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Cessna 210

Development
1960 model Cessna 210, showing the leg braced wing used on the first model 210.
A Cessna T210L shows the model later in strutless cantilever wing
Cessna T210L
A Cessna Centurion P210N Pressurized with small separate windows
A panel update Cessna T210 instrument.
A 1967 Cessna 210G modified with a leading edge cuff and flaperons features for better performance Low Speed
The early Cessna 210 (210 and 210A) had four seats with a Continental IO-470 engine 260 hp (190 kW). It was essentially a Cessna 182B was added in which a retractable landing gear, tail swept, and a new wing. In 1961, the fuselage and wings have been completely redesigned – the fuselage was made wider and deeper, and a third side window was added. The wing planform remained the same (constant 64 "chord from spindle to 100 inches (2,500 mm) outside and form right at 44" agreement to 208 inches of the line Central), but the shutters semi-Fowler (slotted, rear-Mobile) were extended outboard of Wing Station 100 to Station 122 wing, which allowed a landing speed (certification regulations of the FAA indicates that a single-engine airplane must have a flaps down, power off stall speed not exceeding 70 miles per hour). To compensate for the reduced length of fins, the fin profile has been amended and extended its string. The Presented a model 210D 1964 285 HP (213 kW) engine and seating for two small children, put in the recess which contains the mainwheels rear passengers.
In 1967, the 210G model introduces a cantilever wing replacing the wing strut-reinforced. Its planform changed to a constant taper root rope rope edge. In 1970, the 210K became the first comprehensive model 6-seater, which was obtained by replacing the flat leaf springs train conical springs with the main steel tube over the tread width (allowing the tires to be nested further back in the fuselage). In 1979, 210N model eliminated the folding doors that covered the back main gears; tubular sources are returned in the shallow channels along the part lower fuselage and the wheels are adjusted in a closed depression on the lower fuselage. Some models presented de-icing boots Optional.
The device has been available in aspirated version, designated the Model 210 and the T210 turbo versions P210 pressure.
Succession
Cessna re-introduced three models of single engine in 1998 which had been in production since 1986 – the Cessna 172, 182 and 206. The 210 has been reintroduced not at that time that it was company policy that all air is reintroduced to the last re-certified to FAR Part 23 standards instead of the original CAR-3 standards. Thanks to its single spar wing, the 210 could not meet current certification standards. This left a gap in the line of Cessna single engine for high performance that was quickly filled by competitors such as the Cirrus SR22 and Columbia 400. In 2006, Cessna announced that it would produce a new aircraft, while the development known as the Cessna NGP. The intention was that the new aircraft would fill the void left in the line Cessna when the 210 came out of production in 1986.
In November 2007, Cessna has acquired the assets of Columbia Aircraft Company. The Columbia 350 and 400 models have been integrated in the range of Cessna single-engine Cessna and renaming the Cessna 350 and 400. These aircraft replaced the Cessna 210 at the upper end of the line Cessna single engine.
Changes
N & O offers a conversion turboprop aircraft Cessna P210N pressure known as the "Silver Eagle". This conversion includes a review of the cell, the cell changes, new avionics, new paint and the installation of a Rolls-Royce Model 250 powerplant.
The 210 converted to rate of climb of 2,100 ft / min, cruising speed of 200-210 knots and short takeoff and landing distances, while 20 consumers – 28 gallons of Jet A per hour depending on altitude and air temperature. Complete range with 147 gallons of Jet A is greater than 1350 nm (1566 miles). The conversion costs $ 600,000 USD, USD $ 350,000 for the engine, plus the cost of using the Cessna 210.
Aerospace Systems and Technologies provides a system of protection against icing for Cessna models 210, L, M and N. This system is a technology That TKS "weeping" chemicals that lower the freezing point of water and remove accumulated ice and prevent ice formation. The panels are installed on the TKS leading edges of wings, horizontal stabilizers and vertical fin. They are complemented by a slinger ring on the propeller and a spray windshield.
Introduced in November 2008, the Crownair enturion edition T210 is a reconditioned unit comprising a glass cockpit and new engine and other minor improvements. The company says increased payload, cruise speed and range.
Cessna 210 used in the Australian outback for light passenger and cargo charter and aerial survey work. Many have suffered because of these conditions difficult and were found to have severe corrosion on the wing spar carry-through beam. Aeronautical Engineers Australia has proceeded an in-depth analysis to determine the fatigue limits for the safe recovery of deferral through, which prevents the replacement cost Part. This is now available as a CASA approved generic repair.
