CESSNA 205 Civil Aircraft Model Details

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General Information of CESSNA 205

Developed From : Cessna 210

Introduction : 1962 (206)

Manufacturer : Cessna

Number Built : over 8509 (as of approx. 2006)

Role : light aircraft

Status : in production

Unit_Cost : 206H US$557,500 (2012)[1]; T206HUS$597,500 (2012)[2]

General characteristics of CESSNA 205

Airfoil : NACA 2412 (modified)

Capacity : 5 passengers

Crew : one

Empty Weight : 2,176 lb (987 kg)

Height : 9 ft 3½ in (2.83 m)

Length : 28 ft 3 in (8.61 m)

Max Takeoff Weight : 3,600 lb (1,632 kg)

Powerplant : 1 × Lycoming IO-540-AC1A air-cooled flat-six engine, 300 hp (224 kW)

Wing Area : 175.5 ft² (16.30 m²)

Wingspan : 36 ft 0 in (10.97 m)

Performance of CESSNA 205

Cruise Speed : 163 mph (142 knots, 263 km/h) at 6,200 ft (1,890 m)

Maximum Speed : 174 mph (151 knots, 280 km/h) at sea level

Range : 840 mi (730nmi, 1,352 km)

Rate Of Climb : 988 ft/min (5.0 m/s)

Service Ceiling : 15,700 ft (4,785 m)

Stall Speed : 63 mph (54 knots, 100 km/h)

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