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BELL 205A-1 ++

The Bell 205A-1 ++ is a single engine, two blade, medium aircraft with a max take off weight of 10,500 lbs. This helicopter has consistently proven its capabilities supporting missions in areas of high altitude, high temperature and turbulent mountain environments.

Specifications

Length: 42 ft 1 in (12.8 m)


Rotor diameter: 48 ft 4 in (14.63 m)


Height: 14 ft 6 in (4.43 m)


Disc area: 2,492 ft² (231.54 m²)


Range: 300 nm (556 km)


Maximum speed: 120 kn (138 mph)


Cruise speed: 111 kn (125 mph) 


Service ceiling: 20,000 ft 


Rate of Climb: 1,755 fpm @ max gross weight

Engines: Lycoming T53-17


Horsepower: 1,500 shp


Crew: 1/2 (pilots)


Capacity: 9 passengers


Empty weight: 5,900 lb (2,675 kg)


Max. gross weight: 9,500 lb (4,310 kg)


Internal Weight capacity: 10,200 lb (4,626 kg)


External Weight capacity: 10,500 lb (4,762 kg)


Capabilities: Passenger/cargo transport, external lifts, fire suppression.

CALL 800.521.5130 FOR NATIONWIDE SERVICE