Piaggio P.23R

An entirely new design, bearing little resemblance to the original P.23, the Piaggio P.23R of 1936 had a pencil-shaped fuselage, a cantilever low-set wing with straight taper, and was powered by three 671kW Isotta Fraschini Asso XI R V-12 engines in sleek cowlings.

Intended purely as a record-breaker, the P.23R had a crew of two seated side-by-side in individual cockpits, each with its own windscreen and first flew in 1936.

Later modified by the installation of three 746kW Piaggio P.XI RC.40 radials, and with an enclosed canopy over each cockpit and revised main landing gear, the P.23R was used on 30 December 1938 to establish new world records, carrying a payload of 5000kg over distances of 1000km and 2000km at an average speed of 404km/h.

Although the P.23R appeared in Allied wartime recognition manuals as a potential bomber, development of the type had already been abandoned in 1939.

Engine: 3 x Isotta-Fraschini Asso XI R, 671kW

Piaggio P.23

Built to fly the North Atlantic, with potential for development as a commercial transport, the Piaggio P.23 had inverted-gull shoulder-mounted wings and was powered by four 671kW Isotta Fraschini Asso XI R V-12 engines mounted in tandem pairs and driving two tractor and two pusher propellers. It had retractable main landing gear units and twin fins and rudders. A distinctive feature was the ‘avion marin’ boat-type hull underside to the fuselage, intended to assist in an emergency if the aircraft had to alight on the sea.

Maximum take-off weight was 18,400kg and maximum speed a claimed 400km/h; at a cruising speed of 300km/h its range was estimated to be 5100km. However, no transatlantic flight was made and the aircraft was dismantled soon after its appearance in 1935.

Engine: 4 x Isotta-Fraschini Asso XI R, 671kW
Max take-off weight: 18400 kg / 40565 lb
Max. speed: 400 km/h / 249 mph
Range: 5100 km / 3169 miles

Piaggio P.16

The Piaggio P.16 three-engine heavy bomber of 1934 was distinguished by a thick-section semi-elliptical wing set at shoulder height, and of inverted gull configuration. Defensive armament comprised four 7.62mm machine-guns located in the wing leading edge, in a retractable dorsal turret and in the rear fuselage beneath the high-positioned single fin and rudder. Largely of metal construction, the P.16 had retractable main landing gear units and a non-retractable tailwheel with a spat-type fairing. The bomb-aimer’s compartment was located in the underside of the fuselage, just behind the central engine.

Armament: 4 x 7.62mm machine-guns

Piaggio P.8

A parasol-wing single-seat floatplane, the small Piaggio P.8 reconnaissance aircraft of 1928 was intended, like its rival the Macchi M.53, to be stored in a cylindrical container aboard submarines of the large ‘Ettore Fieramosca’ class. It was designed to be assembled rapidly for deployment at sea on patrol or reconnaissance; after being recovered it could as easily be dismantled and re-stowed in its container. Powered by a 56kW Blackburn Cirrus II engine, it had a maximum speed of 135km/h.

Engine: 1 x Blackburn Cirrus II, 56kW
Max. speed: 135 km/h / 84 mph

Piaggio P.7 / Piaggio-Pegna P.c.7

A truly remarkable design, the Piaggio P.7 or Piaggio-Pegna P.c.7 was built for the 1929 Schneider Trophy contest. A cantilever high-wing monoplane with long slender fuselage, it had twin hydrofoils instead of floats and was intended to float with the wing resting on the surface of the water. While water-borne it was to be driven by an ordinary marine propeller connected by a shaft and clutch to the rear of the 723kW Isotta Fraschini Special V.6 engine. Once sufficient speed had been attained to lift the aircraft on to the hydrofoils and the normal tractor propeller was clear of the water, this latter propeller would be clutched-in, the marine propeller disengaged, and a conventional take-off would follow.

In practice, problems with the respective clutches prevented the P.c.7 from ever taking off, and although water trials were conducted on Lake Garda by Dal Molin of the Italian Schneider team, the construction of a second aircraft was abandoned.

Engine: 1 x Isotta-Fraschini Special, 723kW / 850 hp
Wingspan: 28 ft 8.5 in
Length: 29 ft
Height: 8 ft
Empty weight: 3093 lb
Loaded weight: 3709 lb
Max take-off weight: 1738 kg / 3832 lb
Crew: 1

Piaggio P.6

In 1927 two parallel, designs were developed to meet an Italian naval requirement for a two-seat catapult-launched seaplane. One was a small flying-boat, the Piaggio P.6bis powered by a single 194kW Isotta Fraschini V.6 engine mounted between the wings and driving a pusher propeller; the other was the P.6 floatplane with a large central float, two wing-tip stabilising floats, and a 288kW A.20 engine in the nose. The two aircraft had identical wing structure, with rigid strut bracing, and each mounted a single defensive machine-gun, that of the flying-boat in the bow, and the floatplane’s in the rear cockpit.

