Kaman Aerospace K-1200 K-Max
Light Utility Helicopter
The Kaman K-1200 K-Max is a single-engine single-seat light utility helicopter with intermeshing rotors produced by the US-American manufacturer Kaman Aerospace Corporation. The K-Max operates as a medium lift helicopter and is able to lift loads of max. 2720 kg (6000 lbs). The K-Max is used for external load operations as firefighting, heli-logging, construction and spraying.
Propulsion | 1 Turboshaft Engine |
Engine Model | Lycoming T53-17A-1 |
Engine Power | 1342 kW | 1800 shp |
Speed | 185 km/h | 100 kts 115 mph |
Service Ceiling | 4.572 m | 15.000 ft |
Range | 556 km | 300 NM 345 mi. |
Empty Weight | 2.334 kg | 5.146 lbs |
max. Takeoff Weight | 5.443 kg | 12.000 lbs |
Rotor Blades (main/tail) | 4 |
Main Rotor Diameter | 14,73 m | 48 ft 4 in |
Rotor Disc Area | 170,4 m² | 1834 ft² |
Length (Fuselage) | 12,73 m | 41 ft 9 in |
Length | 18,85 m | 61 ft 10 in |
Height | 4,14 m | 13 ft 7 in |
First Flight | 03/1992 |
Production Status | in production |
ICAO Code | KMAX |
FAA TCDS | TR7BO |
Data for (Version) | Kaman K-1200 K-Max |