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Fuselage length 42.1 ft (nose tip to vertical fin tip)
Rotor span 57.2 ft (tip to tip, max. diameter)
Maximum height 12.75 ft (vertical fin)
Design gross Weight 13,000 lbs
Maximum gross Weight 15,000 lbs
Useful load at design gross 2,927 lbs
Power Plant Two Lycoming LTC1K-4K free turbine engines (modified versions of the standard Lycoming T53-L-13B)
Estimated cruise speed 345 mph at 16,500 ft
Estimated maximum speed 375 mph at 16,500 ft
Range 800Km
Service Ceiling 8,8400m
Crew 2

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