1973 Piper Seneca I

Piper Seneca I is a twin-engine light aircraft developed by Piper Aircraft. It was introduced in 1973 and is powered by two Lycoming IO-360 engines. It is an all-metal, low-wing, six-seat aircraft with retractable tricycle landing gear. The Seneca I has a cruise speed of 145 knots and a range of 615 nautical miles. It has stall speeds of 64 knots and is capable of performing short field takeoffs and landings. The Piper Seneca I is a great option for pilots looking for a reliable and economical twin-engine aircraft.