Mainair Blade
The aircraft was designed as a high-end touring trike, to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of and is also certified to comply with UK BCAR Section "S". The aircraft has a maximum gross weight of . It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear and a single engine in pusher configuration. The aircraft is made from bolted-together aluminium tubing, with its double-surface wing covered in Dacron sailcloth. Its span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The occupants are accommodated in tandem seating, with a fibreglass cockpit fairing that includes a small windshield. Engines factory supplied include the Rotax 503 twin cylinder, two-stroke, air cooled powerplant as well as the twin cylinder, two-stroke, liquid cooled Rotax 582 and the four cylinder, four-stroke Rotax 912UL and Rotax 912ULS. Blades have been used for a number of microlight record distance flights, including a flight to Australia by Colin Bodill and Simon Reeve and a flight around the world by Bodhill. The Blade 912 set the record for London to Sydney by microlight of 49 days (175 hours of flying) at an average speed of . Blade 582
Version powered by a Rotax 582 engine. Price in 2003 was £16,450. Blade 912
Version powered by a Rotax 912UL or the Rotax 912ULS. In 2003 it was reported that the Blade 912 accounted for the majority of customer orders. Price in 2003 was £21,800.
Design and development
The aircraft was supplied as a completed aircraft.