Tecnam P2006T

The Tecnam P2006T is a twin-engine light aircraft in high-wing design of the Italian aircraft manufacturer SRL Costruzioni Aeronautiche Tecnam, which was designed by Luigi Pascale.

History

Since 2007, the twin-engined Tecnam P2006T is with retractable landing gear, two-blade constant-speed variable-pitch propeller ( Hoffman HO- V352 ) with 1.78 m diameter and optional IFR glass cockpit (Garmin G950 ) and FAA certification available. The first flight of the first prototype took place on 13 September 2007, the analog instruments followed on 9 June 2008. Was the second EASA approval of equipped with two Rotax 912 engines and two 100 -liter tanks in the wings aircraft on May 25, 2009. Due to extreme lightweight in large parts built from an aluminum alloy engine performance and in particular the price (about $ 500,000 ) to be achieved by single-engine four- seater. The wings are fitted with winglets and have a NACA 63A - profile with laminar flow. By the middle of 2009 had already received more than 100 orders for the aircraft.

Specifications

(*) With modifications are other values ​​possible.

Incidents

On 2 September 2010 Tecnam P2006T a crashed during a go-around maneuver at the airfield Hirschbachwinkel bei Freistadt ( ICAO: LOLF ) from Upper Austria. A student pilot and a flight instructor were killed.

On 11 March 2011 Tecnam P2006T a crashed during a go-around maneuver onto the airfield Vasilkov UKKW in Ukraine. Four occupants were killed.

On 18 November 2012, a Tecnam P2006T crashed while landing at the airfield of Biberach: from (ICAO EDMB ). The pilot was killed.