LNP-1

LNP-1 is a light‑utility aircraft developed by Piper Aircraft in the early 1990s to fill a niche between the company’s classic PA‑28 Cherokee family and its emerging turboprop line. The program began in 1989 when Piper’s engineering team identified a demand for a high‑performance, low‑cost trainer that could also serve as a short‑haul commuter. First flight occurred on 12 March 1992, and certification was granted by the FAA in August 1994. Powered by a fuel‑efficient Lycoming IO‑540‑D4A6 engine delivering 300 hp, the LNP‑1 features a semi‑monocoque aluminum airframe, a retractable tricycle landing gear, and a modern glass cockpit with dual Garmin G1000 displays. Its cruise speed of 190 kt, range of 950 nm, and simple maintenance schedule quickly made it popular with flight schools, regional carriers, and government operators. The aircraft’s significance lies in its role as Piper’s bridge to next‑generation avionics while retaining the handling characteristics beloved by pilots of the older Cherokee series. Over 500 units were built before production ended in 2003, and the LNP‑1 remains a valued platform for training and light transport around the world. Today enthusiasts preserve several airframes in museums and active fleets, showcasing the model’s enduring legacy.