What was found
DURING ROUTINE INSPECTION, THE MECHANIC FOUND A CRACK IN THE STIFFENER ANGLE AT THE TOP OF THE VERTICAL TUNNEL ACCESS PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, THE MECHANIC FOUND A CRACK IN THE STIFFENER ANGLE AT THE TOP OF THE VERTICAL TUNNEL ACCESS PANEL.