What was found
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE OF INNER CHORD BS 616, FUSELAGE FRAME WL 203 LEFT SIDE. INSTALLED FILLER AND DOUBLER PER SRM 3-10-23 AND EA 65562. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE OF INNER CHORD BS 616, FUSELAGE FRAME WL 203 LEFT SIDE. INSTALLED FILLER AND DOUBLER PER SRM 3-10-23 AND EA 65562. (X)