Specifications (K-MAX)
K-1200 orthographical image.svg
Data from K-MAX Performance and Specs[46]
General characteristics
Crew: 1
Capacity: 6,000 lb (2,722 kg) external load
Length: 51 ft 10 in (15.8 m)
Rotor diameter: 48 ft 3 in (14.7m)
Height: 13 ft 7 in (4.14 m)
Empty weight: 5,145 lb (2,334 kg)
Useful load: 6,855 lb (3,109 kg)
Max. takeoff weight: 12,000 lb (5,443 kg)
Powerplant: 1 × Honeywell T53-17 turboshaft, 1341 kW (1,800 shp), flat rated to 1118 kW (1500 shp) for take-off / 1350 shp in flight[47][48])
Performance
Maximum speed: 100 knots (185.2 km/h)
Cruise speed: 80 knots (148.2 km/h)
Range: 267 nm (494.5 km)
Fuel consumption: 85 gallons/hour[12]