The P.6ter of 1928 was similar to the P.6, but had an engine boosted to 306kW to provide a maximum speed of 195km/h. Wing span was 13.50m and maximum take-off weight 2360kg. A batch of 15 P.6ter floatplanes was built, and the type was used for a period aboard several Italian capital ships and cruisers.

P.6bis
Engine: 1 x 194kW Isotta Fraschini V.6

P.6
Engine: 1 x 288kW A.20

P.6ter
Engine: 1 x Fiat A.20, 306kW
Max take-off weight: 2360 kg / 5203 lb
Wingspan: 13.5 m / 44 ft 3 in
Max. speed: 195 km/h / 121 mph

Piaggio P.3

The Piaggio P.3 Pegna-designed night bomber of 1923 was a two-bay biplane with the lower wing of greater span than the upper. The biplane tail unit incorporated triple fins and rudders, and four 149kW S.P.A. 6A engines were mounted in tandem pairs on the lower wing, driving two tractor and two pusher propellers. Pilot and co-pilot were seated side-by-side in an open cockpit ahead of the wings, and there were gunner’s cockpits in the nose and amidships, the rear gunner also operating a tunnel gun for ventral defence. At a later stage two 306kW Fiat A.20V engines were installed but the P.3 was not accepted by the Regia Aeronautica for quantity production.

Engine: 4 x S.P.A. 6A, 149kW
Wingspan: 24 m / 79 ft 9 in
Max. speed: 185 km/h / 115 mph

Piaggio P.2

The Piaggio P.2 was the first original design for the company by Giovanni Pegna. Constructed at the Sestri Ponente (Genoa) works in 1923, it was a cantilever low-wing monoplane single-seat fighter with a semi-mono-coque fuselage and fixed, divided landing gear. Twin radiators for the 224kW Hispano-Suiza engine were mounted on the fuselage sides just forward of the pilot’s open cockpit, and armament comprised twin synchronised Vickers 7.62mm machine-guns.

Engine: 224kW Hispano-Suiza
Wingspan: 10.5 m / 34 ft 5 in
Armament: 2 x Vickers 7.62mm machine-guns

Piaggio

SA Piaggio & Co, an engineering and shipbuilding company, produced some Caproni aircraft and parts during the First World War at a Finale Ligure factory, but subsequently abandoned aircraft manufacture until it took over Pegna & Bonmartini in 1923. First product was the Piaggio-Pegna pursuit monoplane with Hispano-Suiza engine. Later was associated with Societa di Costruzioni Meccaniche Aeronautiche in license-construction of Domier Wal flying-boats. Built P.32 twin-engined heavy bomber at end of 1930s and several four-engined P.108 heavy bombers during Second World War.

Resumed aeronautical work in late 1946 with conversion of Dakotas for airline service. Built P.136 five-seat twin-engined amphibian, prototype flying in 1948, followed by a series of trainers for the Italian Air Force; the P.149 was also license-built by Focke-Wulf in Germany. Produced the P.166 executive transport in 1957, with two Lycoming engines and pusher propellers, as with the P.136; P.166-DL3 turboprop variant later developed and produced, with final P.166-DL3-SEM Maritime variant for search and surveillance, coastal patrol and other roles still available in 1998, but only to special order. Signed agreement with U.S. Douglas company in 1961 for joint development of light utility aircraft, first flown in 1964. Designated PD.808 and powered by two Bristol Siddeley Viper turbojets, only a small number was built.

The present Rinaldo Piaggio company was formed in February 1964 as a separate concern, but in 1994 was put under insolvency protection; 51 percent shareholding in the company was purchased by Tushav, a Turkish holding company, in mid-1998, and protection was thereafter lifted. P.180 Avanti twin-pusher turboprop business aircraft flown September 1986, but only 43 production aircraft ordered; turbofan derivative may be developed. Has manufactured components for Aeritalia/Alenia, AMX International, Dassault and Panavia.
In 1998 three Italian industrial families bought the debt-free assets from the Government and formed Piaggio Aero Industries SpA.

In 2024 Italy approved the sale of Piaggio Aerospace to the Turkish unmanned combat aerial vehicle (UCAV) producer Baykar. In 2023, Baykar ranked among the top 10 exporters in Türkiye across all sectors, racking up $1.8 billion in exports. Türkiye dominates 65% of the global unmanned aerial vehicle (UAV) export market, with Baykar alone holding nearly 60% of the market – three times the size of its closest US competitor. In recent years, Baykar has generated more than 90% of its revenues from exports, delivering Bayraktar TB2 UCAVs and Bayraktar AKINCI UCAVs to 35 countries.