Bell 222

Specifications

 * Model 222
 * Announced 1974
 * First Flight August 13, 1976
 * Certified December 1979
 * Delivered 1980
 * Seats Front: pilot + one. Main: 4–6 (depending on seat types)
 * Maximum 10 (pilot and 9 passengers)[7]
 * Height 11ft 8in (3.56m)
 * Fuselage length 42ft 2in (12.85m)
 * Rotor diameter 40ft (12.2m)
 * Length overall 49ft 6in (15.1m)
 * Engine (2x) Lycoming LTS-101-650C-3
 * Power (2x) 618hp (461kW)
 * Max speed 130kt (149mph, 240km/h)
 * Climb rate 1,580ft/min (8.03m/s)
 * Service ceiling 12,800ft (3,901m)
 * Hover ceiling ~9,000ft (2,743m)
 * Fuel Capacity 188+48US gal (710+182L)
 * Range 324nm (372mi, 600km)
 * Empty Weight 4,555lb (2,066kg)
 * Maximum Take-off Weight 7,848lb (3,560kg)