cessna 210 turboprop

Registration # Search. Additive manufacturing turned what was previously 855 parts into just 12. The wing planform remained the same (constant 64" chord from centerline to 100 inches (2,500 mm) out, then straight taper to 44" chord at 208 inches from centerline), but the semi-Fowler flaps (slotted, rear-moving) were extended outboard, from Wing Station 100 to Wing Station 122, which allowed a lower landing speed (FAA certification regulations state that a single-engined aircraft must have a flaps-down, power-off stall speed no greater than 70 miles per hour (110 km/h). Mooney expressed interest in that engine, but thus far, the project hasnt materialized and it may not for the same reasons that turbines have stumbled before: difficult-to-manage fuel specifics and small airframes with no place to put the fuel.Meanwhile, more than 100 of O&Ns Silver Eagle-modified 210s are flying and we recently visited the companys shop in Factoryville, Pennsylvania, to evaluate the mod and do a flight trial.No sugar coating here: The Silver Eagle, at $980,000 complete, is not a cheap mod. Listing Type. This mod is no latecomer, having been perking along since about 1992, when industry veteran Myron Olson made it a signature product of the O&N shop, whose history dates back to 1986. Its a bit graceless, but when you pull the prop past the detent into Beta and stop in 500 feet, you get over that. Aerospace Systems and Technologies offers an ice protection system for the Cessna 210, models L, M and N. This system is a TKS technology that "weeps" chemicals which depress the freezing point of water and will both remove accumulated ice and then prevent ice formation. This conversion includes an airframe overhaul, airframe modifications, new avionics, new paint and installation of a Rolls-Royce Model 250 powerplant. State. When we visited O&N in June, the company was completing work on yet another conversion-turbines for the popular Cessna 340 pressurized twin. The 210 has the capacity for one crew member and five passengers. These aircraft replace the Cessna 210 at the top end of the Cessna single-engine model line. Write CSS OR LESS and hit save. 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 1986. Enter the CESSNA DENALI single-engine turboprop, a brand-new high-performance aircraft that changes everything. The 210N, T210N (turbocharged), and P210N (pressurized) versions were produced in the greatest quantity. This spawned an entirely new family of Cessna aircraft including the 206 and the eight-seat 207.[13]. Both rugged and flexible, our legendary turboprops are configurable to your requirements. Max climb at gross weight is claimed at 2200 FPM and although we didnt see that, the 210 had no trouble loafing along at 1500 FPM, so the climb into the flight levels is typically going to be under 20 minutes, which is a must for milking max range out of the airplane. O&N Aircraft offers a turboprop conversion of the Pressurized Cessna P210N known as the "Silver Eagle". O&N will take an owners 210 or find one on the market and perform the conversion, which is essentially a remanufacture. The aircraft was offered in a normally aspirated version, designated the model 210, as well as the turbocharged T210 and the pressurized P210 versions. For as fast as it climbs, the Silver Eagle can come down just as fast. 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. Maintenance. Multistage single-crystal turbine blades with internal cooling passages help deliver superior combustion efficiencies and longer overhaul periods. The OAT was -5 degrees C, which is ISA +14. The average price of the Centurion P210 - Turbine is $795,000. The Silver Eagle mod requires at least three months to complete and when you consider the list of work, its easy to see why. The converted 210 will produce climb rates of 2100 ft/min, cruise speeds of 200 - 210 knots and shorter take-off and landing distances, while consuming 20 - 28 gallons of Jet A per hour depending on altitude and air temperature. To compensate for the reduced aileron span, the aileron profile was changed and its chord enlarged. On 12 July 1968, Leonard Bendicks hijacked a Cessna 210 from, While flying N6579X, an early model 210A, famed, This page was last edited on 28 October 2020, at 11:08. O&N is a general maintenance shop with expertise in the Cessna 210 and P210 models, but with a line of mods including extended-range fuel tanks, control modifications for Cessnas and nacelle wing tanks for Navajos and Senecas. Some models featured de-icing boots as an option. Strong partnerships create convenient solutions. Due to its single spar wing structure, the 210 could not meet the current certification standards. The engines performance gradient relative to temperature is greater than the true airspeed gain with altitude. At cruise speeds typically in the 200-knot range, O&N claims a still-air range of about 1000 miles, which the airplane will do under ideal temperature conditions with a comfortable reserve. The early Cessna 210 (210 and 210A) had four seats with a Continental IO-470 engine of 260 hp (190 kW). Its an absolute agita reducer to have the reverse thrust available. CESSNA Turboprop Aircraft For Sale 1 - 25 of 122 Listings. The FAA issued an Airworthiness Directive on 21 February 2020 mandating eddy current inspections of the carry-thru spar lower cap, corrective action if necessary, application of a protective coating and corrosion inhibiting compound, and reporting the inspection results to the FAA. In 1970 the 210K became the first full 6-seat model; this was achieved by replacing the flat-leaf main gear springs with tapered tubular steel springs of greater tread width (which allowed the tires to be nested farther back in the fuselage). Because their fuel specifics arent quite as stingy as piston engines, turbines require more fuel…a lot more fuel. You've disabled cookies in your web browser. Interested in buying this aircraft click here. *Performance data is based on standard conditions with zero wind. In fact, given its weight and power output, it has significant advantages over the competing engine, Pratts PT6. When we lined up on Seamans Airports 2500-foot runway, it felt awfully short for something as heavy as a 210. We use cookies to help you get the best experience when using our website. Of course, the weight cuts both ways, since the 250 is lighter than the gasoline engine it replaces, batteries and other gear have to remain forward. Unless otherwise noted, these reviews carry product pricing from the time of the original review. The turbine engine is impossibly alluring. Cessna 1980 N731LU. The 1964 model 210D introduced a 285 hp (213 kW) engine and 2 small child seats, set into the cavity which contained the mainwheels aft of the passengers. For more information, please visit our Privacy Policy. No thrashing pistons, grinding cams, clicking valves-just far fewer exquisitely balanced parts all whirring in the same direction. In order to make turboprop conversions work in light singles, the engine has to meet a narrow set of parameters with regard to weight and fuel consumption. Serial/Series # Search. It was essentially a Cessna 182B to which was added a retractable landing gear, swept tail, and a new wing. The early strut-winged Cessna 210B was developed into a fixed-gear aircraft known as the Cessna 205. Full of gas, its two people and light bags. With the power lever forward, however, it was obvious after 50 feet of takeoff roll, 2500 feet is a cakewalk. Several modifications and optional fittings are also available including different engine installations, wing tip tanks, speed brakes, STOL kits and gear door modifications. The TKS panels are installed on the leading edges of the wings, horizontal stabilizers and vertical stabilizer.

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