As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"LATE FINDING: CORROSION ON ANGLE STGR 21R BTW FS364 TO FS379. AMAGE ANGLE ON STGR 21RH BTW FS 364 TO FS 379 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6. STGR 21RH WAS MEASURED AS FOLLOW: ORIGINAL THICKNESS 0.080¨, REMAINING THICKNESS 0.038¨ IT WAS FOUND OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01.