| Piaggio P.32 | |
|---|---|
 | |
| General information | |
| Type | Medium bomber |
| Manufacturer | Piaggio Aero |
| Designer | |
| Primary user | Regia Aeronautica |
| Number built | 28 + 1 prototype[1] |
| History | |
| Introduction date | 1938 |
| First flight | 1936 |
| Retired | 1939 |
ThePiaggio P.32 was an Italianmedium bomber of the late 1930s, produced by Piaggio, and designed byGiovanni Pegna. It was a modern design for its time, but was a failure due to lack of powerplants commensurate with its high wing loading.
The P.32 was atwin-enginemonoplane with a crew of five or six. The main structure was of wood, with a glazed nose, lowcockpit, twintailfins, and a distinct 'banana' shape to thefuselage. It was armed with a dorsalturret with two 7.7 mm (0.303 in)machine guns, a ventral turret, a single machine gun in the nose, and it could carry a 1,600 kg (3,527 lb) bomb load.
Utilizing their experience of designing experimental and record-breaking aircraft like thePiaggio P.16,Piaggio P.23M, andPiaggio P.23R, Piaggio designed the P.32 with very small wings for its size. This meant a highwing loading, which required Handley-Pageleading edge slats anddouble trailing-edge flaps to provide enough lift on takeoff and landing.
The development of this aircraft began with the contest announced by theRegia Aeronautica (Italian Air Force) in 1934. The P.32 was one of many contenders, and the most modern.
Theprototype first flew in 1936, and was tested atGuidonia, leading to an order for 12 aircraft, followed by a second order for five. These aircraft were fitted with the 615 kW (825 hp)Isotta Fraschini Asso XI.RC inlineV-12 engines, and were designated theP.32 I.
In early 1937, the P.32 Is were assigned to XXXVIIGruppo BT, 18Stormo. The advanced wing design meant that they could be flown only by specially trained crews, but the aircraft was found to be fatally underpowered, with a maximum speed of only 386 km/h (240 mph; 208 kn), and then only with no bombs or defensive weapons carried. They were unable to fly on only one engine, and theirhandling qualities were inferior to theSM.79 andBR.20.
TheP.32 II, fitted with more powerful 750 kW (1,006 hp)Piaggio P.XI R.C.40radial engines was tested, and 12 were delivered in early 1938. The more powerful engines gave a better rate of climb, but the increased weight meant there was no improvement in maximum speed, while the range dropped from 1,950 to 1,700 km (1,210 to 1,060 mi; 1,050 to 920 nmi) because of higher fuel consumption.
TheP.32 Bis was a redesign that brought the empty weight of the aircraft down from 6,355 to 5,700 kg (14,010 to 12,566 lb) by reducing its overall size slightly. This gave it a top speed of 378 km/h (235 mph; 204 kn) and a ceiling of 6,300 m (20,700 ft) with the Isotta Fraschini Asso XI engines, and 420 km/h (261 mph; 227 kn) and a ceiling of 8,000 m (26,000 ft) with thePiaggio P.XI R.C.40 engines. However, the prototype crashed on 25 February 1938, killing the test pilot, leading to the cancellation of further development.
The P.32 Is and IIs were taken out of service in April 1938 and were used astraining aircraft. In 1939, a P.32 crashed, killing the entire crew. There is no further information about the fate of the remaining aircraft, and most likely they were scrapped soon afterwards.
Data fromItalian Civil and Military Aircraft 1930-1945[4]
General characteristics
Performance
Armament
Aircraft of comparable role, configuration, and era
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