09/30/2010. Remarks by Johan Visschedijk: "The MCR-4S was initiated during development of the two-seat MRC-series, with the objective to produce an 100 hp powered four-seat STOL-aircraft. The MCR-4S prototype was registered F-WNEV (c/n 01) and first flew in June 2000. After gaining its CofA it was reregistered F-PNEV on February 6, 2001, on August 1, 2001, Dyn'Aero sold the aircraft to SARL Acticom of Maisons Alfort. March 18, 2003 it was sold to Willem Kooij of the Netherlands, who had it registered in the Netherlands as PH-SKY on September 11, 2006.

The pictured PH-CRM is fitted with an 100 hp Rotax 912S four-cylinder horizontally-opposed liquid/air-cooled engine, and was initially registered in Luxemburg as LX-NIT, before came on the Dutch register as PH-CRM on January 13, 2006."

Span: 28 ft 7.3 in (8.72 m)
Wing area: 89.34 sq.ft (8.30 sq.m)
Weight empty: 772 lb (350 kg)
Max take off: 1,653 lb (750 kg)
Max speed: 199 mph (320 kmh)
Cruise speed: 174 mph (280 kmh)
Climb: 2,461 ft (750 m)/min
Range: 1,147 mls (1,846 km)