What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT OUTFLOW VALVE. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 51-10-6, AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT OUTFLOW VALVE. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 51-10-6, AND 51-10-2.