Piper PA-28 Cherokee 160 — Performance Data

This document provides performance data specifically for the Piper PA-28 Cherokee 160. It is intended for pilots and aviation enthusiasts who require detailed information about the aircraft's capabilities. The data includes critical performance metrics such as takeoff and landing distances, climb rates, and fuel consumption under various conditions. Understanding this information is essential for safe and efficient flight operations. The document serves as a reference for flight planning and operational decision-making, ensuring that pilots can maximize the aircraft's performance while adhering to safety standards.

• Takeoff distance at sea level: 1,600 feet
• Climb rate: 730 feet per minute
• Landing distance on dry runway: 1,500 feet
• Cruise fuel consumption: 8.5 gallons per hour
• Maximum takeoff weight: 2,550 pounds