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2. Allstar SZD-54 Perkoz - Wikipedia

   en.wikipedia.org/wiki/Allstar_SZD-54_Perkoz

   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 ...

3. Phoenix Air Phoenix - Wikipedia

   en.wikipedia.org/wiki/Phoenix_Air_Phoenix

   Data from World Directory of Leisure Aviation 2011-12 and Phoenix Air General characteristics Crew: one Capacity: one passenger Length: 6.50 m (21 ft 4 in) Wingspan: 15 m (49 ft 3 in) Height: 1.45 m (4 ft 9 in) Empty weight: 295 kg (650 lb) Gross weight: 472.5 kg (1,042 lb) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp ...

4. Schempp-Hirth Janus - Wikipedia

   en.wikipedia.org/wiki/Schempp-Hirth_Janus

   The design was by Dipl-Ing Klaus Holighaus and the prototype first flew in May 1974. The production examples incorporated several improvements in January 1975. The Janus has a glass-fibre monocoque fuselage similar to that of the Nimbus-2 but the cockpit section is lengthened to accommodate the two pilots in tandem with dual controls under a right-hand side-hinged one-piece canopy.

5. Schleicher K 8 - Wikipedia

   en.wikipedia.org/wiki/Schleicher_K_8

   A motor glider conversion of the K 8B was developed by LVD (the Flying Training School of the Detmold Aero Club) similar to their conversion of a Scheibe Bergfalke IV known as the BF IV-BIMO, in which a Lloyd LS-400 piston engine mounted in the fuselage drives a pair of small two-blade pusher propellers rotating within cutouts in each wing near the trailing edge.

6. Rolladen-Schneider LS4 - Wikipedia

   en.wikipedia.org/wiki/Rolladen-Schneider_LS4

   The design of the LS4 was influenced mainly by the experience Rolladen-Schneider had gained with the LS2 and LS3 flapped gliders. Wolf Lemke returned to a double-tapered wing planform, giving it a larger area comparatively to the LS1 and LS2, and enlarged all control surfaces: the ailerons were elongated and brought further inboard and the tailplane span was increased.

7. Grob G 109 - Wikipedia

   en.wikipedia.org/wiki/Grob_G_109

   The aircraft then becomes a pure glider, with a best glide ratio of around 1:28. The Porsche-derived horizontally opposed air-cooled engine had the cylinder bore increase by Grob to make the engine 2.5-litre capacity and has had its Time Before Overhaul (TBO) increased by a technote to 1,600 hours after many examples run on condition reached up ...