As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SX NR 6500161617 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN AROUND STR26L ,BETWEEN STA1788 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X = 0.002" < 15%, FOUND WITHIN LIMITS AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.