What was found
(CAN) 8 INCH CRACK RUNNING LONGITUDINALLY IN BEND OF ANGLE. TOP FORWARD CORNER OF AFT CABIN SEAT STRUCTURE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) 8 INCH CRACK RUNNING LONGITUDINALLY IN BEND OF ANGLE. TOP FORWARD CORNER OF AFT CABIN SEAT STRUCTURE.