What was found
(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT STN 616 LEFT CRACKED IN LOWER FASTENER HOLE AFT FACE. FOUND DURING EDDY CURRENT INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT STN 616 LEFT CRACKED IN LOWER FASTENER HOLE AFT FACE. FOUND DURING EDDY CURRENT INSPECTION.