Variants
The Cessna 210 was Manufactured in 26 variants models, the C210, C210A-D, the Centurion-C210E H & J, Turbo Centurion T210F-H & J, the Centurion II C210K-N & R, the Centurion II Turbo T210K-N & R and P210N & R. The 210N, T210N (turbo), and P210N (pressurized) versions have been produced in greater quantity. Models rarest and most expensive were the T210R and P210R, which were produced in small quantities in 1985-86.
Several modifications and optional equipment are also available, including facilities with different engines, the wing tip tanks, speed brakes, STOL kits and changes gear door.
The start of leg winged Cessna 210B has been developed in a fixed gear airplane called the 205 Cessna. It has generated an entirely new family of aircraft Cessna 206 and whose registered eight 207.
210
variant four-seater with a Continental IO-470-E, 40 ° water component, landing gear doors, introduced in 1960., first flight in 1957, 575 built.
210A
A 210 with a third cabin window on each side, in 1961, 265 built.
210B
A 210A with a cut-down rear fuselage, a viewing window to the rear and a Continental IO-470-S, introduced in 1962, 245 built.
210C
A 210B with some minor changes, introduced in 1963, 135 built.
210D Centurion
On equipped with an HP 210C 285 (213 kW) Continental IO-520-A engine and increased the takeoff weight to £ 3100 (1.406 kg), introduced in 1964, 290 built.
210E Centurion
A 210D with a few modifications Minor, introduced in 1965, 205 built.
210F Centurion / Centurion Turbo
A 210E with minor changes and optional 285 hp (213 kW) turbocharged Continental TSIO-520-C engine, introduced in 1966, 300.
210G Centurion / Centurion Turbo
A 210F with a wing cantilver strutless and modified the rear window increased takeoff weight of 3,300 pounds (1.497 kg), introduced in 1967, 228 built.
210H Centurion / Centurion Turbo
A system with a 210G of new components and instrument panel, 210 built. Flap range decreased to 30 degrees, increased the fuel capacity of 65-90 gallons (246-341 l). Introduced 1968.
210J Centurion / Centurion Turbo
A 210H with dihederal wing reduced, different profile of the nose and a Continental IO-520-J (or engine TSIO-520H), introduced 1969, 200 built.
210K Centurion / Centurion Turbo
210J with a full rear seat changed to provide six seats, an engine IO-520-L 300 hp (224 kW) limited to 5 minutes, the gear has changed, extended cab with a unique rear side window, weight increase to £ 33.800 (1.724 kg), produced 1970-71, 303 built.
210L Centurion / Centurion Turbo
A 210K with a nose-mounted landing lights, electricity system has changed to 24 volts, the motor hydraulic pump replaced by an electric pump and a three-bladed propeller fitted. improved aerodynamics led to an increase of about 8 knots (15 km / h) cruising speed. Produced 1972-76, 2070 built.
210M Centurion / Centurion Turbo
A 210L with an optional 310 hp (231 kW) engine TSIO-520-R and minor changes, produced 1977-80, built in 1381.
210N Centurion / Centurion Turbo
A 210M with wells freewheel to the main landing gear and minor modifications. Although this change appeared only on the C210N, most models have been quick traps Train removed for maintenance and material handling problems, leaving them similar to the "N". Produced 1981-84, built in 1943.
210R Centurion / Turbo Centurion
A 210N with stabilizer span and more minor changes, produced from 1985 to 1986, 112 built.
P210N Pressurized Centurion
A Turbo 210N pressurized cabin, four windows on each side, with a 310 HP (231 kW) Continental TSIO-520-AF motor, produced 1978-83, 834 built.
P210R Pressurized Centurion
A stabilizer P210N with more scope to increase take-off and 325 HP (242 kW) Continental engine GTSIO-520-EC, produced 1985-86, 40 built.
Operators
Military
Bolivia
Dominican Republic
Croatia
El Salvador
Jamaica
Jamaica Defence Force
Mexico
Philippines
Panama
Paraguay
Paraguayan Air Force – 2 210N
Paraguayan Naval Aviation – 2 210N
Civil
Australia
King Leopold Air, Broome, Western Australia – 7
Slingair, Kununurra, Western Australia – 6.
Costa Rica
Service air monitoring
U.S.
