The Tecnam P2006T is a twin-engine four-seat aircraft with fully retractable landing gear. The superior high-wing configuration offers stability, superior cabin visibility and easy access for passengers and luggage. Tecnam has used its extensive experience with aluminium airframes to create in the Tecnam P2006 a robust yet very light airframe, resulting in an outstanding payload-tototal weight ratio. The wings are of traditional construction, that is essentially a mono spar configuration. Integral fuel tanks are located outboard of the engines, holding 100 litres each for a total of 200 litres.
Aircraft does not have a valid Certificate of Airworthiness.
Aircraft is not in an airworthy condition.

Airplane time state:
Airplane time state: 907 hours.
Engine type: two Bombardier-Rotax 912S3 engines.
The aircraft is not enrolled on the Tecnam Factory Airframe and Engine programme. Engines and propellers need overhaul.
Aircraft does not have a valid Certificate of Airworthiness.
Aircraft is not in an airworthy condition.

The avionics comprise a standard package: GPS/NAV R/T COM GARMIN GNS 430-1; GPS/NAV R/T COM GARMIN GNS 430-2; HSI INDICATOR KING KI525A; VOR/LOC INDICATOR GARMIN GI106A-1; VOR/LOC INDICATOR MD200-2; TRANSPONDER GARMIN GTX 328; RMI INDICATOR KING KI229; AUDIO PANEL GARMIN GMA 340; DME INDICATOR KING KDI 572; DME KN 63; SLAVING INDICATOR KING KA 51 B; DIRECTIONAL GYRO KING KG 102A; ADF RECIVER KING KR 87; ADF INDICATOR KING KI 227; COMPUTER CONTROLLER S-TEC 55

The aircraft has a history of damage which was rectified by the manufacturer. Specifically, the aircraft has experienced two major events, one of which involved a wheel up landing resulting in damage.
The second involved aerodynamic manoeuvrers that resulted in damage.