Cantieri Aeronautici Piaggio Piaggio P.111

By AviatorDB Data Bureau

Cantieri Aeronautici Piaggio Piaggio P.111 — research

Overview

The Piaggio P.111 was a pioneering Italian high-altitude research aircraft notable for its advanced pressurized cabin.

Aircraft Information

ICAO Code
PGG
Manufacturer
Cantieri Aeronautici Piaggio
Model
Piaggio P.111
Primary Role
Research
Engine Type
Radial

Technical Data

Engine Model
P.XII R.C.100/2v
Production Years
1939-1941
Units Produced
1
First Flight
1941-04-09
Warbird
Yes
Notable Operators
Regia Aeronautica

The Piaggio P.111 was a pioneering Italian high-altitude research aircraft notable for its advanced pressurized cabin. Manufactured by Cantieri Aeronautici Piaggio as a single experimental prototype, this all-metal, twin-engine low-wing monoplane served as a technical testbed for the Regia Aeronautica during the early 1940s.

The Piaggio P.111 was an experimental aircraft developed in Italy during the late 1930s to explore the frontiers of high-altitude flight. The project was initiated in 1937 under the leadership of engineer Giovanni Casiraghi. In 1938, the Regia Aeronautica (Italian Royal Air Force) formally contracted Piaggio to produce a three-seat, twin-engine aircraft designed for long-range, high-altitude light bombing operations. Construction of the prototype began on April 18, 1939, at the Cantieri Aeronautici Piaggio works located in Finale Ligure.

As the aircraft progressed through development, the Regia Aeronautica shifted its requirements, cancelling the P.111's role as a bomber. Instead, the aircraft was repurposed as a specialized high-altitude research platform. The primary objective of this transition was to allow Italian engineers to study and develop pressurized cabin technology, a critical advancement for the era. This research was intended to provide a foundation for future high-altitude aircraft and potential transatlantic airliners, although the onset of war prevented these subsequent designs from being realized.

Technically, the P.111 was an all-metal low-wing monoplane powered by two Piaggio P.XII R.C.100/2v 18-cylinder air-cooled radial piston engines, each producing 1,000 hp. The aircraft featured a streamlined fuselage and a service ceiling of approximately 11,997 meters (roughly 39,350 feet), which was exceptionally high for a twin-engine aircraft of its size in the early 1940s. Other performance specifications included a maximum speed of 575 km/h, a cruising speed of 449 km/h, and a normal range of 1,659 km. The airframe had a wingspan of 17.30 meters, a length of 12.39 meters, and a maximum take-off weight of 7,590 kg.

The P.111 made its maiden flight on April 9, 1941. Throughout its short career, it was used exclusively for research and testing by the Regia Aeronautica and did not see active combat during World War II. After completing approximately 110 test flights, the aircraft was grounded in early 1943 and subsequently scrapped. No airframes survived the conflict. The legacy of the P.111 remains technical; it stands as a significant example of Italy's early efforts to master pressurization and high-altitude aviation.

Operators

Regia Aeronautica