Avia BH-33

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BH-33
Type Fighter
Manufacturer Avia, PWS (under licence), Ikarus (under licence)
Maiden flight 21 October, 1927
Primary users Czechoslovak Air Force
Polish Air Force
Yugoslav Royal Air Force
Produced ca. 110, plus 50 licence-built in Poland and 22 in Yugoslavia
Developed from Avia BH-21
Variants PWS-A

The Avia BH-33 was a biplane fighter aircraft built in Czechoslovakia in 1927. It was based on the BH-21J that demonstrated promising results by marrying the original BH-21 airframe with a licence-built Bristol Jupiter radial engine. Other than the peculiar Avia hallmark of having an upper wing with a shorter span than the lower, it was utterly conventional; even featuring a tail fin for the first time in a Pavel Beneš and Miroslav Hajn design (previous aircraft had a rudder but no fin).

Contents

[edit] Design and development

Initial tests of the first prototype were disappointing, displaying performance only marginally better than the BH-21, even when fitted with a more powerful version of the Jupiter. Two further prototypes followed, both designated BH-33-1, each with an increasingly powerful Jupiter variant - one a Jupiter VI, the other a Jupiter VII. The performance of the latter example was finally good enough for the Czechoslovakian war ministry to order a small production run - of only five aircraft. Three examples were sold to Belgium, where there were plans to build the type under licence, but this did not eventuate. Licence production was undertaken, however, in Poland, where a single example was sold along with a licence to build fifty aircraft. These were designated PWS-A and put into service with the Polish Air Force in 1930 [1].

Development continued with an almost total redesign of the fuselage, replacing the wooden, slab-sided structure with one of oval cross-section built up from welded steel tubes. Designated BH-33E, this was at last a world-class fighter for its time. Nevertheless, the response from the Czechoslovakian military was lukewarm (although two were bought for the national aerobatics team), and Avia again looked abroad for customers, this time selling twenty aircraft to Yugoslavia, along with a licence to produce another twenty-four. Two or three examples were also bought by Russia for evaluation.

In late 1929, a further development was flown as the BH-33L, featuring longer-span wings, and a Škoda L W-block engine. This version finally brought the company the domestic sales that it had been hoping for, with eighty aircraft ordered by the air force. These became standard equipment with some air regiments up to the outbreak of World War II.

A single, final variant with a BMW-built Pratt & Whitney Hornet engine was built as the BH-33H (later redesignation BH-133) in 1930, but this did not lead to production.

[edit] Operational history

Czechoslovakian BH-33s never saw combat, and Poland's examples had long been replaced in service by the time of the German invasion. Two Yugoslavian machines did, however see combat against Luftwaffe Bf 109s, but were both destroyed and their pilots killed.

[edit] Variants

BH-33
First prototype.
BH-33-1
Two prototypes powered by Jupiter VI (second) and Jupiter VII (third) engines plus 5 serial built aircraft with Jupiter VII engine.
BH-33E
Rebuilt fuselage
BH-33L
Version with longer span wings and powered by Škoda L engine, 80 built.
BH-33H (BH-133)
Version powered by Pratt & Whitney Hornet engine, 1 built.
PWS-A
Polish license-built variant of the BH-33 with minor modifications[2], 50 built between 1929 and 1932.

[edit] Operators

Flag of Belgium Belgium
Flag of Czechoslovakia Czechoslovakia
Flag of Poland Poland
Flag of the Soviet Union Soviet Union
Flag of Yugoslavia Yugoslavia

[edit] Specifications (BH-33L)

General characteristics

  • Crew: one pilot
  • Length: 7.22 m (23 ft 8 in)
  • Wingspan: 8.90 m (29 ft 2 in)
  • Height: 3.13 m (10 ft 3 in)
  • Wing area: 25.5 m² (274 ft²)
  • Empty weight: 1,117 kg (2,463 lb)
  • Gross weight: 1,560 kg (3,439 lb)
  • Powerplant: 1 × Škoda L, 430 kW (580 hp)

Performance

  • Maximum speed: 298 km/h (186 mph)
  • Range: 280 km (450 miles)
  • Service ceiling: 8,000 m (26,200 ft)
  • Rate of climb: 9.9 m/s (1,940 ft/min)

Armament

[edit] References

  1. ^ Belcarz, Avia BH-33 (PWS-A), PWS-10, PZL P.7a, p.6
  2. ^ Belcarz, Avia BH-33 (PWS-A), PWS-10, PZL P.7a, p.6
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 86. 
  • World Aircraft Information Files. London: Bright Star Publishing, File 889 Sheet 86. 
  • Belcarz, Bartłomiej (2005). Avia BH-33 (PWS-A), PWS-10, PZL P.7a, Polskie Skrzydła #3. Sandomierz: Wydawnictwo Stratus, ISBN 83-89450-36-4 (Polish language).
  • Němeček, Vaclav (1968). Československá letadla. Praha: Naše Vojsko.
  • airwar.ru


[edit] See also

Related development BH-17 - BH-21 - BH-22 - BH-23

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