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Turbine 206 Mk.II

Aircraft model

Conversion of the Cessna 206H Stationair or Cessna T206H Turbo Stationair consisting of a replacement of the original engine by a Rolls-Royce 250-B17F/2 turboprop engine.

Manufacturer Soloy Aviation Solutions
Aircraft family Airplane
Aircraft type Cessna 206 Stationair Turboprop
Engine type Turboprop
Engine count 1

Technical specifications

Dimensions
Height
3.1 m
10.17 ft
Length
9.25 m
30.35 ft
Wing area
16.17 m²
174.05 sq ft
Wingspan
10.97 m
35.99 ft
Performance
Service ceiling
20,000 ft
6,100 m
Speed limits
Va
125 kt
232 km/h / 144 mph
Vfe
140 kt
259 km/h / 161 mph
Vmo
150 kt
278 km/h / 173 mph
Weight limits
MLW
1,633 kg
3,600 lb
MTOW
1,633 kg
3,600 lb
MTW
1,641 kg
3,618 lb

Engine models

Manufacturer Name Cont. T/O
Rolls-Royce 250-B17F/2 336 kW 336 kW