What was found
INSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.