As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 26L AND 25L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .067" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.