PZL.43

The PZL.43 was a Polish light bomber and reconnaissance aircraft designed in the mid-1930s by PZL in Warsaw. It was an export development of the PZL.23 Karas. Its main user was the Bulgarian Airforce who called it the Chaika.


PZL.43
Class Aircraft
Type Bomber
Manufacturer PZL
Production Period 1937 - 1939
Origin Poland
Country Name Origin Year
Poland 1937
Country Name Operational Year Retirement Year
Bulgaria View
Poland 1937 1946 View
ManufacturerName Production From Production To Quantity
PZL 1937 1939 54 View

The standard Polish light bomber and reconnaissance aircraft, the PZL.23 Karas could not be exported because of licence restrictions on the use of the Polish-built (PZL) Bristol Pegasus engine. The PZL.43 was an improved export variant of the PZL.23, powered instead by a Gnome-Rhône 14K engine. It was first offered to Romania, but they rejected it in favour of domestic designs. The PZL was more successful in Bulgaria, then reforming their airforce after a period of post-World War I treaty constraints. An order was placed in April 1936.

Like its predecessor, the PZL.43 was conventional in layout, a low-wing, all-metal, metal-covered cantilever monoplane. Its fuselage was semi-monocoque. It had a crew of three: pilot, bombardier and an observer/rear gunner. The pilot and observer's cockpits were in tandem and glazed with the open rear gunner's position behind. The bombardier occupied a ventral combat gondola which had a machine gun position at the rear. The fixed undercarriage was heavily spatted, though not suited for rough airfields. Tanks in the centre section of the wings held 740 litres of fuel. A three-bladed propeller was used.

The differences between the two types derived chiefly from use of the heavier and longer (two rows of seven cylinders) Gnome-Rhône engine. To maintain the centre of gravity the fuselage was lengthened by adding one central section which moved the bombardier's gondola rearwards. The new engine improved performance considerably, for example increasing maximum speed from 319 km/h to 365 km/h. In addition, armament was increased with two forward firing Karabin maszynowy wz. 36 machine guns mounted in offset fairings to clear the radial engine. Up to 700 kg of bombs could be carried under the wings, like the PZL.23. A common option was 24 x 12.5 kg bombs (300 kg in total). A camera was fitted.

No prototype preceded the production series of 12 aircraft completed in 1937. These were designated PZL.43 and powered by Gnome-Rhône 14Kirs motors of 900 to 930 hp (671 to 694 kW).

In March 1938, Bulgaria ordered a further 42 aircraft powered by the new Gnome-Rhône 14N-01 engine, an improved 14K design that delivered 950 to 1,020 hp (708 to 761 kW). These were designated PZL.43A. Production started in 1939, but only 36 were completed and delivered to Bulgaria before the German Invasion of Poland in September 1939.

Sometimes the aircraft is called the "PZL P.43", but despite an abbreviation P.43 painted on the tail fin, the letter "P" was generally reserved for fighters of Pulawski's design (like the PZL P.11). In some older sources the PZL.43 is referred to as the PZL.43A, and the PZL.43A as the PZL.43B. These latter designations are incorrect.

After the German invasion of Czechoslovakia in March 1939, in an increasingly tense political situation, the Polish Air Force proposed to requisition from the Bulgarian order of PZL.43As. A short-sighted decision by the military authorities, afraid of penalties, was to fulfill the order (the penalties would have been less than the worth of two aircraft - about 440,000 zlotys). The first PZL.43As were delivered to Bulgaria in June 1939, the last of 36 in August, just before World War II began. Along with 12 PZL.43s and two PZL.43As delivered by Germany in 1940, these gave Bulgaria a total of 50 aircraft.

They initially served in three 12-aircraft squadrons of the 1st Line Group (linyen orlyak). From 1942 they were used in the 1st Reconnaissance Regiment and 2nd Line Regiment. Chaikas were used mostly for training and searching for partisans in Macedonia in 1943–44. Several of them crashed during service and there were difficulties in obtaining spare parts. In 1944 they were withdrawn from combat service and were eventually written off in 1946.

At the time of the German invasion of Poland, nine PLZ.43As of the Bulgarian order were crated ready for delivery or were incomplete, two lacking propellors. Five were moved to the airfield at Bielany and taken over by the Polish Air Force for use by 41 Eskadra Rozpoznawcza (41st Reconnaissance Squadron) which was mostly equipped with PZL.23 Karas. They undertook reconnaissance duties but by 10 September 1939, there were the only two aircraft remaining. One was shot down by a Messerschmitt Bf 110 at Michalówek near Sulejówek and the crew killed. The second, damaged by a pair of Messerschmitt Bf 109s, two days later, crash landed in Brzesc. Both probably still carried Bulgarian markings.

Another three complete aircraft from the Bulgarian order were left at Okecie and these were damaged during an air raid on 4 September and later captured by the Germans in a factory in Warszawa-Okecie. Some damaged aircraft left at Okecie airfield were captured by the Germans. Five were repaired and delivered to Bulgaria. Another was tested by the Germans in Rechlin in 1940 before joining the others in Bulgaria in October.

Role Light bomber and reconnaissanceaircraft
Manufacturer Panstwowe Zaklady Lotnicze
First flight February 1937
Introduction 1937
Retired 1946 (Bulgaria)
Primary users Bulgarian Air Force
Polish Air Force
Produced 1937 - 1939
Number built 54
Developed from PZL.23 Karas


General characteristics

  • Crew: 3
  • Length: 9.95 m (32 ft 8 in)
  • Wingspan: 13.95 m (45 ft 9 in)
  • Height: 3.3 m (10 ft 10 in)
  • Wing area: 26.8 m² (288 ft²)
  • Empty weight: 2,200 kg (4,850 lb)
  • Loaded weight: 3,100 kg (6,830 lb)
  • Useful load: 900-1,325 kg (1,980-2,920 lb)
  • Max. takeoff weight: 3,525 kg (7,770 lb)
  • Powerplant: 1 × Gnome-Rhône 14N-01 14-cylinder twin radial engine, 1020 hp (750 kW)

Performance

  • Maximum speed: 365 km/h at 4,000 m (227 mph at 13,000 ft)
  • Cruise speed: 300 km/h at ground level (186 mph at ground level)
  • Stall speed: 115 km/h (72 mph)
  • Range: 1,250 km (780 mi)
  • Service ceiling: 8,500 m (28,000 ft)
  • Rate of climb: 7.5 m/s (1,480 ft/min)
  • Wing loading: 115 kg/m² (23.7 lb/ft2)

Armament

  • 4 x machine guns:
  • 2 x 7.92 mm PWU wz.36B fixed in nose;
  • 1 x 7.92 mm PWU wz.36R in rear upper station;
  • 1 x 7.92 mm PWU wz.36R in underbelly station;
  • 600-700 kg bombs.

End notes