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The Jabiru J230 is an Australian light-sport aircraft, designed and produced by Jabiru Aircraft. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly aircraft. [1] [2] Jabiru J230 Jabiru J230 Jabiru J230 Jabiru J230 Jabiru J230
Jabiru J160 Jabiru J170 US light-sport aircraft two-seat model derived from the J160. [1] Jabiru J200 Jabiru J230 A two-seater, designed as a US light-sport aircraft, with a large baggage compartment behind the seats. [1] [5] Jabiru J250 Jabiru J400 Four seat version powered by a 120 hp (89 kW) Jabiru 3300 engine and marketed circa 2004. [2 ...
2001 model Jabiru SP-470 Jabiru UL-450 Microlight UL450 Interior 2004 model Jabiru J450 2003 model Jabiru Calypso 3300 on amphibious floats at the Canadian Aviation Expo, 2004 Jabiru Calypso 2200 on skis at Montebello, Quebec, January 2005 2200 4 Cylinder Engine 3300 6 Cylinder Engine Jabiru 5100 eight cylinder aircraft engine, now out of production.
Jabiru J200 Jabiru J230 A two-seat version of the J430, designed as a US light-sport aircraft, with a large baggage compartment behind the seats. [1] [4] [5] Jabiru J250 Model similar to the J450, with the back seat removed to give a large cargo area. [5] Jabiru J400 Four-seat version powered by a 120 hp (89 kW) Jabiru 3300 engine and marketed ...
The aircraft is made from composite materials. Its 8.12 m (26.6 ft) span wing has an area of 8.04 m 2 (86.5 sq ft) and mounts flaps. The standard engine available is the 80 hp (60 kW) Jabiru 2200 four-stroke powerplant. [1] The design was developed into the Jabiru J170, by adding the wing from the Jabiru J430, for the light-sport aircraft category.
The Jabiru 3300 is a lightweight four-stroke, horizontally opposed "flat-six" air-cooled aircraft engine produced by Jabiru Aircraft. The engines are direct drive and fitted with alternators, silencers, vacuum pump drives and dual ignition systems as standard. The engine is used to power homebuilt and ultralight aircraft. underside of a Jabiru 3300
In December 2010 the CEA-308, powered by the Jabiru 2200, set four FAI records for aircraft weighing less than 300 kg. It averaged 359 km/h; 194 kn (223 mph) for four runs over the 3-km low-altitude course [ 6 ] and 327 km/h; 176 kn (203 mph) on a 100-km circuit.
The J170 was derived from the Jabiru J160, by using the J160 fuselage and the wings from the Jabiru J430 plus a bigger elevator to give it a better rate of climb at higher density altitudes. It was designed to comply with the US light-sport aircraft rules at a gross weight of 600 kg (1,323 lb).