What was found
DURING C-CHECK, LT FUSELAGE SKIN AT FRAME 77-80 CRACKS AROUND RIVET HOLES. MAINTENANCE PERFORMED REPAIR TO LT FUSELAGE SKIN CRACK AT FRAME 77-80 IAW EC5330-02945. 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, LT FUSELAGE SKIN AT FRAME 77-80 CRACKS AROUND RIVET HOLES. MAINTENANCE PERFORMED REPAIR TO LT FUSELAGE SKIN CRACK AT FRAME 77-80 IAW EC5330-02945. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.