As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
- PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 1.5" AFT OF STA132 AND LOOKING AFT AT 1 O'CLOCK. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.080", THE DEPTH OF CLEANUP X=0.004" <15%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-01-1A-1 FIG 101 REVISION NO.122 APR 15/2023.