What was found
(CAN) WE HAVE CRACK ON OUR VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE ON AFT LHS . THE CRACK IS .750 INCH LONG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) WE HAVE CRACK ON OUR VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE ON AFT LHS . THE CRACK IS .750 INCH LONG.