Mooney M20A — Weight And Balance

This document provides the weight and balance information specifically for the Mooney M20A aircraft. It is intended for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe operation of the aircraft. The document outlines the maximum weight limits, center of gravity (CG) ranges, and methods for calculating weight and balance based on various loading scenarios. It is crucial for ensuring that the aircraft is loaded within safe limits for flight operations.

• Maximum takeoff weight: 2,600 lbs
• CG range: 34.0 to 38.0 inches from the datum
• Accurate weight calculations are essential for safe flight