ADVANCED ULTRALIGHT
Always stored in hangar and kept in perfect condition - never involved in accidents - single owner.
Non-deductible VAT sold by private individual 70.000 total price

Airplane time state:
TTAF h.884
TTE Rotax 912 ULS 100HP replaced August 2022.
TOTAL hours new engine 90 to date.

Radio 8.33 Dittel KRT2.
Transpoder Trig TT21 Model S.
Avmap Geopilot2+
Analog anemometer.
Analog FT altimeter.
ELT AK-450
Analog m/s variometer.
MAP control.
RPM control.
Televel left and right fuel tank.
Fuel pressure control.
Double EGT control.
CHT control.
Oil pressure control.
Oil temperature control.

Electric retracted gear - dual indicators for electrical and mechanical operation.
Emergency release of the trolley from the cab.
Woodcomp Vario 170/2R propeller variable pitch in flight.
Treatment of the sheet metal at the origin.
USH 52-S Softpack Magnum ballistic parachute.
Analog anemometer.
Analog FT altimeter.
Analog m/s variometer.
Electrical trim control
2-position flap: take-off position 10 - landing position Fowler 35 .
MAP control.
RPM control.
Televel left and right fuel tank.
Fuel pressure control..
AirBox.
Double heating - pilot area and passenger area.
Gascolator.
Digital thermometer for external temperature.
Electronic carbon monoxide detector.

Performance
Cruise 75% power- 200 km/h Kg 370 - MTOW 190 km/h
Flaps landing position - stall kg.370- 50km/h - MTOW 56km/h
Takeoff Rolling kg. 370-75m- MTOW 100m.
Takeoff distance (up to 50ft) kg. 370-150m- MTOW 200m.
Landing distance (from 50 feet) kg. 370-150 m - MTOW 200 m.
Run out distance kg.370- 75 m - MTOW 100m.
Gliding with engine idling Kg. 370 speed 90/100 km/h 1.8 m/s MTOW speed of 90/100 km/h 2.8 m/s
Gliding with engine stopped - flaps take-off position Kg.370 - 90/95 km/h speed 2 m/s- MTOW Speed of 90/95 km/h 3 m/s
Consumption RPM 5500 27 l/h
Consumption 75% power RPM 4300 16 l/h