As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
* L/H SIDE MLG WHEEL WELL STRUCTURE JUST AFT OF FLAP THERE IS CORROSION. FS 559.0 (C-CHECK) RO 2/07/2020 EVALUATED STIFFENER - FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER (P/N 601R32026-95) WITH NEWLY FABRICATED PART. REF CRJ200 SRM AND BOMBARDIER DRAWING.