As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAK), MAINTENANCE NOTED THAT THE AFT DRAG ANGLE HAS A CRACK MEASURING 0.85Ï¿½ LONG WHICH IS LOCATED IN THE RADIUS OF THE DRAG ANGLE. THE CRACK IS LOCATED BETWEEN A PREVIOUS REPAIR AND THE PULLEY SUPPORT BRACKET. THE AFT DRAG ANGLE (P/N 600-31907) IS FABRICATED FROM 60-10229 EXTRUDED 2024-T3511 ALUMINUM. PASSENGER DOOR AFT DRAG ANGLE PLACED ON EA69-2019-068 PERM REPAIR DUE IN 1000FH