As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERNAL SKIN FRAME 35, STRINGER 40R 0.5 INCHES FOUND ONE EACH DENT. COMPLIED WITH EA 6-5330-T0315007. THIS REPAIR WAS CATEGORY B, REQUIRED INSPECTION AT 41600 FC AFTER REPAIR. THE INTERVAL & INSPECTION METHOD WERE TBD IAW RAS 80021897 003 2015. THIS REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 125.