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Aircraft Type(s) | Twin turboprop three-surface aircraft fixed foreplane | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Parent Company | BAYKAR (Türkiye) | ||||||||
Manufacturer(s) | Piaggio Aerospace (Italy) | ||||||||
Usage Purposes | experimental performance analysis radio calibration passenger transport military patrol ambulance UAV VIP passenger transport and light cargo | ||||||||
First Flight Date | 23 September 1986 | ||||||||
Entry into Service Date | 30 September 1990 | ||||||||
Production Number | 246 (December 2020) | ||||||||
User Nations | United Arab Emirates Russia Poland Canada Italy Türkiye | ||||||||
Engine Variants | PT6A-66B PT6A-66 | ||||||||
Status | Active - In production | ||||||||
The Piaggio P.180 family is a group of executive/VIP light transport aircraft designed by Piaggio Aerospace and manufactured in Italy. These aircraft are known for their innovative design and advanced engineering. The P.180 is equipped with twin turboprop engines mounted on the fuselage, positioned in a pusher configuration. This arrangement enhances the aircraft’s aerodynamic efficiency while providing a significantly quieter cabin environment.
Unlike most conventional aircraft, its design employs a three-surface configuration consisting of a small fixed canard surface, a conventional horizontal tail, and the main wing. This design ensures balanced flight characteristics, though it is often mistaken for a traditional canard configuration. Additionally, the main wing spars pass behind the passenger cabin, offering a significant advantage in interior layout.

P.180 EVO of the Piaggio P.180 Family (Piaggio Aerospace)
Other members of the Piaggio P.180 family cater to diverse user needs by retaining the core features of the base model while offering a wider cabin, extended range, and enhanced technological capabilities. The aircraft are recognized for their fast and efficient transport performance, as well as their luxurious passenger cabins and low operating costs.

Model of the P.180 EVO Displayed at IDEF 2025 (Author’s Photo)
The design and technological features of the P.180 prioritize flight safety, comfort, and efficiency, establishing it as one of the most modern business jets today. These aircraft offer an ideal solution for both commercial and private use, making them popular for VIP transport, executives, and private business travelers. Additionally, they can carry up to nine passengers in a pressurized cabin up to 24,000 feet and are flown by one or two pilots.
Furthermore, the Avanti, with this design, is recognized as the fastest propeller-driven aircraft in the world by has been listed【1】.

Piaggio P.180 Avanti II with M-GCAP Tail Code Displayed at IDEF 2025 Static Area (Anadolu Agency)
In the 1980s, several manufacturers sought to develop fast and efficient business jets targeting large corporations. One such model was the Piaggio P.180 Avanti. Design work began in 1979; wind tunnel tests were conducted in Italy and the United States in 1980 and 1981. The project was led by Prof. Jan Roskam from University of Kansas and Prof. Jerry Gregorek from Ohio State University.

Left: Prof. Jan Roskam and Right: Prof. Jerry Gregorek (Jawhawk Global, Celestis)
The aircraft’s design was planned with three lifting surfaces: a fixed forward surface, a main wing, and a T-tail. This configuration provided low drag and high efficiency. In 1982, Piaggio’s chief engineer Alessandro Mazzoni filed a patent for the design. In 1983, a collaboration with Learjet accelerated fuselage development. Learjet’s influence is clearly visible in the Avanti’s slanted forward windshield and delta-shaped tail surfaces, added to enhance flight stability and prevent stall conditions.
Despite Learjet’s withdrawal from the project in 1986 due to financial difficulties, Piaggio continued development and conducted the aircraft’s first flight on 23 September 1986. The aircraft received certification from Italy and the United States in 1990. The first 12 fuselages were produced in Kansas and then shipped to Italy for final assembly. Although the project was temporarily halted in 1994, it was revived in 1998 under the leadership of Piero Ferrari.

Ferrari and Piaggio Aerospace Executives at the Dubai Show 2007 (Flight Global)
Launched in 2005, the Avanti II featured more powerful PT6A-66B engines and digital “glass cockpit” avionics. This model outperformed many jets in fuel efficiency and performance. It was equipped with modern flight safety systems such as TCAS, TAWS, and weather radar. Compared to the Beechcraft King Air 200 using the same engines, the Avanti II was approximately 100 knots faster. This speed advantage became one of the key factors establishing it as the “fastest twin-engine civil turboprop”.

