TECNAM P2010 TDI — Checklist

This document is the Type Certificate Data Sheet (TCDS) for the Tecnam P2010 TDI aircraft, detailing its certification, technical characteristics, and operational limitations. It includes information on the aircraft's design, performance specifications, and maintenance instructions.

• The Tecnam P2010 is a single-engine, high-wing aircraft with four seats.
• It features fixed tricycle landing gear and is constructed from composite, aluminum, and steel.
• The aircraft has a maximum take-off weight of 1160 kg (2557 lb).
• It is certified under EASA CS-23 Normal category.
• The maximum operating altitude is 12000 ft.
• The aircraft can operate under day/night VFR and IFR conditions.
• It has a maximum flaps extended speed (VFE) of 92 KCAS.
• The aircraft is equipped with a Lycoming IO-360-M1A engine.