The J430 is constructed from composite materials. The 31.3 ft (9.5 m) span high wing is strut-braced and features winglets. The standard engine is the 120 hp (89 kW) Jabiru 3300 six-cylinder, horizontally opposed, four-stroke aircraft engine. The tricycle landing gear has optional wheel pants. The four-seat cabin features a width of 44 in (112 cm). Construction time from the factory-supplied kit is reported to be 600 hours. Twenty-five examples were completed and flying by the end of 2011.
A two-seat version of the J430, designed as a US light-sport aircraft, with a large baggage compartment behind the seats.
Jabiru J250
Model similar to the J450, with the back seat removed to give a large cargo area.
Jabiru J400
Four-seat version powered by a 120 hp (89 kW) Jabiru 3300 engine and marketed circa 2004.
Jabiru J430
A four-seater version of the J230 with two seats in the former baggage compartment.
Jabiru J450
Four seat model.
Jabiru SP
Two-seat version for the US light-sport aircraft market, powered by a 120 hp (89 kW) Jabiru 3300 engine and marketed circa 2004. The SP has a cruise speed of 213 km/h (132 mph)
Jabiru UL
Two-seat version for the European microlight category powered by a 80 hp (60 kW) Jabiru 2200 engine and marketed circa 2004. The UL has a cruise speed of 185 km/h (115 mph)
