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You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation. A model attribution edit summary is Content in this edit is translated from the existing Czech Wikipedia article at [[:cs:Aero A-34 Kos]]; see its history for attribution.
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It was designed in 1929. The design was similar to the De Havilland Gipsy Moth. Of conventional biplane configuration and wooden construction, it featured wings that could be folded to allow it to be towed to and from airfields by automobile (width 2.91 m).
A prototype (registration L-BASO) had an 85 hp Walter Vegaradial engine. It took part in the Challenge 1929 international contest (piloted by Josef Novak), but had to withdraw due to engine failure and crash-landing on August 8, 1929.
Seven A.34s and its variants were built by Aero, with different engines: three A.34Js had the Walter Junior engine, and three A.134s had the 100 hp Walter Venus. They were used as trainers and sports planes in Czechoslovak civilian and military aviation.
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^. Archived from the original on 6 June 2011. Retrieved 6 November 2010.
March 17, 2024
aero, this, article, needs, additional, citations, verification, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, scholar, jstor, december, 2009, learn. This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Aero A 34 Kos news newspapers books scholar JSTOR December 2009 Learn how and when to remove this template message You can help expand this article with text translated from the corresponding article in Czech January 2020 Click show for important translation instructions View a machine translated version of the Czech article Machine translation like DeepL or Google Translate is a useful starting point for translations but translators must revise errors as necessary and confirm that the translation is accurate rather than simply copy pasting machine translated text into the English Wikipedia Consider adding a topic to this template there are already 227 articles in the main category and specifying topic will aid in categorization Do not translate text that appears unreliable or low quality If possible verify the text with references provided in the foreign language article You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation A model attribution edit summary is Content in this edit is translated from the existing Czech Wikipedia article at cs Aero A 34 Kos see its history for attribution You should also add the template Translated cs Aero A 34 Kos to the talk page For more guidance see Wikipedia Translation The Aero A 34 Kos Czech Blackbird was a small sports and touring biplane built in Czechoslovakia in the 1930s 1 A 34 KosAircraft Aero A 34 piloted by Josef Novak 1893 1934 during the Challenge International de Tourisme 1929 Role Light Sport AircraftNational origin CzechoslovakiaManufacturer Aero VodochodyFirst flight 1929It was designed in 1929 The design was similar to the De Havilland Gipsy Moth Of conventional biplane configuration and wooden construction it featured wings that could be folded to allow it to be towed to and from airfields by automobile width 2 91 m A prototype registration L BASO had an 85 hp Walter Vega radial engine It took part in the Challenge 1929 international contest piloted by Josef Novak but had to withdraw due to engine failure and crash landing on August 8 1929 Seven A 34s and its variants were built by Aero with different engines three A 34Js had the Walter Junior engine and three A 134s had the 100 hp Walter Venus They were used as trainers and sports planes in Czechoslovak civilian and military aviation Contents 1 Variants 2 Specifications A 34 3 See also 4 ReferencesVariants editA 34 A 34J A 34W Three aircraft powered by the 105 hp 78 kW Walter Junior inline piston engine A 134 One prototype powered by the 130 hp 97 kW Walter NZ 85 radial piston engine Specifications A 34 edit nbsp Aero A 34 KosGeneral characteristics Crew one Capacity one passenger Length 6 8 m 22 ft 4 in Wingspan 8 8 m 28 ft 10 in Height 2 5 m 8 ft 2 in Wing area 21 3 m2 229 sq ft Empty weight 400 kg 882 lb Gross weight 640 kg 1 411 lb Powerplant 1 Walter Vega five cylinder air cooled radial engine 63 kW 84 hp Performance Maximum speed 160 km h 99 mph 86 kn Range 320 km 200 mi 170 nmi Rate of climb 2 11 m s 416 ft min Wing loading 30 kg m2 6 1 lb sq ft Power mass 100 W kg 0 06 hp lb See also editAircraft of comparable role configuration and era Caudron C 230 De Havilland Gipsy Moth PZL 5References edit nbsp Wikimedia Commons has media related to Aero A 34 Kos Aero Vodochody History Archived from the original on 6 June 2011 Retrieved 6 November 2010 Retrieved from https en wikipedia org w index php title Aero A 34 Kos amp oldid 1121468842, wikipedia, wiki, book, books, library,
