Piper PA-28 Dakota — Performance Data

This document provides performance data for the Piper PA-28 Dakota, a six-cylinder aircraft powered by a Lycoming engine. It includes specifications on engine performance, weights, dimensions, fuel capacity, and various performance metrics such as speed, climb rate, and takeoff distances. The information is crucial for pilots and aviation enthusiasts to understand the aircraft's capabilities and limitations. The document serves as a reference for flight planning and operational procedures, ensuring safe and efficient flight operations.

• Engine: Lycoming 0-540-J3A5D, 235 hp @ 2400 RPM
• Gross Weight: 3000 lbs (1361 kg), Useful Load: 1392 lbs (631 kg)
• Maximum Speed: 148 knots (274 km/h)
• Takeoff Distance: 825 ft (251 m) ground run, 1725 ft (526 m) over 50 ft obstacle
• Service Ceiling: 17,500 ft (5334 m)