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  2. Apollo Delta Jet - Wikipedia

    en.wikipedia.org/wiki/Apollo_Delta_Jet

    Capacity: one passenger; Wingspan: 10.0 m (32 ft 10 in) Wing area: 14.5 m 2 (156 sq ft) Empty weight: 236 kg (520 lb) Gross weight: 472.5 kg (1,042 lb) Fuel capacity: 55 litres (12 imp gal; 15 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp) Propellers: 3-bladed composite ...

  3. Polaris AM-FIB - Wikipedia

    en.wikipedia.org/wiki/Polaris_AM-FIB

    The 11.15 m (36.6 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine. The main landing gear is extended and retracted with a manual crank, while the nose gear uses a catch-and-rope ...

  4. Take Off Merlin - Wikipedia

    en.wikipedia.org/wiki/Take_Off_Merlin

    The 1100 has an empty weight of 195 kg (430 lb) and a gross weight of 400 kg (882 lb), giving a useful load of 205 kg (452 lb). With full fuel of 60 litres (13 imp gal; 16 US gal) the payload is 162 kg (357 lb). [1] [2] Merlin 1200 Model introduced in 2006 and powered by a four-stroke, 95 hp (71 kW) BMW 1200 GS engine. The 1200 has an empty ...

  5. Sea and Sky Cygnet - Wikipedia

    en.wikipedia.org/wiki/Sea_and_Sky_Cygnet

    The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category and the US light-sport aircraft rules. [2] [3] It features a strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, retractable wheeled tricycle landing gear and dual floats and a single engine in pusher configuration.

  6. J & J Ultralights Tukan - Wikipedia

    en.wikipedia.org/wiki/J_&_J_Ultralights_Tukan

    Data from Cliche and Kitplanes General characteristics Crew: one Capacity: one passenger Length: 7 ft (2.1 m) Wingspan: 35 ft (11 m) Height: 10.6 ft (3.2 m) Wing area: 190 sq ft (18 m 2) Empty weight: 250 lb (113 kg) Gross weight: 750 lb (340 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Rotax 447 twin cylinder, two-stroke, single ignition aircraft engine, 40 hp (30 kW ...

  7. Apollo Jet Star - Wikipedia

    en.wikipedia.org/wiki/Apollo_Jet_Star

    The Jet Star was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US light-sport aircraft category. It features a cable-braced or strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.

  8. AOL Mail

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    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. Fly Hard Trikes SkyCycle - Wikipedia

    en.wikipedia.org/wiki/Fly_Hard_Trikes_SkyCycle

    Data from Bayerl General characteristics Crew: one Wingspan: 32 ft 10 in (10.0 m) Wing area: 160 sq ft (14.9 m 2) Empty weight: 205 lb (93 kg) Gross weight: 400 lb (181 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Kawasaki 340 two cylinder, air-cooled, two stroke snowmobile engine, 32 hp (24 kW) Propellers: 3-bladed composite Performance Maximum speed: 65 mph (105 km ...

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