As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT INBOARD FLAP PANEL 584EB, LEADING EDGE CHAFFED. (C-CHECK) RO 3/25/2021 ORIGINAL MATERIAL .090 (IAW CRJ 700 SRM 57-52-01-001-001-A01) AFTER REWORK .067 MAT LOSS .023 MAXIMUM ALLOWED .015 PANEL 584EB FOUND TO BE OUT OF LIMITS. ORDER NEW PANEL 584EB PART# CC670-14177-1. LOCATED AND DRILLED HOLES IN NEW PANEL. PER REF. CRJ700 SRM 51-40-11-001-001-A01