The Allstar SZD-54 Perkoz (English: great crested grebe) is a two-seater, glider for training, aerobatics, cross country flight and cloud flying from the Polish manufacturer Allstar PZL Glider (formerly PZL Bielsko). The sailplane has exchangeable wing tips for either 17.5 or 20 metres (57.4 ft or 65.6 ft) and is manufactured primarily from glass fibre reinforced plastic (GFRP). Without wing extension, it is certified for unlimited aerobatic manoeuvres. For glider training, the short wingspan (17.5 metres) is supplemented with winglets.[1] As a cross-country glider with a 20 metres wing and winglets, the Perkoz has a glider index of 102. The SZD-54-2 Perkoz is the successor of the widely used SZD-50-3 Puchacz trainer, which is part of the SZD family of aircraft.[2]
The SZD-54 was designed in 1991 by Adam Meus as a universal sailplane for flight training and aerobatics, and is certified to European Aviation Safety Agency (EASA) CS22 standards.[3] It is designed as a replacement for the SZD-50-3 Puchacz, a two-seater training glider from 1979, which Adam Meus also led the design.[4][2]
The sailplane can be purchased with 3 wing configurations: 17.5-metres wingspan with simple wing tips for aerobatics, 17.5-metre wingspan with attached winglets for training flights, and 20-metres wingspan with attached wing tips and winglets for cross-country flights. Despite its fixed landing gear, the SZD-54-2 has a best glide ratio of 42:1 with the 20 metres span wing[5] and offering a glide ratio of 38:1 with the 17.5 metres.[6]
The SZD-54-2 (17.5-metre) is engineered for aerobatics and aerobatic instruction with high load factor of +7 g and -5 g that can be exploited up to Vne (never-exceed speed) of 269 km/h[7], meeting the unlimited acrobatic category. This includes manoeuvres with reversed airflow, as well as snap (flick) rolles that exceed the classic figures.[8] The aircraft is made predominantly from glass fibre reinforced plastic (GFRP), selected components such as the rudder and replaceable wing tips are reinforced with carbon fibre.[9] The fuselage is a shell construction with welded tubular steel frames to support the wings and landing gear.[10]
It features a cantilever mid-wingwith the laminar airfoil NN-8 and has a trapezoidal plan form. The laminar airfoil was developed for the SZD-41 / SZD-48 Jantar Standard by the team led by Professor Jerzy Ostrowski at the Aerodynamics Department of the Warsaw University of Technology.[11] The ailerons with 20% of chord depth are generously dimensioned for aerobatics. The wing has Schempp-Hirth-type air brakes. All controls are automatically connected upon assembly.[2]
As the sailplane is designed for aerobatics, it features a conventional tailplane for enhanced strength. The horizontal stabilizer is located far back and is attached to the top of the fuselage. The rudder has a characteristically large rudder horn to reduce control forces in aerobatics.
The Perkoz is equipped with a fixed monowheel gear, a main wheel with spring suspension, a hydraulic disc brake, as well a small nosewheel and a tail caster.[2] The seats in the cockpit are arranged in tandem, one behind the other. The one-piece cockpit canopy with sliding windows opens sideways to the right. It is equipped with a "Röger hook" for emergency jettison.[9] The SZD-54-2 has two instrument panels and two cushioned seat shells with neck support. The pilot can adjust their seating position at the front using the rudder pedals and at the rear using the ground-adjustable seat. Trim weights are located in the front cockpit to compensate for light student pilots (min. 55 kg).[10] The cockpit has been certified as a safety cockpit according to the 2016 CS-22 standard.[12]
The maximum wing loading of the aerobatic version is 36.1 kg/m2, of the 20-metre version is 35.5 kg/m2.The SZD-54 has a design airframe life of 15,000 flight hours, but is approved for 3,000 hours and comes from the factory with a two-year warranty.[13]
Development
The first flight of the SZD-54 Perkoz prototype (registration number SP-P519) took place on 8 May 1991 in Jelenia Góra with pilot Jerzy Śmielkiewicz.[14] Economic shifts in Eastern European nations in the early 1990s slowed down further development.
