As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 2 ENGINE UPPER THRUST REVERSER INBOARD SLIDER GOUGED. CORRECTIVE ACTION: BLENDED AREA OF THE NUMBER 2 ENGINE UPPER THRUST REVERSER INBOARD SLIDER REMAINING THICKNESS REMAINING .145MM WITH IN LIMITS IAW BOMBARDIER REO 670-78-34-384 REV D DATE 11/27/2018.