As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C6 CHECK - CORROSION FOUND ON STIFFENING ANGLE ON FRAME STA 265.00 BETWEEN STR 26L AND 26R. BLENDED CORROSION IAW SRM 51-21-06-00. BLENDED AREA WITHIN LIMITS OF SRM 53-21-06-101-007-A01, AND 53-11-06-991-805. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-00, 51-25-06-00 AND 51-25-16-00. APPLIED AV-25 IAW SRM 51-21-11-00.