As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, FIXED WING LEADING EDGE AT WBL 92.8 INNER VERTICAL SUPPORT 2ND FROM AFT END IS CRACKED AT TOP FASTENER. STOP DRILLED CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER AND FILLER 2024-T3 .050 5 INCH BY 5 INCH AND INSTALLED PER SRM 51-40-2.