Helicóptero Agusta Westland A109E Power – Ano 2006 – 1835 H.T.
Desfrute de uma nova experiência de viagem com o Agusta A109 Power. Voe a negócios ou lazer para qualquer destino em velocidade, estilo e segurança. Além de seu design e aerodinâmica impressionante, a cabine oferece um ambiente espaçoso, silencioso e luxuoso, equipado com um interior com assento de couro com ar condicionado.
Installed Equipment & Accessories:
- Air Conditioning – Dual Control
- Baggage Extender 1,9m – Lr/rh Hinged Doors
- 08 Ea Headsets Bose X – Rotor Brake
- Aux Fuel Tanks – Retractable Landing Light
- Composit Tail Rotor Blades – Dual Dvd Display In Pax Cabin
Avionics
- Dual Vhf Comm Nav King Kx165 – Pilot & Co-pilot Ehsi
- GPS Garmin 400
- BF Goodrich SKY899
- Wheather Radar System
- Skywatch HP Traffic Advisory
- Cabin Audio System
- Entertaiment System
- Audio System
- KI 209 NAV
- Strob Light
- Spare Wiring
- Realocated DME antenna
- Altitude Management System
A aeronave acima é de terceiro e como tal sujeita a venda prévia e/ou alteração de preço. Dados fornecidos pelo proprietário, sujeitos a verificação.
Agusta A109E Power
Model: AGUSTA A109
Engine Takeoff Power: P&W 640 shp • 206 series
Max Seats: 8
| Weights | ||||
| Max take off (int./ loads) | 2850 / 3000 | kg | 6283 / 6614 | lb |
| Max take off (ext./ loads) | 3000 | kg | 6614 | lb |
| Basic empty weights | 1590 | kg | 3505 | lb |
| Engine Rating (2 x Pratt & Whitney PW206C) | ||||
| Take off power (5 min) | 2 x 477 | kW | 2 x 640 | shp |
| Maximum continuous power | 2 x 423 | kW | 2 x 567 | shp |
| O.E.I. max contingency power (2.5 min) | 546 | kW | 732 | shp |
| O.E.I. max continuous power | 500 | kW | 670 | shp |
| Engine Rating (2 x Turbomeca Arrius 2K1) | ||||
| Take off power (5 min) | 2 x 500 | kW | 2 x 670 | shp |
| Maximum continuous power | 2 x 425 | kW | 2 x 570 | shp |
| O.E.I. max contingency power (2.5 min) | 560 | kW | 750 | shp |
| O.E.I. max continuous power | 500 | kW | 670 | shp |
| Transmission Rating | ||||
| Take off power (5 min) | 671 | kW | 900 | shp |
| Maximum continuous power | 671 | kW | 900 | shp |
| O.E.I. max contingency power (2.5 min) | 478 | kW | 640 | shp |
| O.E.I. max continuous power | 417 | kW | 560 | shp |
| Fuel Capacity | ||||
| 3-cell fuel system | 605 | l | 160 | USgal |
| 4-cell fuel system | 699 | l | 185 | USgal |
| 5-cell fuel system | 835 | l | 221 | USgal |
| Crew | |
| Pilot / Passengers | 1 / 7 |
| External Dimensions | ||||||
| Length (rotors turning) | 13.04 | m | 42 | ft | 09 | in |
| Length (rotors stopped) | 11.45 | m | 37 | ft | 07 | in |
| Width (rotor blades at 45°) | 7.80 | m | 25 | ft | 07 | in |
| Maximum height | 3.50 | m | 11 | ft | 06 | in |
| Main rotor diameter | 11.00 | m | 36 | ft | 11 | in |
| Tail rotor diameter | 1.94 | m | 6 | ft | 04 | in |
| MR tip blade ground clearance | 2.45 | m | 8 | ft | 00 | in |
| Fuselage ground clearance | 0.40 | m | 1 | ft | 04 | in |
| Performance (ISA, 2850 kg / 6283 lb) | ||||
| VNE | 311 | km/h | 168 | kt |
| Max cruise speed | 285 | km/h | 154 | kt |
| Rate of climb | 9.8 | m/sec | 1930 | ft/min |
| Hovering IGE (TOP) | 5059 | m | 16600 | ft |
| Hovering OGE (TOP) | 3596 | m | 11800 | ft |
| Service ceiling (MCP) | 5974 | m | 19600 | ft |
| OEI max service ceiling | 3993 | m | 13100 | ft |
| Max Range* | 932 | km | 503 | nm |
| Max endurance* | 4 h 45 min | |||
(*) With 221 USgal fuel, no reserve, @5000 ft
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