What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND FUSELAGE FRAME AT FS 107.00 AND STRINGER 8L CRACKED AT INBD FLANGE TO UPPER FASTENER HOLD, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-071. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION, FOUND FUSELAGE FRAME AT FS 107.00 AND STRINGER 8L CRACKED AT INBD FLANGE TO UPPER FASTENER HOLD, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-071. MAJOR REPAIR.