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AGUSTA
AEROSPACE CORPORATION
AGUSTA A109C |
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Las mejoras técnicas adicionadas al A109 C son principalmente en el diseño y construcción de las palas del rotor principal que anteriormente eran metálicas y ahora son de material compuesto, el motor que ahora es un Allison 250C20-R/1, una transmisión principal reforzada y un nuevo tren de aterrizaje. |
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The improvements added over the years wich led to the configuration of the A109 C were mainly dictated by the technical advancement of certain components of the machine, including some of primary importance such as the blades made initially of metal and now of composite materials, the engines which are more powerful Allison 250C20-R/1 units, the highly upgraded transmission system, and the new landing gear. |
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Characteristics |
Information |
Characteristics |
Information |
First
Flight Primer Vuelo |
19?? | Engine Motor |
2 Allison |
Seating
Capacity Plazas |
1 / 7 |
Power Potencia |
450 SHP each |
Empty
Weight Peso Vacío |
3502 Lbs |
Hover
Ceiling O.G.E. Estacionario O.G.E |
8000 Ft |
Maximum
Weight Peso Máximo |
5997 Lbs |
Hover
Ceiling I.G.E. Estacionario I.G.E |
11400 Ft |
Vel.
Cruise Vel. crucero |
147 Kts |
Service
Ceiling Techo de Servicio |
15000 Ft |
V.N.E. V.N.E |
168 Kts |
Maximum
Range (Std) Alcance (Std) |
358 NM |
Thank you to Agusta Corporation
Copyright © 1999 / 2003