What was found
* THE RH CABIN FLOOR SILL HAS CORROSION IN MULTIPLE SPOTS BETWEEN APPROX. FS 295 AND APPROX. FS 319. (C-CHECK) RO 2/28/2020 REMOVED CORROSION ON R/H CABIN FLOOR SILL BETWEEN FS 295 TO FS 319, ORIGINAL PART THICKNESS = .063", MATERIAL REMOVED = .036", MATERIAL REMAING = .027", ALLOWABLE BLEND DEPTH = 10% OR .006", BLEND IS"OUT OF ALLOWABLE LIMITS", REMOVED AND REPLACED WITH NEW FLOOR SILL, REF CRJ 200 SRM, BOMBARDIER DWG. C/W RII CARD STRUCTURAL MAJOR REPAIR (**RII**)