What was found
(AUS) FUSELAGE FRAME INNER CHORDS LOCATED AT FR 616 AND FR 639 LEFT CRACKED AT THE LOWER RIVET HOLES. 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 CHORDS LOCATED AT FR 616 AND FR 639 LEFT CRACKED AT THE LOWER RIVET HOLES. FOUND DURING EDDY CURRENT INSPECTION.