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 … Continual development of the 210 and T210 range continued through until production ceased in 1985. Wilmington, DE. Pedal inputs must be applied early and held for a relatively long time to cause a change in direction while rolling on the ground. Useful Load (Carrying Capacity) of a Cessna Turbo 210 Centurion. 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. Fuel capacity: 65 GAL. Cessna 210H Centurion / Turbo Centurion A 210G with a new flap system and instrument panel, 210 built. FFC constructions meet the Technical Standard TSO-C80. 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. Ownership costs 1961 Typical Price: $28,110.00 Total Cost of Ownership: $17,006.23 ... Find and Compare CESSNA 210 for sale Also Consider. Cessna 210J Centurion / Turbo Centurion Flap range decreased to 30 degrees, fuel capacity increased from 65 to 90 USgal (246 to 341 l). 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. The 210G introduced a new strutless cantilever wing, increased fuel capacity, restyled rear windows and enlarged tail surfaces. 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. The Cessna 210L has a “steering lag” while taxiing; only steady, smooth pedal inputs will result in a controlled turn. Call us at 1-800-647-6148. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. Introduced in 1968. A significant development of the T210 was the high performance, pressurised P210 which first appeared in 1978. The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear, single-engine high-wing general aviation aircraft produced from 1957 to 1986. 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? 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. 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. 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 … 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 … It has a typical fuel capacity of 90 gallons which means the full fuel useful load is approximately 1,080 pounds. CESSNA 210E Centurion (1965 - 1965) Typical Price: $78,680.00 ... 2009 CESSNA AIRCRAFT CO LC41-550FG. Range decreased to 30 degrees, fuel capacity increased from 65 to 90 USgal ( 246 341! 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