Cessna T206H

The Cessna T206H 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 available production record begins in 1999.

Cessna T206H Turbo Stationair is part of the Cessna 206 / Stationair type family certificated under FAA A4CE. The represented landplane configuration uses the TIO-540-AJ1A rated at 310 hp and a 3,600 lb maximum takeoff weight. The standard fuel configuration represented here provides 88 U.S. gallons usable from 92 gallons total. The T206H is the turbocharged restarted-production Stationair branch approved under A4CE in 1998. 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: 92 U.S. gallons. Standard usable fuel: 88 U.S. gallons. Units T20608001–T20608361: 92 total / 88 usable; units T20608362 and on: 92 total / 87 usable.

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 ramp weight: 3,617 lb. Maximum takeoff weight: 3,600 lb. Maximum baggage: 180 lb at the approved aft baggage station. The represented landplane maximum takeoff weight is 3,600 lb. Maximum ramp weight is 3,617 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 T206H Turbo Stationair calculator.