As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A STRUCTURAL INSPECTION MAINTENANCE FOUND THE RH CLOSING ANGLE CRACKED 1.5 INCHES RFS 303. CLOSING ANGLE CRACK WAS REPAIRED IAW CAS ENGINEERING EA B1900-53-011, RDA-A-RA16-009/D. ORIGINAL SRM CLOSING ANGLE REPAIR REMOVED AND AN EXTENDED REPAIR ANGLE CUT FROM NEW (-7180) PART EXTENDING FIVE (5) ROWS OF FASTENERS BEYOND AFT OF 1.5Ï¿½ CRACK. ALL AFFECTED AREAS PREPPED/EPOXY PRIMED IAW AMM 20-08-00.