Piper PA-28R Arrow IV — Weight And Balance

This document serves as a comprehensive guide for the Piper Arrow PA28R-201, focusing on single-engine aerodynamics, performance metrics, and aircraft systems. It is designed for pilots and aviation enthusiasts, providing essential information on flight characteristics, weight and balance, and operational procedures. The guide includes detailed sections on aerodynamics, speeds, weight limits, takeoff and landing distances, and the aircraft's systems, including the power plant and landing gear. It aims to enhance understanding and operational safety for users of the Piper Arrow.

• Stall speed in landing configuration (VSO) is 55 KIAS.
• Maximum ramp weight is 2,758 lbs; maximum takeoff weight is 2,750 lbs.
• Maximum weight in baggage compartments is 200 lbs.
• Best rate of climb speed (VY) is 90 KIAS with gear up and flaps up.
• The maximum demonstrated crosswind is 17 knots.