What was found
DURING C-CHECK FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R CRACKS AT RIVET HOLE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R IAW EC5330-02978. 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 SKIN AT FRAME 75, STRINGER 1R-2R CRACKS AT RIVET HOLE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 75, STRINGER 1R-2R IAW EC5330-02978. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.