As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ATTACH ANGLE CRACKED BS 294 FWD SIDE OF STUB FRAME RBL 54 WL 208.<[01] REMOVED DAMAGE CLIP I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0; FABRICATION AND INSTALLATION TO BE ACCOMPLISHED ON CCN TTG8Q00WJ92N DUE TO CRACK ON STUB FRAME;[02] VERIFIED CORRECTIVE ACTION 1