As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NO.2 ENG NOSE COWL L/E SKIN AT 10 O'CLOCK FOUND CORROSION. MEASURED THE REWORKED AREA AFT CORROSION REMOVALS, DEPTH OF CLEANUP = 0.037>10% ORIGINAL THICKNESS T =0.080", REMAINING THICKNESS = .043", FOUND EXCEED LIMIT AS PER B767-300 SRM 54-12-01-1A-1 REV 122 APR 15/2023. CARRED OUT THE REPAIR AT NOSE COWL LIP SKIN OF #2 ENG 10 O'CLOCK AS PER EO 5423-080 REV P1. EO 5423-080 REV COMPARED AND COMPLIED WITH EO 5423-080 REV 1R.