What was found
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.