What was found
CORROSION ON FRAME 68 FWD FA CE AT ANCHOR NUT ABOVE STRINGER 23. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12-283-001, FIG 10102, SHEET 1. REPAIRED THE FRAME IAW SRM 53-41-12-300-001, PRINCIPAL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FRAME 68 FWD FA CE AT ANCHOR NUT ABOVE STRINGER 23. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12-283-001, FIG 10102, SHEET 1. REPAIRED THE FRAME IAW SRM 53-41-12-300-001, PRINCIPAL 1.