Not that you can believe everything on wikipedia. But I did see this. (bold my emphasis)
OH-58A
Data from U.S. Army Aircraft Since 1947
General characteristics
Crew: 1 pilot, 2 pilots, or 1 pilot and 1 observer
Length: 32 ft 2 in (9.80 m)
Rotor diameter: 35 ft 4 in (10.77 m)
Height: 9 ft 7 in (2.92 m)
Empty weight: 1,583 lb (718 kg)
Max takeoff weight: 3,000 lb (1,360 kg)
Powerplant: 1× Allison T63-A-700 turboshaft, 317 shp (236 kW)
Fuselage length: 34 ft 4.5 in (10.48 m)
Performance
Maximum speed: 120 knots (222 km/h, 138 mph)
Cruise speed: 102 knots (188 km/h, 117 mph)
Range: 299 mi (481 km, 260 nmi)
Service ceiling: 19,000 ft (5,800 m)
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