1979 Piper Seneca IIMulti-Engine Piston Aircraft

This 1979 Piper Seneca II (N2930V) presents as a well-equipped IFR-capable twin with 8,112 total airframe hours, currently based at KRAP. The aircraft features matched Continental TSIO360EB/LTSIO360EB turbocharged engines with 633 hours since major overhaul (SMOH) against a 1,800-hour TBO, paired with Hartzell three-blade aluminum props showing 706.3 hours SMOH. The avionics suite is highlighted by a modern Garmin G500 TXI glass cockpit with primary flight and multi-function displays, complemented by a GTN 750 GPS, GTX345R transponder, and GFC500 autopilot - all with WAAS, LPV, and ADS-B capabilities. Additional features include a Garmin GI 275 standby instrument, GMA 35 remote audio panel, engine monitoring system, and flight into known icing (FIKI) equipment.

The airframe carries a 1994 exterior paint job and a six-seat interior, with useful load of 1,394.26 lbs at max takeoff weight of 4,570 lbs. Notable modifications include vortex generators and Cies fuel probes. The aircraft's maintenance status shows symmetrical engine and propeller times, suggesting coordinated care, while the comprehensive avionics package positions this Seneca II as a capable cross-country performer with modern navigation and safety systems.