Diamond DA42 VI — Pilot's Operating Handbook

This document is the Type-Certificate Data Sheet (TCDS) for the Diamond DA42 series aircraft, issued by the European Aviation Safety Agency (EASA). It provides essential information regarding the certification basis, technical characteristics, operational limitations, and service instructions for the DA42, DA42 M, DA42 NG, and DA42 M-NG models. The TCDS is intended for use by pilots, maintenance personnel, and aviation enthusiasts who require detailed specifications and operational guidelines for these aircraft. It includes critical data such as weight limits, airspeeds, engine specifications, and operational capabilities, ensuring safe and efficient operation of the aircraft.

• Maximum Take-off Weight: 1700 kg (3748 lb)
• Design Manoeuvring Speed (vA): 119 KEAS up to 1542 kg
• Maximum Landing Gear Operation Speed (vLO): 155 KEAS
• Maximum Operating Altitude: 5486 m (18,000 ft)
• Engine Model: 2 Thielert TAE 125-01 or TAE 125-02-99