What was found
WING LOWER PLANK UNDER PANEL 193AB CHAFED AT RBL 45. C-CHECK RO 10/20/2020. BLENDED OUT CHAFE ON WING LOWER PLANK UNDER PANEL 193AB AT RBL 45, IAW CRJ200 SRM. ORIGINAL MATERIAL THICKNESS OF LOWER WING PLANK AT REWORKED AREA ZONE A .300. REMAINING MATERIAL THICKNESS AT BLENDED OUT .280 -.304, MATERIAL LOSS IS .020, MAXIMUM ALLOWABLE .040 BLEND ZONE A (SINGLE ASTERISK) >0.150 FROM CSK. FOUND TO BE WITHIN LIMITS, REF REO BOMBARDIER ENGINE DWG.