What was found
DURING MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND 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 MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.