What was found
NUMEROUS AREAS OF CORROSION ON ALL STIFFENERS ON PANEL NR 191MM. REMOVED CORROSION AND TREATED AREAS WITH NEG MAT LOSS IAW SRM 51-10-01 AND 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMEROUS AREAS OF CORROSION ON ALL STIFFENERS ON PANEL NR 191MM. REMOVED CORROSION AND TREATED AREAS WITH NEG MAT LOSS IAW SRM 51-10-01 AND 51-10-02.