What was found
INSPECTION FOUND A 3 INCH CRACK IN RT WING TO FUSELAGE ATTACH FITTING AT FRONT SPAR. A STRAP WAS INSTALLED ON WING TO FUSELAGE ATTACH ANGLE IAW ECRA 5340-0100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN RT WING TO FUSELAGE ATTACH FITTING AT FRONT SPAR. A STRAP WAS INSTALLED ON WING TO FUSELAGE ATTACH ANGLE IAW ECRA 5340-0100.