As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, EXTERIOR FUSELAGE VERTICAL STIFFENER ANGLE CRACKED AT LOWER END STATION 950 AFT SIDE OF RIGHT WHEEL WELL AFT BULKHEAD RBL 54 INCHES. STOP DRILLED AS PER SRM 51-10-1. INSTALLED TYPICAL WEB REPAIR AS PER SRM 51-40-2 AT STATION 950 AFT SIDE OF RIGHT WHEEL WELL WITH 2024-T3 MATERIAL .050 5 INCH BY 2 INCH.