BRAND and MODEL
BELL 407
TYPE
General-purpose utility helicopter
ORIGIN
United States of America
ENGINE
One 606 kw (813 shp) Rolls-Royce –Allison 250-C47B turboshaft
SPECIFICATIONS
Rotor diameter:10.67 m (35 ft)
Overall length rotor turning:12.77 m (41 ft 8 in)
Height:3.56 m (11 ft 8 in)
Main rotor disc area:89.4 m² (962.1 sq ft)
Max cruising speed at 1,219 m (4,000 ft):243 km/h (151 mph)
Max cruising speed at sea level:237 km/h (147 mph)
Economical cruising speed at 1,219 m (4,000 ft):213 km/h (132 mph)
Hovering ceiling in ground effect:3,719 m (12,200 ft)
Service ceiling:5,697 m (18,690 ft)
Max range:665 km (413 miles)
Empty weight:1,178 kg (2,598 lb)
Loaded weight:2,268 kg (5,000 lb)
PHOTO
helicopterprivateservices.com:Source of phothograph
