Diamond DA40 TDI — Weight And Balance

This document provides essential weight and balance information for the Diamond DA40 TDI aircraft. It is intended for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe flight operations. The document outlines the maximum weight limits, center of gravity (CG) calculations, and loading procedures to ensure compliance with safety regulations. Proper weight and balance management is crucial for optimal aircraft performance and safety during flight.

• Maximum takeoff weight: 1,150 kg (2,535 lbs)
• CG limits: 35% to 43% of MAC
• Use the provided weight and balance form for calculations