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  2. Diamond DA20 Katana - Wikipedia

    en.wikipedia.org/wiki/Diamond_DA20_Katana

    DV 20 Katana. The nose wheel of the DA20 is not linked to the rudder pedals and turns while taxiing are made with differential braking, with rudder steering becoming more effective as airspeed increases. [17] The Katana possesses a higher glide ratio than many of its competitors; its glide ratio is 11:1 and the DA20-A1 is 14:1. [18]

  3. Diamond Aircraft Industries - Wikipedia

    en.wikipedia.org/wiki/Diamond_Aircraft_Industries

    Following several changes in ownership and naming, the company received the name Diamond Aircraft Industries in 1998. By this point, Diamond was producing a range of light aircraft, including the Dimona, the Diamond DA20, and the in-development Diamond DA40. In 2004, Diamond introduced its first multi-engined aircraft, the Diamond DA42 Twin Star.

  4. Category:Diamond aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Diamond_aircraft

    Diamond D-Jet; Diamond DA20 Katana; Diamond DA40 Diamond Star; Diamond DA42 Twin Star; Diamond DA50; Diamond DA62; Diamond DART 280; Diamond DART series; Diamond Hero; H.

  5. Diamond DA40 Diamond Star - Wikipedia

    en.wikipedia.org/wiki/Diamond_DA40_Diamond_Star

    The Diamond DA40 Diamond Star is an Austrian four-seat, single-engine, light aircraft constructed from composite materials. Built in both Austria and Canada, it was developed as a four-seat version of the earlier DA20 by Diamond Aircraft Industries. By the end of December 2020, 2,200 DA40s had been delivered, including 500 NG models. [1]

  6. Category:1990s Austrian civil utility aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:1990s_Austrian...

    Diamond DA20 Katana; Diamond DA40 Diamond Star; H. HB Flugtechnik HB-207 Alfa This page was last edited on 13 May 2019, at 15:45 (UTC). Text is available under ...

  7. Rotax 912 - Wikipedia

    en.wikipedia.org/wiki/Rotax_912

    The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 80 hp (60 kW) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.

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    mail.aol.com/?rp=webmail-std/en-us/basic

    Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

  9. List of current production certified light aircraft - Wikipedia

    en.wikipedia.org/wiki/List_of_current_production...

    Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389