What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.