What was found
DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79, STRINGER 5L-6L. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501. 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 FUSELAGE CRACKED AROUND RIVET AT FRAME 79, STRINGER 5L-6L. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.