '''P210''' versions. The '''Centurion II''' was an option introduced in 1970 with improved avionics, and was available in both noramlly aspirated and turbocharged versions ('''Turbo Centurion II''')<ref name="Janes 82 p345-6"/>

OnNe 21 Maymaj 2012 the airworthiness authority responsible for the design, the US [[Federal Aviation Administration]], issued an emergency [[Airworthiness Directive]] requiring 3,665 of the cantilever wing Cessna 210s to be inspected for cracks in the spar cap, wing spar and wing. Aircraft with more than 10,000 hours of airframe time were grounded immediately pending a visual inspection.<ref name="Grady21May12">{{cite news|url = http://www.avweb.com/avwebflash/news/FAAIssuesEmergencyADForCessna210s_20672(contracted; show full)[[en:Cessna 210]]
[[es:Cessna 210]]
[[fr:Cessna 210]]
[[no:Cessna 210 Centurion]]
[[pl:Cessna 210]]
[[pt:Cessna 210]]
[[ru:Cessna 210]]
[[sv:Cessna 210 Centurion]]