I read somewhere that KR wings were tested to destruction in Australia and they failed at the wing/fuselage transition. Mac KR2 G-BVZJ ----- Original Message ----- From: "Orma" <o...@aviation-mechanics.com> To: "KRnet" <kr...@mylist.net> Sent: Sunday, December 12, 2004 5:47 PM Subject: KR> Static load testing of KR wing
> Does any one know if the KR wing (original or skins) ever underwent static load testing. Has Dan ever load tested his wing skins. > > Orma > Southfield, MI > N110LR celebrating 20 years > Flying, flying and more flying > http://www.kr-2.aviation-mechanics.com/ > _______________________________________ > Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net > > please see other KRnet info at http://www.krnet.org/info.html
