What was found
CRACK DAMAGE WAS DISCOVERED ON THE RH FRAME 5 BEHIND THE RADIUS APPROXIMATELY 1.00” ABOVE THE FWD ATTACHMENT FITTING FOR THE AVIONICS PLATE. THE CRACK IS APPROXIMATELY 1.35” IN LENGTH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK DAMAGE WAS DISCOVERED ON THE RH FRAME 5 BEHIND THE RADIUS APPROXIMATELY 1.00” ABOVE THE FWD ATTACHMENT FITTING FOR THE AVIONICS PLATE. THE CRACK IS APPROXIMATELY 1.35” IN LENGTH.