What was found
CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT TOP OF WEB FUSELAGE BS 1620-1640 BL 0 INTERCOSTAL WEB. REPAIRED PER SRM 53-60-51 AND 51-10-00. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT TOP OF WEB FUSELAGE BS 1620-1640 BL 0 INTERCOSTAL WEB. REPAIRED PER SRM 53-60-51 AND 51-10-00. (M)