What was found
DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE CRACKED BETWEEN FRAMES 7-8 AND STRINGERS 19R-20R. MX PERFORMED A DOUBLER REPAIR TO THE CRACKED AREA IAW EC5330-02685. 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 FUSELAGE SKIN WAS FOUND TO BE CRACKED BETWEEN FRAMES 7-8 AND STRINGERS 19R-20R. MX PERFORMED A DOUBLER REPAIR TO THE CRACKED AREA IAW EC5330-02685. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.