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  2. CZAW SportCruiser - Wikipedia

    en.wikipedia.org/wiki/CZAW_SportCruiser

    Data from Manufacturer General characteristics Crew: one Capacity: one passenger Length: 6.62 m (21 ft 9 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.315 m (7 ft 7 in) Wing area: 12.3 m 2 (132 sq ft) Empty weight: 388 kg (855 lb) Gross weight: 600 kg (1,323 lb) Fuel capacity: 114 litres (25 imp gal; 30 US gal) Powerplant: 1 × Rotax 912 ULS2, 73.5 kW (98.6 hp) Propellers: 3-bladed Woodcomp ...

  3. General Motors LS-based small-block engine - Wikipedia

    en.wikipedia.org/wiki/General_Motors_LS-based...

    LSX376-B15 (part number 19299306) includes forged steel crankshaft, forged powdered metal I-beam rods (both the crankshaft and rods from the LSA engine), forged aluminum pistons (9.0:1 compression), and high-flow rectangular-port six-bolt LSX-LS3 heads for supercharged and turbocharged combinations producing up to 15 psi (1.0 bar) of boost and ...

  4. Roko Aero NG4 - Wikipedia

    en.wikipedia.org/wiki/Roko_Aero_NG4

    The main differences between the two are in span and weight: the UL has a shorter span (8.10 m (26 ft 7 in) than the LSA (10.10 m (33 ft 2 in). With an empty weight of 298 kg (657 lb) the prototype UL was somewhat over its target of 280 kg (620 lb) but 32 kg (71 lb) lighter than the LSA. [1] [2]

  5. Evektor SportStar - Wikipedia

    en.wikipedia.org/wiki/Evektor_SportStar

    The SportStar was the first special light-sport aircraft (S-LSA) approved by the US Federal Aviation Administration (FAA), and was named "S-LSA Aircraft of the Year" in 2011 by AeroNews Network. [1] According to Flight International , the SportStar held the number-one seller spot in 2005, which the periodical attributed to its high range of ...

  6. Bearhawk LSA - Wikipedia

    en.wikipedia.org/wiki/Bearhawk_LSA

    [1] [4] In 2015 a quick-build kit was introduced at the U.S Sport Aviation Expo. [5] The aircraft fuselage is fabricated from welded 4130 steel tubing covered in doped aircraft fabric. The aluminum structure wing, covered in flush riveted aluminum sheet, employs a new Harry Riblett-designed airfoil and does not have flaps. The wing is supported ...

  7. BRM Aero Bristell - Wikipedia

    en.wikipedia.org/wiki/BRM_Aero_Bristell

    The BRM Aero Bristell NG 5, now called the Bristell Classic, is a Czech low-wing, two-seat in side-by-side configuration, single engine in tractor configuration, ultralight and light-sport aircraft that was designed by Milan Bristela and is produced by BRM Aero. The aircraft is supplied as a complete ready-to-fly aircraft. [2] [3] [4]

  8. Aerospool WT9 Dynamic - Wikipedia

    en.wikipedia.org/wiki/Aerospool_WT9_Dynamic

    Data from Bayerl, Tacke and Aerospool General characteristics Crew: two Capacity: one passenger and one pilot Length: 6.40 m (21 ft 0 in) Wingspan: 9.00 m (29 ft 6 in) Height: 2 m (6 ft 7 in) Wing area: 10.35 m 2 (111.4 sq ft) Empty weight: 350 kg (772 lb) Gross weight: 600 kg (1,323 lb) MTOW depends on certification Fuel capacity: 75 litres (16 imp gal; 20 US gal) standard, 125 litres (27 imp ...

  9. Van's Aircraft RV-12 - Wikipedia

    en.wikipedia.org/wiki/Van's_Aircraft_RV-12

    Minimal use of composites and maximum use of aluminum Maximum use of simple hand tools only for construction The LSA class limits aircraft to a maximum takeoff weight of 1,320 lb (599 kg), a maximum clean, stall speed with no flaps of 51 mph (45 knots) and a maximum level speed of 138 mph (120 knots) and the production RV-12 falls within those ...