As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"R/H I/B FLAP VANE IS CHAFED ON THE LEADING EDGE APPROX 8 INCHES FROM O/B EDGE. BLENDED DAMAGE IAW CRJ900 SRM 57-52-01-101-001-A01 TABLE 1 AND CRJ900 SRM 51-12-00-001-001-A01 PARAGRAPH 7, EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 57-52-01-101-001-A01, MAT. ORIGINAL 0.050"", MAT. REMOVED 0.020"", REMAINING THICKNESS 0.030"". REMOVED AND REPLACED PANEL 684HT."