On 14 May 1999, the second Perkoz prototype flew in Jelenia Góra with test pilot Jack Marszalek. Some modifications were made to the first prototype: for example in order to improve the flight characteristics in aerobatics, the incidence angle of the wing was reduced to + 1°.[15]
In 2002, Allstar PZL Glider took over the rights of this aircraft type from the insolvent state-owned company PDPSz PZL Bielsko. Allstar PZL Glider has made significant improvements to the two-seater glider. Firstly, the wing was extended with an extension and winglet. The new wingspan of 20 metres increases the glide ratio to 42. Secondly, the wingspan of 17.5 metre was equipped with winglets. Dr. Krzysztof Kubrynski of the Warsaw University of Technology developed both winglets. Furthermore, automatic elevator connections, a gas spring assisted canopy opening, a hydraulic disc brake on the main wheel and a "Röger hook" on the canopy were established.[16]
The test flight of the new SZD-54-2 Perkoz (SP-8013) was conducted on 2 April 2007 with pilot Mariusz Stajewski for the EASA certification. The EASA increased the safety requirements for new glider cockpits in the CS-22 construction rules during the certification process. The new requirements were adopted, the cockpit was revised, and the aircraft received its final EASA certification in 2013.[16]
Flight characteristics
The design of the Perkoz as a training and aerobatic two-seater sailplane makes it a very manoeuvrable aircraft with a high roll rate, even with a 20-metre wingspan.[17] For spin training during basic and advanced flight instruction, the aircraft does not have any temporary modifications, such as e.g. adding extra weights to the tail unit. The stall is clearly indicated by decreasing control pressure and buffeting.[8][18] The spin is deliberately initiated, and its recovery is precise and without delay.[19][18]
The SZD-54-2 has well-balanced controls and moderate control forces.[20] In a thermal, the glider circles and centres steadily.[17] The sailplane accelerates quickly with the NN-8 airfoil and achieves a glide ratio of 42 in the 20-metre version. At speeds exceeding 140 km/h, it presents disadvantages in comparison to designs that have been solely optimised for cross-country flight performance.[19]
The take-off distance in aerotow is short because the Perkoz has large wing surfaces and good climb rates for a training two-seater.[17] When landing, the large effective Schempp-Hirth-type air brakes are activated, or it is possible to slip. Landing is on the main wheel.[21] The landing flare is relatively short.[17] In aerobatics tail slide, quarter rolls down and up, snap (flick) as well as negative manoeuvers can be trained.[22]
PZL was the main Polish aerospace manufacturer of the interwar period, and a brand of their aircraft. Based in Warsaw between 1928 and 1939, PZL introduced a variety of well-regarded aircraft, most notably the PZL P.11 fighter, the PZL.23 Karaś light bomber, and the PZL.37 Łoś medium bomber.
The Schempp-Hirth Discus is a Standard Class glider designed by Schempp-Hirth. It was produced in Germany between 1984 and 1995 but has continued in production in the Czech Republic. It replaced the Standard Cirrus. It was designed by Klaus Holighaus.
The Glaser-Dirks DG-300 is a Standard Class single-seat high-performance glider built from glass-reinforced plastic. The DG-300 was designed by Wilhelm Dirks and manufactured by Glaser-Dirks Flugzeugbau's Slovenian partner company Elan (company). A total of 511 of all versions were built since production started in 1983. Representative contemporary types from competing manufacturers are the Rolladen-Schneider LS4 and the Schempp-Hirth Discus.
The PZL Bielsko SZD-50 Puchacz is a Polish two-place training and aerobatic sailplane.
The SZD-30 Pirat is a single-seat multipurpose glider aircraft from the Polish firm PZL Bielsko which first flew in 1966, and started production in 1967.
The SZD-45 Ogar (Hound) is a T-tailed cantilever high-wing monoplane of wooden, aluminium and fibreglass construction designed and manufactured in Poland.
The PZL Bielsko SZD-55 Nexus is a Standard Class sailplane produced by PZL Bielsko since 1988. It was built in direct competition with the Schempp-Hirth Discus. The SZD-55 is still in production with approximately 110 built.
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A glider or sailplane is a type of glider aircraft used in the leisure activity and sport of gliding. This unpowered aircraft can use naturally occurring currents of rising air in the atmosphere to gain altitude. Sailplanes are aerodynamically streamlined and so can fly a significant distance forward for a small decrease in altitude.
Szybowcowy Zakład Doświadczalny (SZD), Glider Experimental Works was a glider design and research centre of the Polish aerospace industry after World War II, located in Bielsko-Biała. Through its history it underwent many organizational and name changes, among others in 1946-1948 it was Instytut Szybownictwa. After 1969 it existed under other names, but an abbreviation SZD continued to be used on designs. The SZD gliders themselves were produced in the production centre in Bielsko-Biała, organized around the SZD, and by several other works of the state aerospace industry and didn't bear specific manufacturer's names.
