Piper PA-34 Seneca III — Performance Data

This document provides performance data specifically for the Piper PA-34 Seneca III. It is intended for pilots and aviation enthusiasts who require detailed information on the aircraft's capabilities, limitations, and operational parameters. The manual includes critical performance metrics such as takeoff and landing distances, climb rates, fuel consumption, and weight limits. Understanding this data 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 performance of the Seneca III while adhering to safety standards.

• Takeoff distance at sea level: approximately 1,500 feet.
• Rate of climb: approximately 1,200 feet per minute at sea level.
• Landing distance on a dry runway: approximately 1,200 feet.
• Maximum takeoff weight: 3,800 pounds.
• Cruise fuel consumption: about 12 gallons per hour at 65% power.