Piper PA-34 Seneca V — Weight And Balance

This document provides essential weight and balance information for the Piper PA-34 Seneca V. It is designed for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe flight operations. The document outlines the maximum takeoff weight, useful load, and specific loading configurations to ensure compliance with safety regulations. It serves as a critical reference for pre-flight planning and weight calculations, ensuring that the aircraft is loaded within its operational limits.

• Maximum Takeoff Weight: 3,800 lbs
• Useful Load: Approximately 1,200 lbs
• Fuel Capacity: 110 gallons (approximately 660 lbs)
• Ensure weight distribution adheres to CG limits
• Example loading scenarios provided for reference.