Flap range decreased to 30 degrees, fuel capacity increased from 65 to 90 USgal (246 to 341 l). Useful Load (Carrying Capacity) of a Cessna Turbo 210 Centurion. Horsepower: 285 Gross Weight: 3300 lbs Top Speed: 172 kts Empty Weight: 1865 lbs Cruise Speed: 165 kts Fuel Capacity: 65.00 gal Stall Speed (dirty): 54 kts Range: 640 nm Takeoff: Landing: Ground Roll: 675 ft Ground Roll 735 ft: Over 50 ft obstacle: 1265 ft Over 50 … The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear, single engine, high-wing general aviation aircraft which was first flown in January 1957 and produced by Cessna until 1985. Fuel capacity: 65 GAL. CESSNA 210E Centurion (1965 - 1965) Typical Price: $78,680.00 ... 2009 CESSNA AIRCRAFT CO LC41-550FG. Looking for an aircraft fuel tank repair, a helicopter fuel cell to buy, or have a rotorcraft fuel cell that needs repairing, or maybe you need to purchase a Cessna, Beech or Piper fuel bladder? Wilmington, DE. Ownership costs 1961 Typical Price: $28,110.00 Total Cost of Ownership: $17,006.23 ... Find and Compare CESSNA 210 for sale Also Consider. A significant development of the T210 was the high performance, pressurised P210 which first appeared in 1978. Cessna 210H Centurion / Turbo Centurion A 210G with a new flap system and instrument panel, 210 built. The Cessna Turbo 210 Centurion has an average empty weight of 2,180 pounds and a gross weight of 3,800 pounds, meaning its effective useful load is around 1,620 pounds. Continual development of the 210 and T210 range continued through until production ceased in 1985. Horsepower: 285 Gross Weight: 3800 lbs Top Speed: 205 kts Empty Weight: 2180 lbs Cruise Speed: 187 kts Fuel Capacity: 90 gal Stall Speed (dirty): 57 kts Range: 732 nm Takeoff: Landing: Ground Roll: 1170 ft Ground Roll 765 ft: Over 50 ft obstacle: 2030 ft Over 50 ft … Call us at 1-800-647-6148. Introduced in 1968. The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear, single-engine high-wing general aviation aircraft produced from 1957 to 1986. The Cessna 210L has a “steering lag” while taxiing; only steady, smooth pedal inputs will result in a controlled turn. Horsepower: 285 Gross Weight: 3400 lbs Top Speed: 174 kts Empty Weight: 1960 lbs Cruise Speed: 167 kts Fuel Capacity: 90 gal Stall Speed (dirty): 55 kts Range: 760 nm Takeoff: Landing: Ground Roll: 800 ft Ground Roll 625 ft: Over 50 ft obstacle: 1365 ft Over 50 ft obstacle: 1355 ft … 1979 Cessna 210N Specifications The C-210 was one of the highest performance single engine piston engine aircraft of its time and still remains one of the top performers. The 210G introduced a new strutless cantilever wing, increased fuel capacity, restyled rear windows and enlarged tail surfaces. Thus, it takes patience and anticipation to taxi a 210 correctly. The bigger turbo was needed to provide enough bleed air to pump up the cabin while not restricting the airplane’s climb or cruise performance. Pedal inputs must be applied early and held for a relatively long time to cause a change in direction while rolling on the ground. FFC constructions meet the Technical Standard TSO-C80. Cessna’s project engineer on the P-210 program, Phillip Hedrick, had his work cut out for him in attempting to sandwich a larger capacity turbo under the bonnet of the 210. With cruise speeds of 160 KTS and a useful load of 1,462 lbs, this is one of the ultimate cross country aircraft ever built. Cessna 210J Centurion / Turbo Centurion Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. The aircraft was a remarkably high-performing load-hauler with its ability to carry serious loads at reasonable speeds and for its ability to fly almost five hours with its 90 gallons of fuel. 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