As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, OIL CANNING WAS FOUND ON THE FUSELAGE SKIN CENTER FUSELAGE I BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L. MAINTENANCE REPAIRED THE CENTER FUSELAGE I SKIN BETWEEN FRAME19 AND FRAME 20 BETWEEN STRINGERS 1L AND 2L IN ACCORDANCE WITH ETD 2011-145-108200 AND SRM 53-21-01.