The Celair GA-1 Celstar is a South African mid-wing, single-seat, aerobatic glider that was designed by Pieter Celliers and produced by his company, Celair (Pty) Limited.
The PZL Bielsko SZD-51 Junior is a Polish single-seat training and club sailplane.
The PZL M-3 Pliszka (Wagtail) was the first all-metal Polish glider. Three were built but its performance, particularly its glide ratio, was not good enough for it to be produced for Polish clubs.
References
↑ Brütting, Georg; Alexander Willberg (2023). Die berühmtesten Segelflugzeuge der Welt[The most famous gliders in the world] (in German). Stuttgart: Motorbuch Verlag. p.241. ISBN978-3-613-04569-9.
1 2 3 4 5 6 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 150. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
↑ Allstar PZL Glider Sp. z o.o. (2017). Type-Certificate Data Sheet EASA.A.574 (Issue 03ed.). EASA European Aviation Safty Agency. p.2.
↑ Murawski, Tomasz (2020). Sylwetki Szybowcow SZD (in Polish). Warzaw. p.108, 204.{{cite book}}: CS1 maint: location missing publisher (link)
↑ Robby Bayerl; Martin Berkemeier (2011). World Directory of Leisure Aviation 2011-12. Lancaster UK: WDLA UK. p.150.
1 2 Georg Brütting; Alexander Willberg (2023). Die berühmtesten Segelflugzeuge der Welt[The most famous gliders of the world] (in German). Stuttgart: Motorbuch Verlag. p.242. ISBN978-3-613-04569-9.
1 2 Allstar PZL Glider Sp. z o.i. Flight Manual for a sailplane SZD-54-2 (Doc. No. 542.4.01ed.). p.1.1 Sailplane description.
↑ Murawski, Tomasz (2017). Przegląd polskich szybowców: 1945-2017 (in Polish). Warszawa. p.87. ISBN978-83-937805-7-0.{{cite book}}: CS1 maint: location missing publisher (link)
↑ Markert, Udo (2016). "Pilot´s Report: SZD 54-2 „Perkoz" – Ein Stern am Vereins-Himmel" [Pilot´s Report: SZD 54-2 „Perkoz“ - A star in the club sky]. segelfliegen (in German). Gabler Media (2): 51.
↑ Allstar PZL Glider Sp. z o.o. (n.d.). "SZD-54 Perkoz". Retrieved 13 December 2012.
↑ Murawski, Tomasz (2020). Sylwetki Szybowcow SZD (in Polish). Warzaw. p.206.{{cite book}}: CS1 maint: location missing publisher (link)
↑ Murawski, Tomasz (2020). Sylwetki Szybowcow SZD (in Polish). Warzaw. p.206.{{cite book}}: CS1 maint: location missing publisher (link)
1 2 Murawski, Tomasz (2016). Polskie Szybowce SZD (in Polish). Warzawa. p.204.{{cite book}}: CS1 maint: location missing publisher (link)
1 2 3 4 Markert, Udo (2016). "Pilot´s Report: SZD 54-2 „Perkoz" – Ein Stern am Vereins-Himmel" [Pilot´s Report: SZD 54-2 „Perkoz“ - A star in the club sky]. segelfliegen (in German). Gabler Media (2): 50.
1 2 Frank-Dieter Lemke (2015). "SZD-54-2 Perkoz - Der Alleskönner aus Tschechien (Polen)" [SZD-54-2 Perkoz - The all-rounder from the Czech Republic (Poland)]. FliegerRevue - Magazin für Luft- und Raumfahrt (in German). Bergkirchen: PPVMEDIEN GmbH (05): 34.
↑ Frank-Dieter Lemke (2015). "SZD-54-2 Perkoz - Der Alleskönner aus Tschechien (Polen)" [SZD-54-2 Perkoz - The all-rounder from the Czech Republic (Poland)]. FliegerRevue - Magazin für Luft- und Raumfahrt (in German). Bergkirchen: PPVMEDIEN GmbH (05): 32.
↑ Allstar PZL Glider Sp. z o.i. Flight Manual for a sailplane SZD-54-2 (Doc. No. 542.4.01ed.). p.1.1 Sailplane description.
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