Sparrow ML is a two-seat, single-engine cantilever low wing UL aircraft with tandem seating. The aircraft has an all composite construction consisting of the carbonfiber sandwich. The wing is of trapezoid shape with main and rear wing spars and is connected to a fixed fuselage midsection of a rectangular shape. The wing is equipped with landing flaps, electrically driven to positions 15° and 35°. The fuselage features a cockpit, tandem seating and a power unit in a pusher configuration. Twin tail booms connect the fuselage with an empennage. The empennage has a shape of double T with a horizontal stabilizer between two fins.
Sparrow ML has the white-red design.
Sparrow ML is equipped glass cockpit for EFIS and EMS, one mechanical airspeed indicator and radio IC-A210E 8,33KHZ.
Rotax 912 ULS 100 hp
Sparrow ML is equipped ballistic rescue system.
Stall speed flaps down 57 km/h
Manoeuvring speed 160 km/h
Maximum cruise speed 210 km/h
Sparrow ML allows to take off and land on the short airfield.