What was found
FUSELAGE SKIN HAS MULTIPLE AREAS OF CORROSION AND FASTENERS PULLING THROUGH FRAME Y898-Y1053 R29-L26. REPLACED SKIN PANEL IAW SRM 51-40. RII COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS MULTIPLE AREAS OF CORROSION AND FASTENERS PULLING THROUGH FRAME Y898-Y1053 R29-L26. REPLACED SKIN PANEL IAW SRM 51-40. RII COMPLETED.