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General characteristics
Crew:
1-4
Capacity: 3,880 lb including 14 troops, or 6 stretchers,
or equivalent cargo
Length: 57 ft 1 in (17.40 m) with rotors
Wingspan: 48 ft 0 in (14.63 m)
Width: 8 ft 7 in (2.62 m) (Fuselage)
Height: 14 ft 5 in (4.39 m)
Empty weight: 5,215 lb (2,365 kg)
Gross weight: 9,040 lb (4,100 kg)
Max takeoff weight: 9,500 lb (4,309 kg)
Powerplant: 1 × Lycoming T53-L-11 turboshaft,
1,100 shp (820 kW)
Main rotor diameter: 48 ft 0 in (14.63 m)
Performance
Maximum speed:
135 mph (217 km/h; 117 kn)
Cruise speed: 125 mph (109 kn; 201 km/h)
Range: 315 mi (274 nmi; 507 km)
Service ceiling: 19,390 ft (5,910 m) (Dependent on environmental
factors such as weight, outside temp., etc)
Rate of climb: 1,755 ft/min (8.92 m/s)
Power/mass: 0.15 hp/lb (0.25 kW/kg)
Armament
Variable, but may include a combination
of:
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