Cessna TU206A

The Cessna TU206A Turbo Super Skywagon / 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 1966.

Cessna TU206A Turbo Super Skywagon / Stationair 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. 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. The standard 65/63-gallon system is represented; approved long-range installations are serial/configuration dependent.

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 TU206A Turbo Super Skywagon / Stationair calculator.