Boorabee

The Boorabee is a light multipurpose aircraft, developed by the Australian engineer Tom Cadet. The aircraft’s first prototype took to the skies in 1992, marking its entry into aviation history.

Key Features

The Cadet Boorabee is characterized as a single-seat, strut-braced high-wing monoplane with fixed landing gear. It is equipped with a two-cylinder, two-stroke Rotax 503UL-2V engine, delivering 50 hp (37 kW).

This engine features electronic cooling and dual ignition, driving a three-blade pusher propeller. Its robust and straightforward design made it suitable for various light-duty applications.

Engine and Versions

As alternative powerplants, the 60 hp HKS 700 E engine or the 64 hp Rotax 582 could be utilized, offering operators flexibility. The Boorabee aircraft was manufactured in three main versions.

These included the Mark 1 with a wingspan of 9.14 m (30 feet), and the Mark 2, which featured an 8.83 m (29 feet) wingspan and an extended cabin.

Development and Production

In total, approximately a dozen Boorabee aircraft were built. This production number reflects its limited series nature, catering to a specific niche market for light aircraft.

Technical Specifications

Modification	Boorabee Mk.1
Wingspan, m	9.14
Aircraft length, m	5.85
Empty weight	284
Maximum takeoff weight	554
Fuel, l	94
Engine type	1 Piston engine HKS 700 E
Power, hp	1 x 60
Maximum speed, km/h	167
Cruising speed, km/h	111
Flight duration, h	10
Maximum rate of climb, m/min	152
Crew	1

Image and diagram gallery of the Boorabee

Boorabee	Boorabee
Boorabee	Boorabee
Boorabee