PETAKAS AEROCLUB S.No. 1800, year 1996 model, 250Hp (8.874cc) Fuel Injected Lycoming IO-540 engine, 2 blade Hartzell Constant Speed Propeller, Retractable landing gear, main gear with trailing link suspension, 150 Kts TAS cruise speed, 25 Kts demonstrated crosswind limit, 1.400 Kg MTOW, 490 Kg useful load, 86 US Gal's AVGAS fuel capacity, 6.5 hrs Endurance, 900nm operational range. Two axis KFC150 Autopilot with Altitude Preselect, IFR instrumentation incl. Flight Director, 8,33Khz comm's, ADF, DME. Shadin Air Data Computer, Mode S Transponder, Avidyne TAS605 (Traffic Advisory) displayed in GNS530 GPS, L3 Stormscope, 5 seats. September 2024 Propeller/Governor Overhaul January 2025 Avionics upgrades 1 x GARMIN GFC500 Digital Autopilot 1x GARMIN GNC215 VHF 2 remote unit 1 x GARMIN GTN750 Xi Primary Navigator and COM1/COM2 VHF 2 x GARMIN GI275 as ADI & HSI untis 1 x GARMIN GTX345 ADS-B In-Out Transponder 1 x Garmin GMA35C (remote panel for GTN750 + Bluetooth connectivity) 1 x Garmin GSB15 (USB charger) January 2026 Overhauled IO-540 zero(0) hours Engine.