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#1
January 11th 06, 10:33 PM
posted to rec.aviation.homebuilt
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eLSA certification
In reviewing the definitions from the FAA na dfrom comments posted in this newsgroup, there seem to be some special opportunities when building aircraft that could fit LSA derfinitions. If my understanding is correct, it would be possible for someone to build (for instance) a Van's RV-6a with a Lyc O-235 or Conti O-200 and a ground adjustable prop set to its extreme climb configuration to limit speed to 138 mph. As long as the plane's max TOW is stated to be 1320 lbs, that would fit the LSA category. Is this assumption correct? TIA, CV 
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