Cessna 206H

The Cessna 206H 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 1998.

Cessna 206H Stationair is part of the Cessna 206 / Stationair type family certificated under FAA A4CE. The represented landplane configuration uses the IO-540-AC1A5 rated at 300 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 206H restarted Cessna 206 production under an amended A4CE certification basis. 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 20608001–20608173: 92 total / 88 usable; units 20608174 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: 3,614 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 3,614 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 206H Stationair calculator.