What was found
INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14.