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Aircrafts in data base:
865
May 06/2008
1 new model
in aircraft
encyclopedia
Several data updated
Agusta / AgustaWestland A109 / AW109Photo ©: Karsten Palt
A109 / AW109 Light Utility Helicopter | Crew | 1-2 | | Passengers | 6-7 | | | ||
| Propulsion | 2 Turboshaft Engines | | Engine Model | Allison
250-C20B | | Engine Power (each) | 313 kW | 420 shp | | | ||
| Speed | 311 km/h | 168 kts | | Service Ceiling | 4.572 m | 15.000 ft | | Range | 948 km | 512 nm | | | ||
| Empty Weight | 1.418 kg | 3.126 lbs | | max. Takeoff Weight | 2.600 kg | 5.732 lbs | | | ||
| Rotor Blades (main/tail) | 4/2 | 4/2 | | Main Rotor Diameter | 11,00 m | 36,1 ft | | Tail Rotor Diameter | 2,03 m | 6,7 ft | | Rotor Disc Area | 95,0 m² | 1023 ft² | | Length (Fuselage) | 11,45 m | 37,6 ft | | Length | 13,04 m | 42,8 ft | | Height | 3,40 m | 11,2 ft | | | ||
| First Flight | 04.08.1971 | | Production Status | in production | | | ||
| ICAO Code | A109 | | FAA TCDS | H7EU | | EASA TCDS | R.005 | | | ||
| Data for (Version) | Agusta A109A Mk II | | Variants | A109LUH, A109 Power, A109S Grand |
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