As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 512. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN, ADJACENT TO REFUELING PANEL AT STA 512 AS PER SRM 57-10-00 FIG. 25 VOL.I AND SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.