RAND and MODEL
BELL 222
TYPE
Light utility helicopter
ORIGIN
United States of America
ENGINE
Two 510 kw (684 shp) Avco Lycoming LTS 101-750C-1 turboshafts
SPECIFICATIONS
[Bell 222UT]
Rotor diameter:12.8 m (42 ft)
Fuselage length:12.85 m (42 ft 2 in)
Height:3.51 m (11 ft 6 in)
Main rotor disc area:128.7 m² (1,395.4 sq ft)
Max speed at sea level:278 km/h (172 mph)
Max speed at 1,220 m (4,000 ft):289 km/h (179 mph)
Economical cruising speed at sea level:246 km/h (153 mph)
Max rate of climb:512 m/min (1,680 ft/min)
Service ceiling:4,815 m (15,800 ft)
Range with max fuel at 1,220 m (4,000 ft) and 20 mins reserve:691 km (429 miles)
Empty weight:2,210 kg (4,874 lb)
Loaded weight:3,742 kg (8,250 lb)
PHOTO
hangar67.com:Source of phothograph
