Design and Development
The PZL P.24 was developed as an export version of the PZL P.11, a gull-wing all-metal fighter designed by Zygmunt Puławski. The P.11 was powered with a license-built Bristol Mercury engine. The license did not permit export sales, so the French Gnome-Rhône company proposed using their engines in the P.11. The first P.24/I prototype, based on the P.11a and powered by a Gnome-Rhône 14Kds 760 hp (570 kW) engine, was flown in May 1933. The second P.24/II prototype, named the "Super P.24", set a world speed record for radial engine-powered fighters (414 km/h). The third P.24/III prototype was the "Super P.24bis" with a more powerful 14Kfs engine. The type was shown at the Paris air show in 1934 attracting great interest from the participants.
The aircraft was conventional in layout, with high wings. It was all-metal and metal-covered. The wings had a gull-wing shape, with a thin profile close to the fuselage, to provide a good view for the pilot. This configuration was developed by Zygmunt Pulawski and called "the Polish wing". The canopy was closed (apart from prototypes). An internal 360 liter fuel tank in the fuselage could be dropped in case of fire emergency. It had conventional fixed landing gear, with a rear skid.
The armament was a combination of 20 mm Oerlikon FF cannon and 7.92 mm Colt-Browning machine guns in the wings.
- P.24A, P.24E and P.24F had two cannon and two machine guns.
- P.24B, P.24C and P.24G had four machine guns.
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