The Jabiru J250 is one model in a large family of two and four seat Australianlight aircraft developed as touring aircraft and provided in kit form by Jabiru Aircraft. The aircraft was also assembled and sold in the US by Jabiru USA as a Light Sport Aircraft (LSA).
The J250 is constructed from composite materials. The 30 ft (9.1 m) span high wing is strut-braced. 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 two-seat cabin features a width of 44 in (112 cm). The J250 shares the same fuselage as the four-seat J450 model, the difference being that the rear seats are not installed on the J250. As a result, the baggage area in the J250 is among the largest in its class.
A two-seater, designed as a US light-sport aircraft, with a large baggage compartment behind the seats.
Jabiru J250
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
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 SP has a cruise speed of 185 km/h (115 mph)