Flydog1966(at)aol.com
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 Posted: Sat May 10, 2008 4:39 pm Post subject: Zenith Builders Analysis Group -- "I'm in" responders -- |
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In a message dated 5/8/2008 7:33:11 PM Eastern Daylight Time, ttp44(at)rkymtn.net writes:
| Quote: | "To attempt to determine whether the structure (including the skin), as designed, has adequate strength to meet the published design loads of ±6G," as well as, for several optional tasks that may be done, if funding is available.
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Just testing to see if it can take +/- 6g ?
I have faith that Chris got that right.
I thought to get to the bottom of this the wing was going to have to be tested for flutter at various fuel loads,
do the ailerons need balancing, what effect wing lockers,and leading edge fuel tanks,etc. Oh,and what about that rear spat attachment?
Would the time and money be better spent on a failure analysis expert to look at the wrecks?
Actually I'm building, the 701, but of course I'm interested to see this all get settled.
please do not archive
Phil Day
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