 First flew on 23 December 1991. Certification and initial deliveries took place in 1994. Using intermeshing main rotors, no tail rotor is required. Kaman K-Max Engine: Textron Lycoming T 5317 A1, 1479 shp Instant pwr: 1118 kW. Length: 51.837 ft / 15.8 m Height: 13.583 ft / 4.14 m Rotor diameter: 48.228 ft / 14.7 m Max take off weight: 11501.3 lb / 5216.0 kg Weight empty: 4701.1 lb / 2132.0 kg Payload: 2722 kg Max. speed: 100 kts / 185 kph Max cruise: 100 kts Service ceiling: 25000 ft / 7620 m Crew: 1 Payload: max 2700kg ext. |
