Diamond DA40 TDI — Parts Catalog

This document is a Type-Certificate Data Sheet for the Diamond DA40 series aircraft, issued by the European Aviation Safety Agency (EASA). It provides detailed information on the certification basis, technical characteristics, operational limitations, and service instructions for the DA40, DA40 D, DA40 F, and DA40 NG models. The document is intended for use by aircraft operators, maintenance personnel, and regulatory authorities to ensure compliance with safety and operational standards. Key information includes specifications for the aircraft's dimensions, engine types, weight limits, and performance characteristics, as well as references to relevant manuals and service bulletins.

• Maximum take-off weight: 1150 kg (2535 lb) for Normal category, 980 kg (2161 lb) for Utility category.
• Wingspan: 11.94 m (39 ft 2 in), Length: 8.01 m (26 ft 3 in), Height: 1.97 m (6 ft 6 in).
• Engine: Textron Lycoming IO-360 M1A, Max RPM: 2700 for take-off, 2400 continuous.
• Fuel capacity: 156 liters (41.2 US gallons), Usable: 152.2 liters (40.2 US gallons).
• Maximum operating altitude: 5000 m (16,404 ft).