Cessna T206 Turbo Stationair — Supplemental Type Certificate

This document provides detailed information about the Soloy Mark II conversion for the Cessna 206 series, specifically focusing on the turbine modifications that enhance performance. It discusses the history of turbine conversions for the Cessna 206, starting with the Mark I model and transitioning to the Mark II, which features a more powerful Rolls-Royce 250-B17F engine. The document outlines the advantages of the Mark II conversion, including improved takeoff performance, fuel efficiency, and operational capabilities for various missions. It is intended for pilots and aviation enthusiasts interested in turbine modifications for the Cessna 206 series, particularly the 206H and T206H models.

• Rolls-Royce 250-B17F engine provides 417 shp and 510 thermodynamic horsepower.
• Maximum takeoff weight is 3,600 lbs with a useful load of 1,477 lbs.
• Cruise speed can reach 180 KTAS at higher altitudes with a fuel burn of 25 gph.
• Takeoff distance over a 50-ft obstacle is 1,195 ft.
• Maximum operating altitude is 20,000 ft.