Cessna 210
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Cessna 210
Le Cessna 210 sur Wikipedia de langue anglaise :
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The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine [Vous devez être inscrit et connecté pour voir ce lien] which was first flown in January [Vous devez être inscrit et connecté pour voir ce lien] and produced by [Vous devez être inscrit et connecté pour voir ce lien] until 1985.
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The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine [Vous devez être inscrit et connecté pour voir ce lien] which was first flown in January [Vous devez être inscrit et connecté pour voir ce lien] and produced by [Vous devez être inscrit et connecté pour voir ce lien] until 1985.
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Re: Cessna 210
Development
The early Cessna 210 (210 and 210A) had 4 seats with a [Vous devez être inscrit et connecté pour voir ce lien] engine of 260 hp (190 kW).
It was essentially a Cessna 182B to which was added a retractable landing gear, swept tail, and a new wing.
In 1961 the fuselage and wing were completely redesigned - the fuselage was made wider and deeper, and a third side window was added.
The early Cessna 210 (210 and 210A) had 4 seats with a [Vous devez être inscrit et connecté pour voir ce lien] engine of 260 hp (190 kW).
It was essentially a Cessna 182B to which was added a retractable landing gear, swept tail, and a new wing.
In 1961 the fuselage and wing were completely redesigned - the fuselage was made wider and deeper, and a third side window was added.
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Re: Cessna 210
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-engine aircraft must have a flaps-down, power-off stall speed no greater than 70 miles/hour).
regulations state that a single-engine aircraft must have a flaps-down, power-off stall speed no greater than 70 miles/hour).
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Re: Cessna 210
To compensate for the reduced aileron span, the aileron profile was changed and its chord enlarged.
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.
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.
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Re: Cessna 210
In 1967 the model 210G introduced a [Vous devez être inscrit et connecté pour voir ce lien] wing replacing the strut-braced wing.
Its planform changed to a constant taper from root chord to tip chord.
In 1970 the 210K became the first full 6-seat model.
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.
Its planform changed to a constant taper from root chord to tip chord.
In 1970 the 210K became the first full 6-seat model.
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.
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Re: Cessna 210
This allowed the tires to be nested farther to the rear of the fuselage, making room for the full size rear seats.
In 1979 the 210N model eliminated the folding doors which previously covered the two retracted main wheels.
The tubular spring struts retract into shallow channels along the bottom of the fuselage and the wheels fit snugly in closed
depressions on the underside of the fuselage.
Some models featured de-icing boots as an option.
In 1979 the 210N model eliminated the folding doors which previously covered the two retracted main wheels.
The tubular spring struts retract into shallow channels along the bottom of the fuselage and the wheels fit snugly in closed
depressions on the underside of the fuselage.
Some models featured de-icing boots as an option.
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Re: Cessna 210
Succession
Cessna re-introduced three single engine models in 1998 that had been out of production since 1986 - the [Vous devez être inscrit et connecté pour voir ce lien], [Vous devez être inscrit et connecté pour voir ce lien] and [Vous devez être inscrit et connecté pour voir ce lien].
The 210 was not reintroduced at that time as it was company policy that all re-introduced aircraft would be recertified to the latest [Vous devez être inscrit et connecté pour voir ce lien] Part 23 standards instead of the original CAR-3 standards.
Due to its single spar wing structure, the 210 could not meet the current certification standards.
Cessna re-introduced three single engine models in 1998 that had been out of production since 1986 - the [Vous devez être inscrit et connecté pour voir ce lien], [Vous devez être inscrit et connecté pour voir ce lien] and [Vous devez être inscrit et connecté pour voir ce lien].
The 210 was not reintroduced at that time as it was company policy that all re-introduced aircraft would be recertified to the latest [Vous devez être inscrit et connecté pour voir ce lien] Part 23 standards instead of the original CAR-3 standards.
Due to its single spar wing structure, the 210 could not meet the current certification standards.
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Re: Cessna 210
This left a gap in the Cessna line for a high-performance single engine aircraft that was quickly filled by competitors such as the [Vous devez être inscrit et connecté pour voir ce lien] and [Vous devez être inscrit et connecté pour voir ce lien].
In 2006 Cessna announced that it would produce a new aircraft, known while under development as the [Vous devez être inscrit et connecté pour voir ce lien].
The intention was that this new aircraft would fill the gap left in the Cessna line when the 210 went out of production in 1986.
In 2006 Cessna announced that it would produce a new aircraft, known while under development as the [Vous devez être inscrit et connecté pour voir ce lien].
The intention was that this new aircraft would fill the gap left in the Cessna line when the 210 went out of production in 1986.
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Re: Cessna 210
In November, 2007, Cessna acquired the assets of [Vous devez être inscrit et connecté pour voir ce lien].
The Columbia 350 and 400 models were integrated into the Cessna single engine range and redesignated as the [Vous devez être inscrit et connecté pour voir ce lien] and [Vous devez être inscrit et connecté pour voir ce lien].
These aircraft replace the Cessna 210 at the top end of the Cessna single-engine model line.
The Columbia 350 and 400 models were integrated into the Cessna single engine range and redesignated as the [Vous devez être inscrit et connecté pour voir ce lien] and [Vous devez être inscrit et connecté pour voir ce lien].
These aircraft replace the Cessna 210 at the top end of the Cessna single-engine model line.
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Re: Cessna 210
Modifications
O&N Aircraft offers a [Vous devez être inscrit et connecté pour voir ce lien] conversion of the Pressurized Cessna P210N known as the "Silver Eagle".
This conversion includes an airframe overhaul, airframe modifications, new avionics, new paint and installation of a [Vous devez être inscrit et connecté pour voir ce lien] powerplant.
O&N Aircraft offers a [Vous devez être inscrit et connecté pour voir ce lien] conversion of the Pressurized Cessna P210N known as the "Silver Eagle".
This conversion includes an airframe overhaul, airframe modifications, new avionics, new paint and installation of a [Vous devez être inscrit et connecté pour voir ce lien] powerplant.
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Re: Cessna 210
The converted 210 will produce climb rates of 2100 ft/min, cruise speeds of 200 - 210 [Vous devez être inscrit et connecté pour voir ce lien] and shorter take-off and landing distances, while consuming 20 - 28 gallons of Jet A per hour depending on altitude and air temperature.
Range with a full 147 gallons of Jet A is over 1350 nm (1566 miles).
As of 2004 65 P210Ns had been converted at a cost of [Vous devez être inscrit et connecté pour voir ce lien]$600,000, including [Vous devez être inscrit et connecté pour voir ce lien]$350,000 for the engine, plus the cost of the used Cessna 210.
Range with a full 147 gallons of Jet A is over 1350 nm (1566 miles).
As of 2004 65 P210Ns had been converted at a cost of [Vous devez être inscrit et connecté pour voir ce lien]$600,000, including [Vous devez être inscrit et connecté pour voir ce lien]$350,000 for the engine, plus the cost of the used Cessna 210.
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Re: Cessna 210
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.
The TKS panels are installed on the leading edges of the wings, horizontal stabilizers and vertical stabilizer.
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.
The TKS panels are installed on the leading edges of the wings, horizontal stabilizers and vertical stabilizer.
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