Diamond DA40 TDI — Performance Data

This document serves as a performance data reference for the Diamond DA40 TDI equipped with the G1000 avionics system. It provides essential information regarding the aircraft's dimensions, operating limitations, mass and balance, performance metrics, and emergency procedures. The manual is compiled by Peter Schmidleitner and is intended for pilots and aviation enthusiasts who operate or are interested in the DA40 TDI. Key performance data includes takeoff and landing distances, climb rates, and fuel consumption rates under various conditions. The document emphasizes the importance of understanding how density altitude affects engine performance and provides detailed specifications for the aircraft's systems.

• Wingspan: 11.94 m, Length: 8.01 m, Height: 1.68 m
• Max Takeoff Weight: 1150 kg, Max Landing Weight: 1150 kg
• Operating temperature range: -20°C to 54°C
• Cruise speed at 6000 ft and 70% power: 121 KIAS
• Takeoff distance at max weight: 640 m
• Fuel capacity: 28 USG (standard), 39 USG (long-range)