| Qualifying Ultralight / Microlight Aircraft | |
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Classes: weightshift / 3 axis / single seat / 2 seat.
"Microlight" is an aeroplane having no more than two seats, Vso not exceeding 35 knots (65 km/h)CAS, and a maximum take-off mass of no more than:
Note: Foot-launched aircraft are excluded from this definition" |
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| Please visit http://www.quicka.com/gtglobal/pln/ for a very detailed description of Brian Miltons GT Global Flyer | |
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Competing classes (provisional)
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| Equipment Requirements
If this is going to be a Internationally Sanctioned Event, the FAI’s definition of qualified "Ultralights", "Microlights" and "VLA’s" (very light aircraft), is going to have to be trashed out and accepted before serious planning can get under way. Has such a craft been defined yet with certainty? What max empty weight, max all up weight and max fuel capacity are my first questions. Starting from there other solutions can be worked out. Here are some of my personal specifications of what I would call a doable craft:
What? Did you expect to fly only in the calm?
Weight, Weight, Weight, what shall we do to meet those pesky requirements. November 1, 2001 Captain Sivaraman (see country contacts) |
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