What was found
INSPECTION FOUND A .50 INCH CRACK WITH CORROSION IN RT FUSELAGE SKIN AT STA 360, STRINGER 23. A REPAIR 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 A .50 INCH CRACK WITH CORROSION IN RT FUSELAGE SKIN AT STA 360, STRINGER 23. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3.