Ultraleggeri Usati

Specification:
Date of manufacture – 04/2021
Airframe + engine – 115 mth
Rotax 912ULS2 engine – 100 HP (currently after service), oil and water thermostat, insulated exhaust
pipes, cabin heating, electric fuel pump, LED landing reflector, KLIXON switches
Propeller – DM Prop, 3 blade (on ground adjustable)
MAGNUM 601 parachute rescue system, validity of the revision until 2027
Empty weight – 285 kg, MTOW – 600 kg
Fuel tank capacity – 100 L + 5 L (header tank)
Folding wings – equipped with VORTEX turbulators, LED Strobe and NAV lights
Instrument equipment KANARDIA INDU + artificial horizon KANARDIA, engine instruments KANARDIA
El. controlled trim and el. controlled flaps, radio station TQ – KRT2, transponder TQ – KTX2
Double steering + basic instruments also for the back seat
Differential brakes + parking brake
Beringer main chassis wheels and breaks + Aero Classic; tires, MATCO spur wheel
Towing device TOST + camera with display in cabin

The plane can be tested at the Sládkovičovo (LZSLAD) airport by agreement.

We can offer a specially adapted two-axle trailer up to 750 kg for transporting aircraft too.