Cessna TU206G

The Cessna TU206G Turbo Stationair 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.

The cataloged production period is 1977–1986.

Cessna TU206G Turbo Stationair is part of the Cessna 206 / Stationair type family certificated under FAA A4CE. The represented landplane configuration uses the TSIO-520-M rated at 310 hp and a 3,600 lb maximum takeoff weight. The standard fuel configuration represented here provides 59 U.S. gallons usable from 61 gallons total. The TU206G uses the higher-powered turbocharged TSIO-520-M branch and serial-dependent fuel systems. 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: 61 U.S. gallons. Standard usable fuel: 59 U.S. gallons. A4CE lists 61/59-gallon standard and 80/76-gallon optional systems for specified serials, and a later 92/88-gallon integral-tank system.

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. Later applicable serial numbers carry a 180 lb baggage-net limitation; earlier aircraft refer to approved W&B data. 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 TU206G Turbo Stationair calculator.