jj_jetmech
Well Known Member
Is there, will there be or should there be a thread to report and track findings following the inspection of the HS per the SB? Does Vans try to capture any data from owners? How many airplanes as of today have had discoveries/cracks? Is this truly a structural design issue or isolated? Did a crack propagate from poor edge prep and relief or aerodynamic loads and stress? I started my 7 in November tail is complete, SB kit ordered, building fuse now QB wing coming. I'm a career AP/IA and FAA designee (DMIR) so I get it yeah it's an SB I trust VAns and I will do it but I'd like to know a little more before I start drilling.. I plan to wait until just before I mate the HS to the Fuse to comply with the SB. Hoping to Learn more prior to that date.