As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, CONTROL CABIN FUSELAGE FRAME WEB IS CRACKED AT INNER FLANGE AT BS 360 STR 2A RT. REPAIR CARRIED OUT IAW Q/NOTE 17 /2000 AND SRM 53-10-04 FIG 18. STOP DRILLED CRACKS AND FABRICATED NEW REPAIR DOUBLERS ON NDT INSP CLEARANCE FITTED DOUBLERS. APPROVED 8110 ISSUED FOR REPAIR.