As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT SCHEDULED ROUTINE MAINTENANCE LEFT FUSELAGE HAS CREASED SKIN LOCATED 3 INCHES AFT OF CARGO DOOR BETWEEN FUSELAGE STATIONS 513.00 THRU 544.250 AT STRINGER 9L AND 10L. INSTALLED REINFORCEMENT DOUBLER OF 2024-T3 .050 IN DIMENSION 19.0 IN X 7.0 IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN THE RAYTHEON STRUCTURAL REPAIR MANUAL SECTION 51-70-06.