LWD Szpak

infobox Aircraft
name =LWD Szpak
type =Utility aircraft
manufacturer =LWD, WSK-Mielec



caption =
Szpak-4T

designer =Tadeusz Sołtyk
first flight =October 28, 1945
introduced = 1946
retired = 1955
status =
primary user =Polish civilian aviation
more users =
produced = 1945–1948
number built =13
unit cost =
variants with their own articles =The LWD Szpak was a Polish utility aircraft of 1945, the first Polish aircraft designed after World War II and built in a short series.

Development

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

On October 28, 1945, the prototype of Szpak-2 was flown for the first time; first Polish post-war civilian plane in operation. It broke landing gear during landing, but was repaired. The official first flight took place on November 10 that year. Szpak was a strutted monoplane low-wing utility/touring plane of wooden construction, powered by a radial engine Bramo Sh 14, left in the country by the retreating Germans. A crew of 4 sat in a closed cab under a multi-part canopy, in two rows. Szpak-2 was not built in a series. The single aircraft was used by the factory, then in 1947-1948 by the Polish government as a utility and light transport plane. 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 December 17, 1946, for the first time flew its improved experimental variant called Szpak-3 with a fixed tricycle 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 Szpak-4A was designed as an aerobatics plane. 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 aerobatics plane 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 called Szpak-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 the PZL (later WSK) in Mielec as the first Polish post-war planes built in a series. The very first one 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 - regional aero clubs until 1952, except for the SP-AAG, which was retired in 1955. They are also known as WSK Szpak-4T.

urvivors

;Szpak-2 (SP-AAA):Preserved in the Polish Aviation Museum in Kraków (damaged);Szpak-3 (SP-AAB):Preserved in the Polish Aviation Museum in Kraków (disassembled as of 2008);Szpak-4T (SP-AAG):Preserved in the Polish Aviation Museum in Kraków (disassembled as of 2008)

Operators

;POL
*Ministry of Foreign Affairs
*Polish Aero Club
*LWD workshops

pecifications (Szpak-4T)

aircraft specifications

plane or copter?=plane
jet or prop?=prop
crew=one, pilot
capacity=three passengers
length main=8.05 m
length alt=
span main=11.4 m
span alt=
height main=2.4 m
height alt=
area main=18.20 m²
area alt=
empty weight main= 700 kg
empty weight alt=
loaded weight main= 1,200 kg
loaded weight alt=
max takeoff weight main=
max takeoff weight alt=
engine (prop)=Bramo Sh.14A-4
type of prop= air-cooled 7-cylinder radial engine
number of props=1
power main=160 hp
power alt=118 kW

max speed main=180 km/h
max speed alt=
range main=630 km
range alt=
ceiling main=3,350 m
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
power/mass main=
power/mass alt=

ee also

aircontent
related=

similar aircraft=
*Aero A.200

lists=

see also=

References

*Babiejczuk, Janusz and Grzegorzewski, Jerzy: "Polski przemysł lotniczy 1945-1973" (Polish aviation industry...), Wydawnictwo MON, Warsaw 1974 (no ISBN) pl icon
*Krzyżan, Marian: "Samoloty w muzeach polskich", Warsaw 1983, ISBN 83-206-0432 pl icon

External links

* [http://www.airwar.ru/enc/la/szpak.html Photos at Ugolok Neba]