| Jabiru J250 | |
|---|---|
| | |
| General information | |
| Type | Light Sport Aircraft Homebuilt |
| National origin | Australia |
| Manufacturer | Jabiru Aircraft |
| History | |
| Developed from | Jabiru J230 |
The Jabiru J250 is one model in a large family of two and four seat Australian light aircraft developed as touring aircraft and provided in kit form by Jabiru Aircraft. [1] [2] The aircraft was also assembled and sold in the US by Jabiru USA [3] 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.
data from Jabiru [4]
Data from Jabiru Pacific [6]
General characteristics
Performance