The Bell CTR-1900 was an all-new 19-passenger design. It was the result of a trade comparing the V-22 high-wing and H-tail configuration and new configurations (low-wing and conventional tail or low-wing, V-tail and canard). The CTR-1900 configuration with the V-tail and canard had the lowest drag and weight. This aircraft would have used two 3440shp Rolls-Royce/Turbomeca RTM-322 engines.
Technical data for Bell CTR-1900:
Wing span: 11.28m, rotor diameter: 8.53m, overall length: 14.20m, take-off weight: 10328kg, cruising speed: 524km/h, range: 1180km
Source:
http://www.aviastar.org/helicopters_eng/bell_ctr-1900.php