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SLIDE SHOW COMPONENT

  • SLIDE SHOW COMPONENT
    Photography of a fly-off between a Beechcraft A-36 and a Cessna 210 owned by the San Diego Flight Corporation. Jacqueline Cochran Regional Airport (TRM) Thermal CA USA

Overview

  • The Cessna 210 is an all metal, six place, high wing, single engine airplane equipped with retractable tricycle landing gear and is designed for general utility purposes. Over many models, each with continued improvements, the 210 became a high-performance load hauler with reasonable speeds for its 260-hp Continental IO-470-S engine. The latest model 210R’s—available in 310-hp nonturbo, 325-hp turbocharged, and 325-hp pressurized iterations—are rare but highly desirable. Factory and aftermarket support remains strong for the later airplanes, so owning one can be feasible despite the admittedly-complex maintenance.

     

    https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-210

     

Specifications

  • Powerplant

    Continental IO-470-S (260 hp)

  • Propellers

  • Length

    27' 9"

  • Height

    9’ 9”

  • Wingspan

    36’ 7”

  • Wing Area

    176 sq ft

  • Wing loading

    17.1 lb

  • Power loading

    11.5 lb

  • Cabin Width

    44"

  • Empty Weight

    1,780 lb

  • Maximum gross weight

    3,000 lb

  • Useful load

  • Payload with full fuel

  • Fuel capacity

    65 gal

  • Baggage capacity

    120 lb

Performance

  • Takeoff distance ground roll

    695 ft

  • Takeoff distance over 50-ft obstacle

    1,210 ft

  • Rate of climb sea level

    1,270 fpm

  • Service ceiling

    20,300 ft

  • Landing distance over 50-ft obstacle

    1,110 ft

  • Landing distance ground roll

    485 ft

  • Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption, ea engine) @ 75% power, best economy

    5 hours

  • Range

    680 nm

Limiting and Recommended Airspeeds

  • VX

    100 KIAS

  • VY

    1270 fpm

  • VNE

    225 mph

  • VS1

    52 KIAS

  • VSO

    60 mph

All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.