Aircraft › Cessna › Cessna 206 Stationair › Cessna T206H, TU206 Turbo Stationair

Cessna T206H, TU206 Turbo Stationair

This page covers the turbocharged Stationairs: the TU206 and TP206 models with a Continental TSIO-520 of 285 hp to 310 hp, and the T206H with a Lycoming TIO-540-AJ1A of 310 hp. The figures are those of the older T206H handbook, which three copies agree on: a maximum weight of 3,600 pounds, 87 gallons of usable fuel, a 75 percent power cruise of 164 knots at 20,000 feet, a range of 559 nautical miles with a 45 minute reserve, and a service ceiling of 27,000 feet. The current Turbo Stationair HD has a higher takeoff weight.

Range
645 miles (559 nm, 1,040 km) with the load named above
Cruise speed
164 knots (300 km/h)
Seats
About 6
Engines
One piston engine in the nose: Continental TSIO-520 series (TU206 and TP206, 285 to 310 hp) and Lycoming TIO-540-AJ1A (T206H, 310 hp)
Max takeoff weight
3,600 lb (1,633 kg)
Cessna T206 Turbo Stationair
Photo: ZLEA, CC BY-SA 4.0
Cessna T206H, TU206 Turbo Stationair seen from above: length 28 ft 3 in (8.61 m), wingspan 36 ft 0 in (10.97 m)
Drawing: cwsi.net, from published dimensions (a schematic, not to exact detail)

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Specifications

Length28 ft 3 in (8.61 m)
Wingspan36 ft 0 in (10.97 m)
Height9 ft 3 in (2.83 m)
Fuselage width4 ft 1 in (1.25 m)
Ceiling27,000 ft (8,200 m)
Fuel capacity90 US gal (329 L)
StatusIn service
Type codesICAO T206

Private aircraft show specs only. No flight data is shown for them.

Sources

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