What was found
DURING C-CHECK, RT FUSELAGE SKIN AT FRAME 75 STRINGER 1R-2R CRACKED AT RIVET HOLE VERIFIED WITH EDDY CURRENT. REPAIRED THE SKIN IAW EC5330-02976. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, RT FUSELAGE SKIN AT FRAME 75 STRINGER 1R-2R CRACKED AT RIVET HOLE VERIFIED WITH EDDY CURRENT. REPAIRED THE SKIN IAW EC5330-02976. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.