As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURE INSPECTION WE FOUND THE FUSELAGE SKIN WITH TWO SCRATCHES LOCATED BETWEEN STRINGER 01L AND 01R, JUST FORWARD TO FR 60. THE SCRATCHED AREAS WERE REWORKED BY BLEND OUTS IN ACCORDANCE WITH THE SRM 51-10-03. SINCE BLENDED AREAS ARE LOCATED IN A NON-DAMAGE ALLOWED AREA AS PER SRM 53-22-01 AD51, DUE TO THIS FACT THE DISCREPANCIE WAS REPAIRED IAW EMB ETD2025-190-902018 AND COOPESA ENGINEERING ORDER COO-EO-2025-21727 DTD FEB 18 2025.