Overview
The Cessna Denali is a single-engine turboprop developed as a competitor in the high-performance utility segment. Announced in the 2010s, it introduces a new engine and modern avionics. The aircraft is intended for corporate and regional operations.
Specifications
Units
- Engine
- 1 × General Electric Catalyst
- Engine type
- Turboprop
- Power
- 1,300 shp · 969 kW
- Avionics
- Garmin G3000
- Wing tips
- Blended tips
- Seats
- 11
- Crew
- —
- Cabin width
- 5 ft 3 in · 1.60 m
- Cabin height
- 4 ft 10 in · 1.47 m
- Cabin length
- 16 ft 9 in · 5.11 m
- Exterior length
- 48 ft 9 in · 14.86 m
- Tail height
- 15 ft 2 in · 4.62 m
- Fuselage diameter
- 5 ft 11 in · 1.80 m
- Wing span
- 54 ft 3 in · 16.54 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- —
- Max landing weight
- —
- Max payload
- —
- Fuel capacity
- 170 gal · 600 L · 500 kg (Jet A)
- Max cruise speed
- 285 kt · 328 mph · 528 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,600 nm · 1,840 mi · 2,960 km
- Fuel burn
- —
- Ceiling
- 31,000 ft · 9,400 m
- Rate of climb
- —
- Takeoff distance
- 2,950 ft · 900 m
- Landing distance
- —
Gallery
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