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Aero-Kros MP02 Czajka  The Aero-Kros MP-02 Czajka (English: Lapwing) was designed and developed by Aero-Kros of Krosno, Poland, to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules.
It features a cantilever high-wing, a two seats in side-by-side configuration enclosed cockpit, tricycle landing gear and a single engine in tractor configuration.
 The aircraft is made from carbon-fiber-reinforced polymer. Its 9.72 m (31.9 ft) span wing employs Fowler flaps to keep the stall speed low enough for the FAI microlight category. The standard engine provided is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant which gives a cruise speed of 230 km/h (143 mph). The cockpit is 1.215 m (48 in) wide.
Introduced at the Friedrichshafen Aero show held in in 2009, the aircraft is supplied ready-to-fly.
Since March 2017 the design has been built by HMS Aviation, which is also located in Krosno, Poland.
Aero-Kros MP-02 Czajka
Powerplant: 1 × Rotax 912ULS, 75 kW (101 hp)
Wingspan: 9.72 m (31 ft 11 in)
Wing area: 10.2 m2 (110 sq ft)
Empty weight: 268 kg (591 lb)
Gross weight: 472.5 kg (1,042 lb)
Fuel capacity: 112 litres (25 imp gal; 30 US gal)
Wing loading: 46.3 kg/m2 (9.5 lb/sq ft)
VNE: 146 kt / 168 mph / 270 kmh
Maximum speed: 230 km/h (140 mph, 120 kn)
Cruise speed: 170 km/h (110 mph, 92 kn)
Stall speed: 65 km/h (40 mph, 35 kn)
Rate of climb: 6.5 m/s (1,280 ft/min)
Crew: one
Capacity: one passenger
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