Piper PA-28RT Arrow IV Turbo — Performance Data

This document provides detailed performance specifications for the Piper PA-28RT Arrow IV Turbo, model PA 28RT-201 T, manufactured by Piper Aircraft Corporation in 1984. It is intended for pilots and aviation enthusiasts seeking comprehensive data on the aircraft's capabilities, including engine specifications, weight limits, dimensions, fuel capacity, and performance metrics. The document outlines critical performance figures such as maximum speed, cruising speeds, fuel consumption rates, and takeoff and landing distances, making it a valuable resource for flight planning and operational understanding.

• Engine: Continental TSIO-360-FB, 200 hp @ 2575 RPM
• Maximum Speed: 178 knots (328 km/h) at gross weight
• Cruise Range: Over 1,560 nautical miles (2,893 km)
• Takeoff Distance: 790 feet (1463 m) ground run
• Fuel Consumption at 75% power: 12.0 gph (45.4 lph)