What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3.