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Good day.
I am the Russian owner of G202 #29.
I need help. I have been using this great aircraft for the couple of years- but this year to renew its flight permit our local authorities started to require some sort of "load calculation" for all kitplanes and homebuilds.
I suppose there in no way to calculate composite wings besides static load tests.
Is there any way to get the static load tests of the G202 airframe.
B.R.
Stress test
Hello Mikhail, I have a calkukation from my German Giles. Hope it helps.
stress test
Dear Michael . If you could send it to my email m[at]ranchinskiy[dot]com it will be great.
Stress data
I would also try to contact Richard Giles. His e-mail is in topic "NTSB Report on Newburgh NY Crash".
Structural Substantiation Report
Mikhail, please send me your email address and I will send you a copy of the Structrual Substantiation Report for the G-202. Richard Giles rcgiles@gmail.com
Richard