Mooney M10 Cadet — Weight And Balance

This document provides critical information regarding the weight and balance specifications for the Mooney M10 Cadet aircraft. It is intended for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe flight operations. The manual outlines the maximum takeoff weight, empty weight, and the necessary calculations for determining the center of gravity, which is essential for maintaining aircraft stability during flight. Additionally, it includes tables and diagrams to assist in the accurate assessment of weight and balance before flight.

• Maximum takeoff weight: 2,400 lbs (1,088 kg)
• Empty weight: approximately 1,450 lbs (658 kg)
• CG limits: 34.0 to 38.0 inches from the leading edge of the wing
• Perform weight and balance calculations before each flight
• Distribute weight evenly to maintain aircraft stability.