As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS PUNCTURED AND TRIMMED AWAY OVER AN 8 BY 8 AREA BETWEEN FS 303 AND 311 AND BETWEEN STRINGERS 26L AND 29L. STRINGERS 27L AND 28L WERE SEVERED AND REPAIRED PER SRM. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 363527-14, REV A.