Kaman Aerospace K-1200 K-Max
Photo ©: Thomas Schmid (www.tsis.ch/heli)
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.
| Crew | 1 | |
| 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 | 4 |
| Main Rotor Diameter | 14,73 m | 48,3 ft |
| Rotor Disc Area | 170,4 m² | 1834 ft² |
| Length (Fuselage) | 12,73 m | 41,8 ft |
| Length | 18,85 m | 61,8 ft |
| Height | 4,14 m | 13,6 ft |
| First Flight | 03/1992 | |
| Production Status | in production | |
| ICAO Code | KMAX | |
| FAA TCDS | TR7BO | |
| Data for (Version) | Kaman K-1200 K-Max | |
| Weblinks | Extras |
| Kaman Aerospace |
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