What was found
LT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LEFT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. LT DRAG ANGLE REPAIRED PER REO 670-55-31-018. REMOVED PAINT IAW CRJ SRM 51-12-00, VERIFIED CORROSION TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 FIG 102. REPAIR OR REPLACEMENT REQUIRED. REMOVED FLOOR LANDING PLATE, LOCATED AND DRILLED NEW PLATE FS 559+112 - 621 IAW CRJ 200 SRM 51-42-06. CUT NEW FLOOR LANDING PLATE IAW BOMBARDIER REO 601R-53-61-593A STEPS 1 AND 2.