What was found
DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STR 1R AND 2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING CHANGE AND RA EC 5330-02353, AND ACFT APPROVED FOR SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STR 1R AND 2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING CHANGE AND RA EC 5330-02353, AND ACFT APPROVED FOR SERVICE.