What was found
CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LEFT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED FASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LEFT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED FASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M)