BRAND and MODEL
BELL 212 EAGLE SINGLE
TYPE
Utility helicopter
ORIGIN
United States of America
ENGINE
One 1,343 kw (1,800 shp) Honeywell T53-17 or T53-BCV turboshaft
SPECIFICATIONS
Fuselage length: 12.92 m (42 ft 4 in)
Overall length with rotor and tail rotor turning: 17.46 m (57 ft 3 in)
Fuselage width: 2.43 m (8 ft)
Height: 3.9 m (12 ft 8 in)
Never exceed speed: 241 km/h (150 mph)
Economical cruising speed: 204 km/h (127 mph)
Service ceiling: 6,096 m (20,000 ft)
Hovering ceiling at max gross weight at sea level: 2,377 m (7,800 ft)
Rate of climb at 120 km/h (75 mph): 433 m/min (1,420 ft/min)
Fuel capacity standard tank: 834 litres (179 Imp gals)
Fuel capacity of auxiliary or ferry tank: 681 litres (150 Imp gals)
Max range with standard fuel: 622 km (387 miles)
Range with auxiliary fuel no reserves: 1,156 km (718 miles)
Endurance: 3.07 hrs
Empty weight: 2,722 kg (6,000 lb)
Useful load: 2,363 kg (5,210 lb)
Cargo hook capacity: 2,041 kg (4,500 lb)
Loaded weight: 5,080 kg (11,200 lb)
PHOTO
Airliners.net:Source of phothograph
