What was found
DURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, 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 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.