What was found
AT C-CHECK, UPPER LEFT WING TO FUSELAGE FILLET PANEL BRACKET HAS CRACKED 24 INCHES FROM L/E. STOP DRILLED CRACK AND REPLACED BRACKET PER SRM 53-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, UPPER LEFT WING TO FUSELAGE FILLET PANEL BRACKET HAS CRACKED 24 INCHES FROM L/E. STOP DRILLED CRACK AND REPLACED BRACKET PER SRM 53-2-0.