Specification
The numbers and technical information of the P180 Avanti II will give you an idea of its excellence and its "difference" not only from aircraft in the same class, but also from many turbojets as well. The spaciousness and comfort of the cabin, the versatile passenger configurations, the external dimensions and the weights, the record performance in terms of both speed and distance of takeoff and landing, and the power of the engines are all world-class qualities that can be appreciated even more when they are evaluated together with the technical specifications of the P180 Avanti II. Roll the mouse pointer over the image of the aircraft depicted above and discover the supremacy of the P180 Avanti II's numbers and technical information.
Performance
Maximum cruising speed
402 KTAS/745 km/h at 31,000 ft/9448 m
Takeoff distance
S.L. - ISA 2,850 ft (869 m)
Landing distance
S.L. - ISA 2,860 ft (872 m)
Rate of climb
S.L. - ISA 2,950 ft/min (899 m/min)
Service ceiling
41,000 ft/12,500 m
Maximum IFR Range
1,470 nm/2,722 km
Differential pressurization
9.0 psi/ 0.62 bar
S.L. Cabin to:
24,000 ft / 7315 m
External dimensions
Wingspan
46.03 ft/14.03 m
Length
47.28 ft/14.41 m
Height
13.06 ft/3.98 m
Cabin dimensions
Height
5.74 ft /1.75 m
Width
6.07 ft/1.85 m
Length
14.93 ft/4.55 m
Configurations
High-density configuration
9 passengers + 2 crew members
Typical executive configuration
7 passengers + 2 crew members
Super VIP executive configuration
6 passengers + 2 crew members
Engines
2 Pratt & Whitney Canada PT6 66-B, with 1630 thermodynamic HP each, derated to 850 SHP
Service Ceiling
41,000 ft/12500 m
One engine ceiling
23,800 ft/7254 m
Weights
Maximum takeoff weight (MTOW)
12,100 lbs/5,489 kg
Standard empty weight
7,800 lbs/3,538 kg
Useful load (including crew)
4,150 lbs/1882 kg
Maximum payload
1,800 lbs/816 kg