What was found
FUSELAGE FRAME UPPER CHORD HAS CORROSION STA 1640, S-22L. AFTER FURTHER EVALUATION IAW DWG NR 146N1023 FRAME THICKNESS IS .080, AFTER BLEND OUT FOR CORROSION REMOVAL, MAT REMAIN IS .077, FRAME IS WITHIN LIMITS IAW SRM 53-00-07 FIG. 101 DET. 2 AND IS A MINOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.