As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN FWD SUPPORT ANGLE AT BS 1176 RBL 53-70 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED NEW ANGLE (CLASSIFIED AS A MINOR REPAIR) REF DWG 65-29548-11& 51-30-02.