As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN AT BS 600 HAS A SHARP DENT WITH A CREASE BETWEEN STR 15L AND STR 16L. REPAIRED WITH SKIN PANEL INSTALLATION -WEIGHT CHANGE FOR THIS REPAIR IS 9.64 LB INCREASE. SCRIBELINE INSPECTION ACCOMPLISHED, BTW BS 439 TO 661 LH BUTT JOINTS AND SKIN LAPS S-14L AND S-19L