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LWD Szpak

From Wikipedia, the free encyclopedia
LWD Szpak
Szpak-4T
General information
TypeUtility aircraft
ManufacturerLWD,WSK-Mielec
Designer
Tadeusz Sołtyk
Primary userPolish civilian aviation
Number built13
History
Manufactured1945–1948
Introduction date1946
First flightOctober 28, 1945
Retired1955

TheLWD Szpak (starling) was a Polish utilityaircraft of1945, the first Polish aircraft designed afterWorld War II and built in a short series.

Development

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The war destroyed the whole Polish aviation industry. As soon as the Eastern part of Poland was liberated by theRed Army in October 1944 a group of designers gathered inLublin, under the direction ofTadeusz Sołtyk, thus creating the first Polish post-war construction team. They designed a touring low-plane aircraft of a wooden construction calledSzpak-1, with aM-11F radial engine. The plane was not built, nevertheless it gave the beginning to a Szpak family. In early 1945 the construction team moved toŁódź and on April 1, 1945, createdLotnicze Warsztaty Doświadczalne (LWD,Aviation Experimental Workshops).

On October 28, 1945, the prototype of theSzpak-2 was flown for the first time; first Polish post-war civilian plane in operation. It broke its landing gear during a landing, but was repaired. The official first flight took place on 10 November 1945. Szpak was astrutted monoplane low-wing utility/touring plane of wooden construction, powered by a radial engineBramo Sh 14, left in the country by the retreating Germans. A crew of 4 sat in a closed cab under a multi-partcanopy, in two rows. Szpak-2 was not built in series, the single aircraft was used by the factory, then in 1947-1948 by the Polish government as a utility and light transport aircraft. Being the first plane registered in Poland after the war (on 10 May 1946) it carried the registration SP-AAA. It completed some 500 flights and transported some 250 passengers in total and was retired on April 5, 1948.

The Szpak-2 had a conventional fixed landing gear. On 17 December 1946, for the first time flew its improved experimental variant calledSzpak-3 with a fixedtricycle landing gear (markings SP-AAB). It was not built in a series either, and the prototype was used as a courier plane by the Ministry of Foreign Affairs during 1947, then by the factory. It was retired on March 6, 1950.

The next variant, theSzpak-4A, was designed as anaerobatic aircraft. Only one prototype was built, flown on May 20, 1947. It had a steel fuselage frame rather than a wooden one, and a two-men side-by-side open cab. It was not certified as an aerobatic aircraft however, and was used by the factory as a utility plane in 1947–1948.

The only variant produced in a series was the 4-seater utility plane calledSzpak-4T, utilizing the steel fuselage frame with a conventional landing gear. Contrary to Szpak-2 and 3, its fuselage was lowered behind a canopy. It was ordered by the Ministry of Communication and ten planes were built in 1947-1948 by thePZL (later WSK) inMielec as the first Polish post-war planes built in a series. The first was flown on January 5, 1948. The planes had markings: SP-AAF to SP-AAO, and SP-AAR. They were used by the Polish civilian aviation - regionalaero clubs until1952, except for the SP-AAG, which was retired in1955. They are also known as WSK Szpak-4T.

Variants

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Szpak-1
The design concept which spawned the Szpak series
Szpak-2
A version with a Bramo Sh 14 engine and portions of the wooden structure replaced with metal
Szpak-3
A tricycle undercarriage prototype
Szpak-4a
A single prototype aerobatic aircraft.
Szpak-4T
10 production aircraft.

Operators

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 Poland

Surviving aircraft

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Specifications (Szpak-4T)

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Data from[citation needed]

General characteristics

  • Crew: 1
  • Capacity: 3 pax
  • Length: 8.05 m (26 ft 5 in)
  • Wingspan: 11.4 m (37 ft 5 in)
  • Height: 2.4 m (7 ft 10 in)
  • Wing area: 18.2 m2 (196 sq ft)
  • Empty weight: 700 kg (1,543 lb)
  • Gross weight: 1,200 kg (2,646 lb)
  • Powerplant: 1 ×Bramo Sh.14A-4 7-cylinder air-cooled radial piston engine, 118 kW (158 hp)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Range: 630 km (390 mi, 340 nmi)
  • Service ceiling: 3,350 m (10,990 ft)

See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^"LWD Szpak 2".Muzeum Lotnictwa Polskiego (in Polish). Retrieved24 November 2024.
  • Babiejczuk, Janusz and Grzegorzewski, Jerzy:Polski przemysł lotniczy 1945-1973 (Polish aviation industry...), Wydawnictwo MON, Warsaw 1974 (no ISBN)(in Polish)
  • Krzyżan, Marian:Samoloty w muzeach polskich, Warsaw 1983,ISBN 978-83-206-0432-0(in Polish)

External links

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Wikimedia Commons has media related toLWD Szpak.
PZL aircraft
PZL - up to 1939
(Państwowe Zakłady Lotnicze)
PZL:
CSS / WSK-Okęcie
/ PZL Warszawa-Okęcie
PZL:
Other:
WSK-Mielec / WSK PZL-Mielec
/ PZL Mielec
(Polskie Zakłady Lotnicze)
PZL:
Other:
WSK-Świdnik / WSK PZL-Świdnik / PZL-Świdnik
PZL:
Other:
WSK PZL-Krosno
Szybowcowy Zakład Doświadczalny
/ PZL Bielsko-Biała / Allstar PZL Glider
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