Overview
The Pilatus PC-12 NG is a single-engine turboprop aircraft designed for passenger, cargo, and special mission roles. Developed in Switzerland, it has become one of the most successful aircraft in its class. The NG variant introduced upgraded avionics and improved performance.
Specifications
Units
- Engine
- 1 × Pratt & Whitney PT6A-67B
- Engine type
- Turboprop
- Power
- 1,200 shp · 895 kW
- Avionics
- Honeywell Primus Apex Glass Cockpit
- Wing tips
- No winglets
- Seats
- 9
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 23,000 lb · 10,500 kg
- Max landing weight
- —
- Max payload
- 1,500 lb · 700 kg
- Fuel capacity
- Max cruise speed
- 270 kt · 311 mph · 500 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- —
- Fuel burn
- 12.90 nm/gal · 6.31 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- 1,480 ft · 450 m
- Landing distance
- 940 ft · 290 m
Gallery
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Private Single Engine
ICAO: PC12
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