As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*PANEL 163AB TRAILING EDGE ATTACH ANGLE INNER SIDE CORRODED IN THE WHEEL WELLS (MARKED) ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW STIFFENER P/N 601R32026-131 AT AFT FAIRING (WING-TO-FUSELAGE) FS559.00 BETWEEN RBL38 - LBL38. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, C