As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT STA Y=1156 ON TEE CAP INTERNAL RT SIDE BETWEEN LONGERONS 39-40 FOUND CRACK 3 INCHES LONG. REMOVED TEE ANGLE AND INTERNAL DOUBLER IAW SRM 53-40-00 FIG 8 VOL 1. PERFORMED NDT INSPECTION FOUND CRACK 4.3 INCHES LONG. REPAIRED PER SRM 53-40-00 FIG 8 VOL 1.