BRAND and MODEL
MCDONNELL DOUGLAS MD-600N
TYPE
Seven/eight-seat utility helicopter
ORIGIN
United States of America
ENGINE
One 448 kw (600 shp) Allison 250-C47 turboshaft
SPECIFICATIONS
Rotor diameter: 8.38 m (27 ft 6 in)
Length: 11.25 m (36 ft 10¾ in)
Rotor disc area: 55.18 m² (594 sq ft)
Max speed: 282 km/h (175 mph)
Max cruising speed at sea level: 248 km/h (154 mph)
Max rate of climb at sea level: 518 m/min (1,700 ft/min)
Max operating altitude: 6,100 m (20,000 ft)
Hovering ceiling in ground effect: 3,200 m (10,500 ft)
Max range at sea level: 620 km (385 miles)
Endurance: 3 hrs 42 mins
Empty weight: 875 kg (1,930 lb)
Loaded weight: 1,859 kg (4,100 lb)
PHOTO
Airliners.net:Source of phothograph
