Cessna
C206
Stationair

C206G
Photo: Robert Deering 10/12/2008
Alliance Airport (AFW)
Fort Worth, Texas

The six-seat Model 206 was introduced as a 1964 model and was built until 1986, when Cessna halted production of its single-engine product. It was then re-introduced in 1998 and remains in production in 2008.

There were many sub-variants, including the U206, P206 all certified to CAR3 standards and later 206H certified to FAR Part 23.

The total Model 206 production between 1964 and 2004 was 6,581 aircraft.

Cessna U206

The original 1964 model was the U206, powered by a 285 hp (213 kW) Continental IO-520-A. The “U” designation indicated “utility” and this model was equipped with a pilot side door and large clamshell rear door serving the back two rows of seats, allowing easy loading of over-sized cargo.

There was a TU206 turbocharged version powered by the Continental TSIO-520-C engine producing 285 hp (213 kW). After 1967 the turbo TU206 was powered by a TSIO-520-F of 300 hp (220 kW) (the extra 15 hp (11 kW) were obtained by turning the engine at a higher rpm, and was only allowed for five minutes.[4] Due to the large propeller diameter, the additional engine speed meant that the propeller tips were pushed to transonic speeds, which required much more power.

From 1964 to 1969 the U206 was known as the “Super Skywagon”. From 1970 it was named the “Stationair”, a contraction of “Station Wagon of the Air”, which is a good description of the aircraft's intended role. Sub-variants were designated U206 to U206G.

In 1977 the U206 had its engine upgraded to a Continental IO-520-F of 300 hp (220 kW) (continuous rating, obtained at a lower speed than the previous IO-520-F) and the TU206 powerplant was changed to the TSIO-520-M producing 310 hp (230 kW).

Production of all versions of the U206 was halted in 1986 when Cessna stopped manufacturing all piston engine aircraft. A total of 5,208 U206s had been produced.

Cessna P206

1965 saw the P206 added to the line. In this case the “P” stood for “people”, as the P206 had passenger doors similar to the Cessna 210, from which it was derived, on both sides.

The P206 was produced from 1965 to 1970 and was powered by a Continental IO-520-A of 285 hp (213 kW). There was a turbocharged model designated TP206 which was powered by a Continental TSIO-520-A also of 285 hp (213 kW).

647 P206s were produced under the name “Super Skylane” which made it sound like a version of the Cessna 182, which it was not. Sub-variants were designated P206 to P206E.

SPECIFICATIONS: PERFORMANCE:
Span:  36 ft 0 in (10.97 m) Maximum speed:  174 mph (151 knots, 280 km/h) at sea level
Length:  28 ft 3 in (8.61 m) Cruising speed:  163 mph (142 knots, 263 km/h) at 6,200 ft (1,890 m)
Height:  9 ft 3½ in (2.83 m) Range:   840 mi (730 nmi, 1,352 km)
Empty Weight:   2,176 lb (987 kg) Service ceiling:  15,700 ft (4,785 m)
Gross Weight:  3,600 lb (1,632 kg)  
Crew:  Pilot and up to five passengers
Engines:  1 × Lycoming IO-540-AC1A air-cooled flat-six engine, 300 hp (224 kW)
   
SOURCE:  Wikipedia