The first prototype flew in 2002 and was followed by four more T-10 pre-production aircraft. These were followed by a batch of production
T-10M machines for purchase as complete aircraft. The production of kits may follow. The T-10M has some changes to undercarriage and fin, plus a change of engine. The main gear sprung element has been moved from the half-axle to the rearward V strut and the early castoring nosewheel replaced with a steerable system with a simpler single leg. The fin of the T-10M is more angular and narrower than that of the T-10 and incorporates a triangular
fillet. The T-10s are powered by 60 kW (80 hp)
Jabiru 2200s, the T-10Ms by 74 kW (100 hp)
Rotax 912S flat four engines. ==Operational history==