Performance | |
Standard day, sea level, maximum gross weight unless otherwise noted | |
Maximum speed (VNE) | 95kts. 176km/hr |
Maximum cruise speed (vh) | 86 kts. 159km/hr |
Hover ceiling, In-Ground-Effect (1700 lb) | 10,800 ft. / 3,292 m |
Hover ceiling, Out-of-Ground-Effect (1700 lb) | 8,600 ft. / 2,621 m |
Range (long range cruise* speed @ 4,000 feet) (no reserve) | • 32.5 gallon • 64.0 gallon |
Weights | |
Maximum takeoff gross weight | 2,050 lb. / 930kg |
Empty weight, standard configuration | 1,100 lb. / 499 kg |
Useful load | 950 lb. / 431 kg |
Dimensions | |
Fuselage length | 22.19 ft. / 930 kg |
Fuselage width | 4.25 ft. / 1.30 m |
Fuselage height | 7.17 ft. / 2.18 m |
Overall length (rotors turning) | 30.83 ft. / 9.40 m |
Overall height (to top of tail rotor | 8.72 ft. / 2.65 m |
Width (canopy) | 4.25 ft. / 1.30 m |
Main rotor Diameter | 26.83 ft. / 8.18 m |
Main landing gear tread (fullycompressed) | 6.54 ft. / 1.99 m |
Accommodations | |
Normal cabin seating (training) | 2 passengers |
Maximum certified cabin seating (utility) | 3 passengers |
Cabin length | 4.75 ft. / 1.45 m |
Cabin width | 4.92 ft. / 1.50 m |
Powerplant | |
Type | Textron Lycoming HIO–360–D1A |
Powerplant ratings (per engine, standard day, sea level) | - Takeoff (5-minute) 190 shp / 141 kw - Maximum continuous 190shp /141 kw |
Fuel Capacity | |
Standard fuel capacity | 32.5 US gal - 123.03 |
Extended range capacity | 64.0 US gal - 242.27 |
Performance | |
Standard day, sea level, maximum gross weight unless otherwise noted | |
Maximum speed (VNE) | 94kts. 174km/hr |
Maximum cruise speed (vh) | 80kts. 148km/hr |
Hover ceiling, In-Ground-Effect (1700 lb.) | 7,000 ft / 2,133 m |
Hover ceiling, Out-of-Ground-Effect (1700 lb.) | 4,800 ft. / 1,463 m |
Range (long range cruise* speed @ 4,000 feet) (no reserve) | • 32.5 gallon • 64.0 gallon |
Weights | |
Maximum takeoff gross weight | 1,750 lb. / 794kg |
Empty weight, standard configuration | 1,102 lb. / 500 kg |
Useful load | 648 lb. / 294 kg |
Dimensions | |
Fuselage length | 22.19 ft. / 930 kg |
Fuselage width | 4.25 ft. / 1.30 m |
Fuselage height | 7.17 ft. / 2.18 m |
Overall length (rotors turning) | 30.83 ft. / 9.40 m |
Overall height (to top of tail rotor) | 8.72 ft. / 2.65 m |
Width (canopy) | 4.25 ft. / 1.30 m |
Main rotor Diameter | 26.83 ft. / 8.18 m |
Main landing gear tread (fully compressed) | 6.54 ft. / 1.99 m |
Accommodations | |
Normal cabin seating (training) | 2 passengers |
Maximum certified cabin seating (utility) | 3 passengers |
Cabin length | 4.75 ft. / 1.45 m |
Cabin width | 4.92 ft. / 1.50 m |
Powerplant | |
Type | Textron Lycoming HIO–360-G1A |
Powerplant ratings (per engine, standard day, sea level) | -Takeoff (5-minute) 180 shp / 134 kw -Maximum continuous 180shp / 134 kw |
Fuel Capacity | |
Standard fuel capacity | 32.5 US gal / 123.03 |
Extended range capacity | 64.0 US gal / 242.27 |