TechnologyLeonardo NGCTR tiltrotor demonstrator completes first flight in Italy
Leonardo and the EU Clean Aviation Joint Undertaking completed the first flight of the Next Generation Civil Tiltrotor – Technology Demonstrator (NGCTR-TD) on 19 December at Leonardo’s Cascina Costa di Samarate facility in Varese, Italy.
The NGCTR-TD enters its flight test phase as part of a European project involving 11 partners from several EU countries and the UK. The program aims to advance civil vertical lift by integrating helicopter versatility with the cruise performance of fixed-wing aircraft.
“Building on our established expertise in the tiltrotor domain, bringing this Technology Demonstrator to the air for the first time sets a major milestone on our path to provide a key contribution towards an even more advanced, effective and sustainable use of rotorcraft technologies in Europe,” said Gian Piero Cutillo, Managing Director of Leonardo Helicopters.
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The demonstrator features a cruise speed of 280 knots and a range of approximately 1,000 nautical miles. Its configuration combines an AW609 fuselage with GE Aerospace CT7 engines.
The NGCTR project is part of the Clean Sky 2 initiative, which funds research to reduce environmental impact and improve efficiency in aviation.
Leonardo’s AW609 is an early-generation civil tiltrotor concept that has been under development for many years and has yet to achieve full type certification. It remains a novel aircraft in the civil domain, combining vertical takeoff and landing with fixed-wing cruise by using tilting rotors that provide both vertical lift and horizontal thrust.
The design aims to merge helicopter flexibility with airplane speed and range, but it reflects an older approach to tiltrotor integration, with rotating nacelles, conventional tail surfaces, and systems architecture shaped by long-standing certification challenges.
The NGCTR-TD represents a clear evolution of that concept, not just a testbed but a demonstrator for a future operational configuration. It introduces visible and functional changes, including a V-tail and a simplified tilt system in which only the engines rotate while the nacelles remain fixed.
This reduces mechanical complexity and improves control during the transition between vertical and forward flight. The aircraft is intended to validate a more mature tiltrotor layout, with better efficiency, handling, and integration, serving as the technological bridge toward a new generation of certified civil tiltrotor aircraft beyond the AW609.
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