Flight Express (airline of the United States), Orlando, Florida – 59
Accidents and Incidents
While flying N6579X, an early model 210A, famous test pilot Scott Crossfield crashed and died in the woods of Georgia April 19, 2006. The National Transportation Safety Board determined the probable cause as "failure of the driver to get updated weather information way, which resulted in his continued instrument flight in a large area of severe convective activity, not the air traffic controller to provide adverse weather avoidance assistance, as required by Federal Aviation Administration directives, both of which led to the aircraft encountered with a violent storm and lost control. "
Specifications (T210N Turbo Centurion II)
Data from Janes' All The World's Aircraft 1982-83
Characteristics
Crew: One
Capacity: Five passengers
Length: 28 m 2 in (8.59 m)
Wingspan: 36 feet 9 inches (11.20 m)
Height: 9 ft. 8 in. (2.95 m)
Wing area: 175 ft (16.23 m)
Curb weight: £ 2303 (1045 kg)
Max takeoff weight: 4,000 pounds (1.814 kg)
Engines: 1 Continental Motors TSIO-520-R air-cooled flat-six turbo, 310 hp (231 kW)
Performance
Maximum Speed: 204 knots (235 mph, 378 km / h) at 17,000 feet (5,200 m)
Cruising speed: 193 knots (222 mph, 358 km / h) at 20,000 feet (6,100 m)
Stall Speed: 58 knots (67 mph, 108 km / h) CAS, flaps, power off
Range: 900 nautical miles (1036 km, 1.668 km) cruising at 10,000 Economy feet (3,050 m)
Service ceiling: 27,000 feet (8230 m)
Rate of climb: 930 m / min (4.7 m / s)
Wing loading: 22.9 lb / ft (111.8 kg / m)
Power / mass: 0.078 hp / lb (0.13 kW / kg)
See also
Related development
Cessna 182
Cessna 206
Comparable aircraft
Beechcraft Deal
Cessna 206
Piper Saratoga
Piper Malibu
References
Notes
Ab ^ Taylor 1982, p. 345,346
^ ABCDEFGHIJKLMNOPQR Simpson, 1991 103-104
^ Textron (November 2007). "Textron Cessna Aircraft Company to Acquire Assets of Columbia Aircraft". http://investor.textron.com/phoenix.zhtml?c=110047&p=irol-newsArticle&ID=1081833&highlight =. Retrieved 28/11/2007.
Developments ^ FibreGlast Corp (January 2004). "January 2004: O & N Aircraft. http://www.fibreglast.com/contentpages-aircraft-346.html. Retrieved 19/10/2007.
Aviation Crownair ^ (Undated). Centurion T210 New Edition by Crownair aviation. http://www.crownairaviation.com/upgrade-centurion.html. This Retrieved 13/11/2008.
^ Aviation Engineers Australia (March 2009). "Aeronautical Engineers Australia – Changes". http://www.aeroengaus.com.au/mods.htm. Retrieved 03/03/2009.
^ Abcdefg Danielle Bruckert and Oleg Roud (2008). Cessna 210 Training Manual. ISBN 978-0-557-01418-7.
^ Australian civil research aircraft register using "210" and "King Leopold Air" as the search parameters. Search 12/12/2008.
^ Australian Research Civil Aircraft register using "210" and "Slingair" as search parameters. Search 31/10/2007.
^ Flight Express (2005). "Cessna 210". http://www.flightexpress.com/flight_express_fleet_cessna_210.htm. Retrieved 20/10/2007.
^ NTSB (September 2007). "NTSB Probable Cause Report CHI06MA115 [2007]. Http: / / www.ntsb.gov/ntsb/brief.asp?ev_id=20060501X00494&key=1. Retrieved 02/06/2008.
bibliography
Taylor, John WR (1982). Jane's All The World's Aircraft 1982-1932. London: Jane's Yearbooks. ISBN 0 7106-0748-2.
Simpson, RW (1991). General Aviation Airlife. England: Airlife publishing. ISBN 1 85310 104 X.
References
Wikimedia Commons has media related to: Cessna 210
Cessna Pilots Association
Cessna Owner Organization
FAA Type Certificate Data Sheet 3A21 Type Certificate Data Sheet for Cessna 210 models.
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Categories: Cessna | United States civil utility aircraft 1950-1959Hidden categories: Articles lacking sources from October 2007 | All articles lacking sources | High wing aircraft | Propeller aircraft | single engine aircraft About the author

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