As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT HORSE COLLAR CRACKED TWO PLACES ON TOP AFT FLANGE IN RADIUS. REPAIRED TWO EACH CRACKS ON LEFT NACELLE HORSE COLLAR TOP ANGLE BY REMOVING DAMAGE, CRACK DETECT USING EDDY CURRENT METHOD PER NDT MANUAL PSM 1-8-7A, AND INSTALLING REPAIR ANGLE AND PACKERS OF 0.063 TITANIUM, MIL-T-9046 WITH NAS1200M4 AND CR3553-4 RIVETS IAW BOMBARDIER REPAIR DRAWING 8-54-3305. W/O 50373, W/C 4354