What was found
EVIDENCE OF CORROSION FOUND ON FRAME FLANGE AT BS 156, STRINGERS 24 TO 25L. INSTALLED NEW REINFORCEMENT ANGLE IAW SRM 51-42-05 REPAIR-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EVIDENCE OF CORROSION FOUND ON FRAME FLANGE AT BS 156, STRINGERS 24 TO 25L. INSTALLED NEW REINFORCEMENT ANGLE IAW SRM 51-42-05 REPAIR-01.