As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DENT/CREASE WAS IDENTIFIED IN THE FORWARD FUSELAGE 1 AREA, LOCATED BETWEEN FRAMES 1A AND 2 AND BETWEEN STRINGERS 15R AND 13R. NO STRUCTURAL DEFORMATION OR ADDITIONAL ANOMALIES WERE OBSERVED. PERMANENT REUNFORCING REPAIR PERFORMED ON RF FWD DUSELAGE SKIN AT FRAME 2 BETWEEN STR 13R AND 15R, REPAIR INCLUDED DOUBLE INSTALLATION.