EOL 2 Remos -Mmirage

History of the EOL aircraft. 1. the prototype of Remos EOL - 2 was built on 24.11.1992 at the manufacturer : Základ Produkcji Konstrukcji Lekkich in Bielsko Biala, Poland. It was a two-seat strut monoplane with tricycle landing gear. The wing with flaps has an all-composite structure and Kevlar reinforced load-bearing elements. The fuselage, including the wing surfaces, is also composite and the tail surfaces are also composite. Part of the covering is made of synthetic fabric. In the cabin, the seats are side by side. The aircraft was designed, constructed and manufactured by A. Kurbiel. Over time, the EOL 2 was modified and improved, and with each minor modification the commercial name of the aircraft was changed, but its design was not altered, and so the eOL - 2 Gull ( Geminy), which received a type licence from the LAA of the Czech Republic under number 10/1996. By installing the Rotax 912 UL, ULS engine, a modification called G.3.3.C Mirage was created in 1997. 2. During the time the name of the manufacturer changed, from Základ Produkcji Konstrukcji Lekkich in Bielsko Biala, Poland to Wytwornia i Naprawa konstrukcji Lekkich, then Wytwornia i Naprawa konstrukcji Lekkich Remos Adam kurbiel i L. Kreichmer, Remos Sp.z.o.o., Zaklady Lotnicze 3Xtrim (since 200). The EOL G.3.3 C Mirage aircraft has the same design as the EOL-2 aircraft, with a Rotax 912 ULS engine and a Junkers Magnum rescue system installed. Aircraft specifications : Wingspan 9,8 m Length 6,5 m Height 2,4 m Wing area 12,04 m2 Empty weight 300 kg Empty weight with rescue 320 kg Max. permissible weight 495 kg Max cruising speed 195 km Max. permissible weight Speed. No 220 km Minimum speed 65 km Climb rate 6,4 m/sec Max operating multiples +4/-2 g.