SZD-19 Zefir


The SZD-19 Zefir is a single-seat glider aircraft that was designed and built in Poland from 1957.
Although they all bore the same name, the different versions of Zefir were actually quite different gliders in terms of materials used, design and performance. What unified them most was the person of the lead designer - Bugumił Szuba and the use of large Fowler flaps to get superior performance both at low and high-speed flight. The Zefir series is perhaps the ultimate design of the wooden glider construction era.
Intended to replace the SZD-8 Jaskółka as the Polish team mount at the World Gliding Championships in 1958 in Leszno, the SZD-19 Zefir was a high-wing glider with a wooden and glass-fibre fuselage, retractable undercarriage and all-metal wings incorporating hydraulically actuated flaps. The first prototype SZD-19X Zefir flew on 31 December 1958, missing the 1958 championships, but the flight tests revealed problems with control and stability as well as operation of the flaps and complexity of the hydraulic system.
The SZD-19 was totally re-designed with all-wooden wings, revised fuselage and tail section, and towing hook relocated to the retractable undercarriage chassis, designated as the SZD-19-2 Zefir 2, first flying on 11 March 1960, showing a marked improvement over the Zefir. Two prototypes of the Zefir 2 were built, flying in the 1960 World Championships at Köln in Germany to gain second, piloted by Edward Makula, and third, piloted by Jerzy Popiel, places in the Open class.
With significant success in the World Championships, the SZD-19-2 was refined with new stabilisers and landing gear to become the SZD-19-2 Zefir 2A, flying for the first time in 1962, in time for the 1963 World Championships, held in Argentina, where Makula and Popiel took first and second places. As a result of these successes, demand for the SZD-19-2 was significant with 14 units built, most being sold to other countries,. From the beginning until Zefir 3 these gliders did not have spoilers - a tail chute was used. The chute drag could be controlled by the pilot.
Several records were established by the Zefir 2A/B's, including; a flight distance of and a closed triangle speed record of 102 km/h.
To improve the performance, further development with wings extended to 19m was carried out as the SZD-29 Zefir 3, of which two prototypes were built, and the Open-class 19m SZD-31 Zefir 4 of which three were built. Two SZD-31 Zefir 4's competed in the 1968 World Gliding Championships at Leszno with mediocre results - they took 14th and 28th place.
Because the Zefir series pushed the limits of a wooden wing construction, all construction elements were carefully designed with unusually narrow tolerance margins. Jerzy Śmielkiewicz describes a catastrophic in-flight wing failure
of one of Zefir's caused by
a careless minor change of the design of a few rivet placements - the whole original design was accounting for forces resulting from and/or involving individual rivets.

Handling characteristic

Historical accounts report that all the Zefir versions required superior piloting abilities but the modern restoration aircraft is reported to be docile. Until Zefir 4 they had no airbrakes which had caused multiple landing incidents. A chute was used for braking, from 2B version the pilot could adjust the chute drag. The forward visibility was considered poor. Similarly, the controls required substantial force, were causing strain for the pilots and in general their ergonomics was not optimal. All these inconveniences were the result of the design striving to squeeze every possible bit of performance, handling comfort was considered second. One of the test pilots recalls that the introduction of airbrakes in the Zefir 4 model was welcomed by the pilots, despite their dreadful influence on glider performance. Also, Zefir 3 had substantial horizontal stabilizer flatter issues.

Variants