SZD-21 Kobuz

The SZD-21 was a successor to the IS-4 Jastrząb. Development began in January 1958 as the SZD-21 Sokół, but due to problems with the flying surfaces and a wood metal sandwich, a construction of the design was restarted as the SZD-21 Kobuz (Eurasian hobby), than SZD-21-2 Kobuz. The new SZD-21-2 retained the overall shape of the original project, but was constructed with wood throughout, using multiple spars for the wings. Design team was headed by Jerzy Trzeciak, later joined by M. Gracz in Kobuz 3 constructing. Flight testing of the SZD-21 Kobuz began on 3 June 1961 with Stanisław Skrzydlewski at the controls, but the results were disappointing prompting a re-build as the SZD-21-2A, with a completely revised fuselage, landing gear, canopy and differential ailerons. Flight tests resumed on in May 1962, but serious problems with the pitch and roll stability at high speed as well as flutter in a certain speed range prompted a further round of modifications. The resulting SZD-21-2AZ (still registered as SP-1990) continued the test program until 20 April 1963, when the aircraft broke up in flight during flutter testing, killing the pilot Sławomir Makaruk. == Variants ==

• SZD-21 Sokół – The original designation of the project as begun in 1958. • SZD-21-2 Kobuz – The initial prototype version, (reg'n SP-1990), which proved unsatisfactory, modified to Kobuz 2A. • SZD-21-2A Kobuz 2A – The second version of the prototype, (reg'n SP-1990), again disappointing, modified to SZD-21-2AZ • SZD-21-2AZ – The final modification state of the SZD-21 prototype, (reg'n SP-1990), which crashed on 20 April 1963 • SZD-21-2B Kobuz 3 – The final version of the Kobuz, first flight 10 December 1964, which proved acceptable and a small production batch were completed. ==Specifications (SZD-21 Kobuz 3)==