The Piper PA-28RT-201 Arrow IV represented the final evolution of Piper's retractable-gear Cherokee variant, distinguished by its innovative T-tail configuration designed to reduce cabin noise and improve handling characteristics. First certified on November 13, 1978, it was a low-wing single-engine monoplane that could seat four occupants with retractable tricycle landing gear. Powered by a 200-horsepower Lycoming IO-360-C1C6 engine, the Arrow IV achieved a maximum cruise speed of 138 knots and had a gross weight of 2,750 pounds. The aircraft was manufactured by Piper Aircraft Corporation from 1979 to 1994 with significant production interruptions.
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