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Operators
The only surviving example of a PZL P.24 in the world. Turkish Aviation Museum, Istanbul
A Greek PZL P.24 F/G, 1940. The Δ120 marking shows that the aircraft belonged to Marinos Mitralexis.
Bulgaria - The Bulgarian Air Force ordered 14 PZL P.24Bs in 1937-1938. Bulgaria placed a repeat order for 20 PZL P.24C, to be delivered by the end of 1938. It later ordered 26 PZL P.24Fs, 22 of which were delivered from Poland in July 1939, just before the outbreak of World War II. The remaining four, lacking propellers, were bombed in the Okecie factory in September 1939 by the Germans. Total: 56 PZL P.24B/C/F
Greece - The Royal Hellenic Air Force bought 30 P.24Fs and six P.24Gs in 1936. Delivered 1937-38. All Fs eventually re-armed with 4x Colt-Browning 7.7mm MGs.
Romania - The Royal Romanian Air Force ordered five PZL P.24E fighters in 1937 and built 25 IAR P.24E aircraft under license.
Turkey - The Turkish Air Force ordered 14 P.24A and 26 P.24C, delivered by 1937. Another 20 P.24A/Cs were built under license in Turkey in Kayseri, followed by an additional 30 P.24G aircraft.

General characteristics
Crew: 1
Capacity: fighter
Length: 7.50 m (22.96 ft)
Wingspan: 10.71 m (32,80 ft)
Height: 2.69 m (8.82 ft)
Wing area: 17.90 m² (192.7 ft²)
Empty weight: 1,327 kg (2,925 lb)
Loaded weight: 1,870 kg (4,121 lb)
Max. takeoff weight: 2,000 kg (4,400 lb)
Powerplant: 1 × Gnome-Rhône 14Kfs 14-cylinder double row radial engine, 900 hp / 930 hp (max) (671 kW / 693 kW (max))

Performance
Maximum speed: 410 km/h (254 mph)
Range: 700 km (435 mi)
Service ceiling: 9,000 m (29,527 ft)
Rate of climb: 11 m/s (2,160 ft/min)
Power/mass: 370.6 kW/tonne (451.5 hp/ton)

Armament
P.24A
2 MGs
2 20mm cannon
2 x 50 kg (110 lb) bombs
P.24B, P.24C
4 MGs
4 x 12,5 kg (27,5 lb) bombs
Specifications (P.24E)

General characteristics
Crew: 1
Capacity: fighter
Length: 7.50 m (22.96 ft)
Wingspan: 10.71 m (32,80 ft)
Height: 2.69 m (8.82 ft)
Wing area: 17.90 m² (192.7 ft²)
Empty weight: 1,327 kg (2,925 lb)
Loaded weight: 1,900 kg (4,188 lb)
Max. takeoff weight: 2,000 kg (4,400 lb)
Powerplant: 1 × Gnome-Rhône 14KIIc32 14-cylinder double row radial engine, 900 hp / 930 hp (max) (671 kW / 693 kW (max))

Performance
Maximum speed: 408 km/h (253 mph)
Range: 700 km (435 mi)
Service ceiling: 10,000 m (32,808 ft)
Rate of climb: 11 m/s (2,160 ft/min)
Power/mass: 364.7 kW/tonne (445 hp/ton)

Armament
2 MGs
2 20mm cannon
2 x 50 kg (110 lb) bombs
Specifications (P.24F, P.24G)

General characteristics
Crew: 1
Capacity: fighter
Length: 7.81 m (22.96 ft)
Wingspan: 10.68 m (32,80 ft)
Height: 2.69 m (8.82 ft)
Wing area: 17.90 m² (192.7 ft²)
Empty weight: 1,329 kg (2,930 lb)
Loaded weight: 2,000 kg (4,409 lb)
Max. takeoff weight: 2,000 kg (4,400 lb)
Powerplant: 1 × Gnome-Rhône 14N-07 14-cylinder double row radial engine, 970 hp (700 kW)

Performance
Maximum speed: 430 km/h (267 mph)
Range: 700 km (435 mi)
Service ceiling: 10,000 m (32,808 ft)
Rate of climb: 11,1 m/s (2,165 ft/min)
Power/mass: 350 kW/tonne (440.1 hp/ton)

Armament
P.24F
2 MGs
2 20mm cannon
2 x 50 kg (110 lb) bombs
P.24G
4 MGs
4 x 12,5 kg (27,5 lb) bombs

The PZL P.24 was a Polish fighter aircraft, designed during mid-1930s in the PZL factory in Warsaw. It was developed as a dedicated export version of the PZL P.11, a gull wing all-metal fighter designed by Polish aeronautical engineer Zygmunt Puławski.

While the P.11 had been powered with a license-built Bristol Mercury radial engine, the terms of this license did not permit PZL to export the engine as well as placing restrictions upon any aircraft that were powered by it. The French engine manufacturer Gnome-Rhône proposed the adoption of their 14K engine to PZL and offered to partially finance the development of a fighter using the engine, which would have no such export restrictions. Accordingly, during early 1932, PZL commenced work on a new derivative of the P.11, which became known as the P.24. The prototypes soon demonstrated favourable performance during testing; notably, the second P.24/II prototype, often referred to as the "Super P.24", established a new world speed record for a radial engine-powered fighter of 414 km/h. The initial production aircraft closely resembled the P.24/II configuration, albeit with some changes such as the adoption of an enclosed cockpit.

First entering operational service during 1936, the P.24 was exported to multiple countries, including Bulgaria, Greece, Romania, and Turkey. It was produced under licence by Romanian aviation firm Industria Aeronautică Română (IAR), who had also licence-produced the earlier P.11 as well. Reportedly, elements of the P.24, such as its tail section, were incorporated into a Romanian-designed monoplane fighter, the IAR 80. In Greece, the Royal Hellenic Air Force (EVA) was the only air service in Second World War to operate the P.24 as its primary fighter. However, wartime experience soon showed that, as a result of the rapid advances in aircraft design made during the late 1930s, the P.24 had become obsolete in comparison to newer fighters as early as 1940. Despite a relatively powerful engine and satisfactory armament, it could not stand up against some of the Axis fighters, such as the Macchi MC.200 and the Fiat G.50. Just like the Greek fighters, by 1942, it had become clear that Romania's P.24s were unable to effectively challenge the fighters of the VVS, and were relegated to training operations.