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