| /Airplanes/Allies/Others/01-Poland/01-Fighters/PZL-P.24/PZL-P.24.htm / | Up-dated: |
P-24Specifications |
| General |
Type:
Fighter |
| Engine |
| 1× 14-cylinder double row radial engines: P.24A, B, C: Gnome-Rhône 14Kfs, P.24E: Gnome-Rhône 14K IIc32, P.24F, G: Gnome-Rhône 14N07, P.24A, B, C: 900 hp / 930 hp (max) (Gnome-Rhône 14Kfs), P.24E: 900 hp / 930 hp (max)(Gnome-Rhône 14K IIc32), P.24F, G: 950 hp / 970 hp (max) (Gnome-Rhône 14N07) (P.24A, B, C: 671 kW / 693 kW (max) (Gnome-Rhône 14Kfs), P.24E: 671 kW / 693 kW (max) (Gnome-Rhône 14K IIc32), P.24F, G: 709 kW / 723 kW (max) (Gnome-Rhône 14N07)) |
| Dimensions/Masses |
| Length: 7.81 m | Width:
10.68 m | Height: 2.7 m Weight: 1330 kg | Max. Combat Weight: 1915 kg-2000 kg |
| Performances |
| Max. Speed: 430 km/h | Ceiling: 10500 m | Range: 550 km |
| Armament |
MG:
4 Mx Gs (P.24B, P.24C and P.24G) or 2 x Oerlikon FF cannons and 2 MG's
(P.24A, P.24E and P.24F), |
