The 412 model was followed by the 412SP (Special Performance) version featuring larger fuel capacity, higher takeoff weight and optional seating arrangements.
General characteristics
- Crew: 1-2 pilots
- Capacity: up to 13 passengers, the maximum external load of 4.500 lb (2.040 kg)
- Length: 56 ft. 1 in. (1.17 m)
- Rotor diameter: 46 ft (14.0 m)
- Height: 15 ft (4.6 m)
- Disc area: 1.662 ft ² (154.4 m²)
- Empty weight: 6.789 lb (3.079 kg)
- Max takeoff weight: 11.900 lb (5.397 kg)
- powerplant: 2 × Pratt & Whitney Canada PT6T Twin-Pac-3BE turboshafts, 900 shp (671 kW) EACH
- fuselage length: 43 ft (13.1 m)
- Maximum speed: 140 knots (161 mph, 259 km / h)
- Cruise speed: 122 knots (140 mph, 226 km / h)
- Range: 402 nmi (463 mi, 745 km)
- Service ceiling: 20,000 ft (6.096 m)
- Rate of climb: 1.350 ft / min (6.86 m / s)
- Power / mass: 0.2663 hp / lb (437 W / kg)
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