What was found
DURING C-CHECK, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 79, STRINGERS 3L-4L. MX REAMED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02796. 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, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 79, STRINGERS 3L-4L. MX REAMED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02796. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.