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The MZ 202 was developed first as a 60 hp (45 kW) lightweight competitor to the liquid-cooled 64 hp (48 kW) Rotax 582.Later the MZ 201 was developed from the MZ 202 as a de-rated 45 hp (34 kW) version intended for motorgliders and single place ultralights that needed more power than the single-cylinder Zanzottera MZ 34.
The Firefly was intended to be a FAR 103 legal ultralight that was powered by the heavier 40 hp (30 kW) Rotax 447 engine. The 28 hp (21 kW) Rotax 277 engine was also an option when the aircraft was first offered. [2] [3] [4] The design features a forward fuselage of welded 4130 steel tubing, mated to an aluminum tailboom.
The Barnstormer was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. [2] The aircraft is a single-seat ultralight with an unusual reverse-stagger on its biplane wings, the top wing being behind the bottom wing. The airfoil used is a NACA 2305 section.
Data from Airdrome Aeroplanes & Kitplanes General characteristics Crew: one Capacity: 170 lb (77 kg); no passengers Length: 14 ft 0 in (4.27 m) Wingspan: 21 ft 6 in (6.6 m) Height: 6 ft 0 in (1.83 m) Wing area: 86 sq ft (8.00 m 2) Empty weight: 223 lb (101 kg) Max takeoff weight: 393 lb (178 kg) Powerplant: 1 × Rotax 447 fixed pitch, 40 hp (30 kW) Performance Maximum speed: 76 mph (123 km/h ...
254 The basic ultralight fuselage design, for powerplants of 28 to 45 hp (21 to 34 kW). [1] [2] [3] [6]Superlite Maximum weight reduction fuselage for larger engines of 50 hp (37 kW), with an empty weight of 278 lb (126 kg) when equipped with the Hirth F-23 engine of 50 hp (37 kW).
Huntair Pathfinder Mark 1 ultralight. Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".
Single seat, high wing ultralight, powered by a 28 hp (21 kW) Rotax 277 engine or optionally a 40 hp (30 kW) Rotax 447 or a 50 hp (37 kW) Rotax 503 two stroke engine. [2] [3] [4] Firestar II Two seat, high wing ultralight, powered by a 40 hp (30 kW) Rotax 447 or a 50 hp (37 kW) Rotax 503 two stroke engine. [2] [4] [5] Tandem
The Kolb Ultrastar is an American single seat, high wing, strut-braced, single engine, pusher configuration, conventional landing gear-equipped ultralight aircraft that was produced in kit form by Kolb Aircraft of Phoenixville, Pennsylvania and intended for amateur construction.