Cessna 206 Stationair
Overview
The Cessna 206 Stationair is a general aviation aircraft manufactured by Cessna, with the profile centered on its personal/training/utility role. It first flew in 1962 and entered service in 1964. The current production-status field is listed as In Production. The listed configuration provides for a crew of 1 and passenger capacity of 5. Power is provided by 1 Lycoming IO-540 engine. Recorded dimensions include length 28.3 ft, wingspan 36 ft, height 9.3 ft. Maximum takeoff weight is listed as 3,600 lb. Listed performance includes cruise speed 140 kt. Its ICAO type designator is C206. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | C206 |
|---|---|
| First Flight | 1962 |
| Introduction Date | 1964 |
| Crew | 1 |
| Passenger Capacity | 5 |
| Length | 28.3 ft |
| Wingspan / Rotor Diameter | 36 ft |
| Height | 9.3 ft |
| Empty Weight | 2200 lb |
| Max Takeoff Weight | 3,600 lb |
| Cruise Speed | 140 kt |
| Engine Manufacturer | Lycoming |
| Engine Model | IO-540 |
| Engine Count | 1 |
Data verification status: Partially Verified