PZL P.24
infobox Aircraft
name = PZL P.24
type = fighter
manufacturer =
caption =The second prototype of the PZL P.24
designer =Zygmunt Puławski
first flight =May 1933
introduced =1933
retired =
number built =
status =
unit cost =
primary user =
more users =
developed from =
variants with their own articles =
Development
The PZL P.24 was developed as an export version of the
In the meantime, a new version of the P.11, the P.11c, was developed for the Polish Air Force. It had a new refined fuselage, and the radial engine was lowered to give a pilot a better view. These changes were applied also to the new P.24 prototype, flown in 1936. This design used the whole tail fuselage section from the P.11c, was powered with a Gnome-Rhône 14Kfs engine (930 hp), and was armed with two 20 mm cannons and two
The P.24D was developed for sale to
The last two production versions were the P.24F and P.24G, produced from 1937 and powered with the more powerful convert|970|hp|abbr=on
The P.24H was to be powered with a Gnome-Rhône 14N21 engine (1,100 hp) and carry four cannons or two cannons and two machine guns, but it was not completed. The P.24H was considered for purchase by the Polish Air Force, but progress was slow due to the P.24's similarity to the PZL P.11, which was already in service, and also interest in the hypothetically superior
Operational history
Despite being a better fighter than the P.11, the P.24 was not acquired by the Polish Air Force, which preferred to wait for the PZL.50. When it became clear the PZL.50 would not be ready in time to counter the imminent German attack, the PAF resumed production of the P.11 and ordered the P.24. However, no PZL.24s were produced before the war started, and none were used in the Polish Campaign in 1939. The aircraft had greater success abroad, though.
;Turkey: Turkish P.24s were used for training until the late 1940s. Some were refitted with
;Greece: The PZL P.24 was the main Greek fighter at a time of the Italian attack in 1940, and engaged Italian bombers during the
;Romania: The
Technical description
The aircraft was conventional in layout, with high wings. It was all-metal and metal-covered. The wings had a
The armament was a combination of 20 mm
*P.24A, P.24E and P.24F had two cannons and two machine guns.
*P.24B, P.24C and P.24G had four machine guns.
The P.24A and B models could carry 4 x 12.5 kg bombs, while the P.24C, F and G could carry 2 x 50 kg bombs.
Operators
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*The
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pecifications
aircraft specifications
jet or prop?=prop
plane or copter?=plane
crew=1
capacity=fighter
length main=7.81 m
length alt=25 ft 7 in
span main=10.68M
span alt=35 ft 1 in
height main=2.7 m
height alt=8 ft 19 in
area main=17.90 m²
area alt=192.7 ft²
empty weight main=1330 kg
empty weight alt=2,930 lb
loaded weight main=1915 kg
loaded weight alt=4,220 lb
useful load main=
useful load alt=
max takeoff weight main=2000 kg
max takeoff weight alt=4,400 lb
engine (jet)=
type of jet=
number of jets=
thrust main=
thrust alt=
engine (prop)=
type of prop=14-cylinder double row
number of props=1
power main= 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)
power alt=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)
max speed main=430 km/h
max speed alt=270 mph
cruise speed main=
cruise speed alt=
never exceed speed main=
never exceed speed alt=
stall speed main=
stall speed alt=
range main=550 km
range alt=340 mi
ceiling main=10,500 m
ceiling alt=34,449 ft
climb rate main= 11.5 m/s
climb rate alt=2,260 ft/min
loading main=
loading alt=
thrust/weight=
power/mass main=0.376 kW/kg
power/mass alt=0.230 hp/lb
armament=
* 2
* 4 MGs (P.24B, P.24C and P.24G),
* 4 x 12.5 kg (4 x 28 lb) bombs (P.24A and B),
* 2 x 50 kg (2 x 110 lb) bombs (P.24C, F and G).
ee also
aircontent
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similar aircraft=
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References
Notes
Bibliography
* Cynk, Jerzy B. "Polish Aircraft 1893-1939". London: Putnam & Company Ltd., 1971. ISBN 0-370-00085-4.
* Cynk, Jerzy B. "The P.Z.L. P-24 (Aircraft in Profile no. 170)". Leatherhead, Surrey, UK: Profile Publications Ltd., 1967.
* Eberspacher, Warren and Koniarek, Jan P. "PZL Fighters Part Three - P.24 Variants". Austin, CO: Creative & Customized Support, 2002.
* Glass, Andrzej. "Polskie konstrukcje lotnicze 1893-1939" (in Polish). Warszawa, Poland: WKiŁ, 1976. No ISBN.
* Glass, Andrzej. "PZL P.24 (Wydawnictwo Militaria 2)" (in Polish). Warszawa, Poland: Wydawnictwo Militaria, 1994. ISBN 83-86209-13-5.
* Glass, Andrzej. "PZL P.24 A-G (Monographie no.7)" (Bilingual Polish/English). Lublin, Poland: Kagero, 2004. ISBN 83-89088-33-9.
* Green, William. "War Planes of the Second World War, Volume Three: Fighters". London: Macdonald & Co.(Publishers) Ltd., 1961. ISBN 0-356-01447-9.
* Napier, Sid. "Le PZL P.24 en Grèce" (In French), "AirMagazine No34", Oct-Nov 2006.
* Skulski, Przemyslaw. "PZL P.24 (Seria "Pod Lupą" 15)" (in Polish with English captions). Wrocław, Poland: ACE Publication, 2002. ISBN 83-86153-24-5.
* Skulski, Przemyslaw. "PZL P.24, The Last Polish Gull-wing Fighter", "Scale Aviation Modeller International", Vol. 10, Issue 9, September 2004.
External links
** [http://imansolas.freeservers.com/Aces/The%20Greek%20PZL%20fighters.html The Greek pilots fighting with PZLs - 1940]