What was found
DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING VISUAL INSPECTION OF WING ATTACH FITTING FOUND CRACKS BETWEEN RIVET HOLES UPPER FWD PORTION OF FITTING (LT AFT WING TO FUSELAGE ATTACH FITTING).