Diamond DA62 — Other Documents

This document is the Type Certificate Data Sheet (TCDS) for the Diamond DA62, issued by the European Aviation Safety Agency (EASA). It provides essential information regarding the aircraft's certification, technical characteristics, operational limitations, and operational suitability data. The DA62 is a twin-engine, low-wing aircraft designed for up to seven occupants, featuring a composite structure and retractable landing gear. This TCDS is crucial for operators and maintenance personnel to ensure compliance with safety and operational standards. It outlines the aircraft's specifications, including dimensions, engine details, weight limits, and performance data, which are vital for safe operation and maintenance of the aircraft.

• Maximum take-off weight: 1999 kg (4407 lb)
• Maximum operating altitude: 6096 m (20,000 ft)
• Total fuel capacity: 196.8 liters (52 US gallons)
• Maximum structural cruising speed: 160 KEAS
• Minimum control speed airborne: 75 KEAS