What was found
INSPECTION FOUND A .5 INCH CRACK AT SCREW HOLE OF FUSELAGE SKIN, STA 380, BL 0. REPAIRED IAW ECRA 5330-02894.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT SCREW HOLE OF FUSELAGE SKIN, STA 380, BL 0. REPAIRED IAW ECRA 5330-02894.