BELL 412EP
General characteristics
Crew: one-two pilots
-
Capacity: up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[3]
-
Length: 56 ft 1 in (17.09 m) including rotors
-
Fuselage length: 43 ft (13 m)
-
Height: 15 ft 0 in (4.57 m)
-
Empty weight: 6,789 lb (3,079 kg)
-
Max takeoff weight: 11,900 lb (5,398 kg)
-
Powerplant: 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac coupled turboshaft engine, 1,250 shp (930 kW)/900 shp (671 kW) single power section emergency power
-
Main rotor diameter: 46 ft 0 in (14.02 m)
-
Main rotor area: 1,662 sq ft (154.4 m2) *Blade sections: - root Boeing VR-7 ; tip Wortmann FX 71-H-080[54]
Performance
-
Maximum speed: 140 kn (160 mph, 260 km/h)
-
Cruise speed: 122 kn (140 mph, 226 km/h)
-
Range: 529 nmi (609 mi, 980 km)
-
Service ceiling: 20,000 ft (6,100 m)
-
Rate of climb: 1,350 ft/min (6.9 m/s)
-
Power/mass: 0.2663 hp/lb (0.4378 kW/kg)
|