HELICÓPTEROS "THE SITE"
AGUSTA AEROSPACE CORPORATION

AGUSTA   A109C

a109c.JPG (7161 bytes)


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.


 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.


Characteristics
Características

Information
Información

Characteristics
Características

Information
Información

First Flight
Primer Vuelo
19?? Engine
Motor

  2 Allison
250C-20R

Seating Capacity
Plazas

1 / 7

Power
Potencia

450 SHP each
380 Cont

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


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