Avanti EVO – New Delivery Position
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Aircraft Specification
The Avanti EVO is a business aircraft like no other. Having learnt everything there is to know about aviation in its 100-year history, Piaggio Aerospace rewrote the rulebook to combine renowned Italian design with superb craftsmanship in an aircraft that simply works best for business.
The Avanti EVO is refreshingly different – not just in terms of its head-turning looks, but also in terms of superior performance and comfort. The EVO is very much a business aircraft for the future, built on the best traditions of the past and today’s state-of-the-art technology.
The EVO is one of the most environmentally friendly aircraft on the market, with reduced emissions and aircraft noise making it a logical choice. The fastest twin turboprop ever made – faster than some jets – the Avanti EVO achieves greater speed without compromising operating costs, running at up to 30% less than a jet of the same size. The spacious cabin is truly an office in the sky, allowing passengers to maximize their working day while also arriving fresh, prepared and ready to do business.
Unveiled in 2014, customer deliveries of the Avanti EVO began in 2015, with production now ramped up at a new facility in Italy. The benefits of ownership are considerable. As well as flying one of the smartest, most efficient, aircraft in the skies, Piaggio Aerospace’s expansive customer support and service network minimizes downtime while also keeping costs under control through an innovative fixed-fee program.THIS IS THE AVANTI EVO ADVANTAGE.
PIAGGIO AEROSPACE AVANTI EVO SPECIFICATIONS
EXTERNAL DIMENSIONS | ||
Span | 14.345 m | 47.06 ft |
---|---|---|
Length | 14.408 m | 47.27 ft |
Height | 3.980 m | 13.06 ft |
CABIN DIMENSIONS | ||
Height | 1.75 m | 5.74 ft |
Width | 1.85 m | 6.07 ft |
Length | 4.55 m | 14.92 ft |
Max Seating Capacity | 8+2 crew | |
Typical Executive Payload | 6+1 crew | |
BAGGAGE COMPARTMENT | ||
Volume | 1.00 m3 | 35 ft3 |
Length | 1.70 m | 5.58 ft |
Maximum Weight | 159 Kg | 350 lb |
PRESSURIZATION | ||
Differential | 0.62 bar | 9.0 psi |
Sea Level cabin up to | 7,315 m | 24,000 ft |
WEIGHTS | ||
Max Take-off Weight | 5,489 Kg | 12,100 lb |
Max Landing Weight | 5,216 Kg | 11,500 lb |
Max Zero Fuel Weight | 4,445 Kg | 9,800 lb |
Standard Empty (Shuttle Configuration) | 3,561 Kg | 7,850 lb |
Max Fuel Capacity | 1,271 Kg | 2,802 lb |
Fuel with Max Net Payload | 1,066 Kg | 2,350 lb |
Max Net Payload | 794 Kg | 1,750 lb |
Net Payload with Max Fuel | 589 Kg | 1,298 lb |
Max Fuel Capacity (Increased Range Config.) | 1,451 Kg | 3,200 lb |
POWERPLANT | ||
2 x Pratt & Whitney Canada PT6A–66B Engines 850shp/634kW each (ISA, sea level), at-rated from 1,630hp | ||
2 x Hartzell ve-scimitar blades low noise Propellers | ||
PERFORMANCE | ||
Maximum Speed (at 31,000ft ISA) | 745 km/h | 402 KTAS |
MMO | 0.70 Mach | |
Max Range (NBAA IFR, Standard Conf.) | 2,759 km | 1,490 NM |
Max Range (NBAA IFR, Increased Range Conf.) | 3,278 km | 1,770 NM |
Service Ceiling | 12,497 m | 41,000 ft |
Rate of Climb (MTOW, 12,100lb) | 844 mpm | 2,770 fpm |
Take-Off Distance (SL, ISA, to clear 50ft) | 972 m | 3,190 ft |
Landing Distance (SL, ISA, 50ft, MLW, no reverse) | 1,000 m | 3,282 ft |