Cessna T207A

The Cessna T207A Turbo Stationair is a model in the 205 / 206 / 207 family. It is described here as a Seven/eight-seat high-wing piston single. FAA type-certificate reference: A16CE.

The cataloged production period is 1977–1984.

Cessna T207A Turbo Stationair is the stretched Cessna 207-family Stationair derivative certificated under FAA A16CE. The represented configuration uses the Continental TSIO-520-M rated at 310 hp and a 3,800 lb maximum takeoff/landing weight. The fuel configuration represented here provides 73 gallons usable from 82 gallons total. The 207 family adds cabin length and seating capacity relative to the 206 and includes both normally aspirated and turbocharged branches.

Standard total fuel: 82 U.S. gallons. Standard usable fuel: 73 U.S. gallons. Later T207A production uses the higher-capacity wing-tank configuration; published POH/NTSB data identify 36.5 usable gallons per wing, 73 usable total.

FAA A16CE contains serial-number-dependent fuel and seating data. Verify exact serial number, engine, tank installation, seating arrangement and the current POH/AFM before applying model-level values.

Maximum takeoff weight: 3,800 lb. Maximum landing weight: 3,800 lb. A16CE uses model/serial-number-specific baggage and loading stations; do not replace them with a single generic baggage arm. Maximum takeoff and landing weight is 3,800 lb. The longer cabin uses multiple passenger and baggage stations, so operational calculations must use the aircraft-specific station arms and limits. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna T207A Turbo Stationair calculator.