Diamond DA40 Tundra Star — Weight Balance

This document provides essential weight and balance information for the Diamond DA40 Tundra Star aircraft. It is designed 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 importance of maintaining proper weight and balance to ensure aircraft performance and safety. It includes detailed charts and tables for calculating weight and balance based on various loading scenarios, ensuring pilots can make informed decisions before flight.

• Maximum takeoff weight: 1,150 lbs (521 kg)
• Empty weight: approximately 1,050 lbs (476 kg)
• Baggage compartment maximum weight: 120 lbs (54 kg)
• Forward CG limit: 35 inches; Aft CG limit: 43 inches
• Use provided charts for accurate weight and balance calculations.