Cessna TU206

The Cessna TU206 Turbo Stationair Series is a model in the 205 / 206 / 207 family. It is described here as a Six-seat high-wing piston single. FAA type-certificate reference: A4CE.

Cessna TU206 Turbo Stationair Series is part of the Cessna 206 / Stationair type family certificated under FAA A4CE. The represented landplane configuration uses the TSIO-520-C rated at 285 hp and a 3,600 lb maximum takeoff weight. The standard fuel configuration represented here provides 63 U.S. gallons usable from 65 gallons total. This catalog entry is a series-level designation rather than a single model-year production suffix. The 206 family spans Super Skylane, Super Skywagon, Stationair and turbocharged derivatives, so model suffix, serial number, engine and fuel-system applicability must be kept distinct.

Standard total fuel: 65 U.S. gallons. Standard usable fuel: 63 U.S. gallons. Series-level baseline. Individual TU206 suffixes and later TU206G fuel systems have separate applicability.

FAA A4CE contains model-, serial-number-, float/skiplane-, fuel-system- and equipment-specific branches. Use the aircraft data plate, serial number, applicable POH/AFM, equipment list and current weight-and-balance record before applying these model-level figures.

Maximum takeoff weight: 3,600 lb. FAA A4CE refers to the approved weight-and-balance data for baggage/cargo loading. The represented landplane maximum takeoff weight is 3,600 lb. Floatplane, amphibian or skiplane limits can differ where approved. Operational loading must use the individual aircraft's approved station arms, baggage/cargo limits and CG envelope. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna TU206 Turbo Stationair Series calculator.