Piaggio P.180 Avanti II with M-GCAP Tail Code Displayed at IDEF 2025 Static Area (Anadolu Agency)
The unmanned variant developed in 2013, the P.1HH HammerHead, experienced a crash in 2016 following test flights. Production was moved to the new Albenga facility in 2015, and the first EVO model was delivered in 2016.

Piaggio P.1HH-HammerHead Variant (Piaggio Aerospace)

Cockpit View of the Piaggio P.180 Avanti II in “GPU on / Hot and Bright” Position at IDEF 2025 Static Area (Author’s Photo)
In 2018, Piaggio Aerospace declared concordato due to financial difficulties. Avanti deliveries dropped from 30 aircraft in 2008 to just 3 in 2018. In the same year, the Italian government announced nearly 700 million euros in orders and support to rescue the project. These included new aircraft, modernization programs, engine maintenance services, and unmanned systems. As of 2020, a total of 246 Avantis had been produced and the fleet had surpassed 1 million flight hours. The aircraft remain in active service across Europe, the Americas, Asia-Pacific, and Africa.

Cabin View of the Piaggio P.180 Avanti II Displayed at IDEF 2025 Static Area (Author’s Photo)

Plan Views of the Piaggio P.180 Avanti from Different Angles (Doc8643)
The Avanti’s counter-rotating turboprop engines are mounted to a high-efficiency main wing located behind the cabin. The aircraft features a three-lifting-surface design comprising a fixed forward surface (canard-like), a main wing, and a T-tail. Flaps on the forward surface open automatically in coordination with the main wing flaps, reducing the load on the tail surface and enabling a smaller wing and tail design. This configuration was patented in 1982 and provides a more spacious cabin than other aircraft in its class.

Piaggio P.180 Avanti EVO Cabin Width Comparison (Piaggio Aerospace)
The forward surface stalls before the main wing, inducing a nose-down response that enhances flight safety. Additionally, the slight sweep and negative dihedral of the forward surface optimize airflow to the engine inlets and tail surfaces. The fuselage shape is specially designed to generate 20% of the total lift through laminar flow, with the remaining 80% generated by the forward and rear surfaces.
The Avanti II is significantly more efficient than small jets flying at the same speed and altitude. Laminar flow is preserved up to 50% better than in conventional turboprops. Its specific range is 3.1 km/kg, approximately 70% more efficient than typical jets. However, these advantages are achieved at relatively lower speeds such as 315 KTAS and FL410.
Cabin noise levels are very low (approximately 68 dBA) because the engines and propellers are located at the rear. However, external noise levels are higher. The high-frequency noise generated by the pusher configuration has caused complaints at some airports. For example, the aircraft has been criticized for noise at Naples (Florida) and Aspen (Colorado) airports.
Piaggio P.180 Avanti II with M-GCAP Tail Code Registered in the Isle of Man (YouTube)
At sea level, the maximum takeoff distance is 869 m and the landing distance is 872 m. In 2008, 30 aircraft were delivered, but by 2013, this number had dropped to 2.
The range of the most advanced EVO variant is 1,809 nautical miles.

Piaggio P.180 EVO Range Characteristics (Piaggio Aerospace)
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[1]
Piaggio Aerospace, “Piaggio Aerospace: the P.180 fleet reaches one million flight hours,” basın bülteni, 1 Aralık 2020, https://www.piaggioaerospace.it/en/media/archivio/news/2020-12-01-piaggio-aerospace-the-p180-fleet-reaches-one-million-flight-hours
Aircraft Type(s) | Twin turboprop three-surface aircraft fixed foreplane | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Parent Company | BAYKAR (Türkiye) | ||||||||
Manufacturer(s) | Piaggio Aerospace (Italy) | ||||||||
Usage Purposes | experimental performance analysis radio calibration passenger transport military patrol ambulance UAV VIP passenger transport and light cargo | ||||||||
First Flight Date | 23 September 1986 | ||||||||
Entry into Service Date | 30 September 1990 | ||||||||
Production Number | 246 (December 2020) | ||||||||
User Nations | United Arab Emirates Russia Poland Canada Italy Türkiye | ||||||||
Engine Variants | PT6A-66B PT6A-66 | ||||||||
Status | Active - In production | ||||||||
Henüz Tartışma Girilmemiştir
"Piaggio P.180 Fleet" maddesi için tartışma başlatın
Historical Development
Piaggio P.180 Family – Design, Efficiency, and Noise Characteristics
Design and Aerodynamics
Flight Safety and Aerodynamic Details
Fuel Efficiency and Comparisons
Interior and Exterior Noise
Performance
Range