What was found
DURING A D2/C1/A3 INSPECTION, DETECTED A MAJOR DENT ON THE FUSELAGE FRAME AT BS 1840, S-11R; CUT OUT THE DAMAGED PORTION OF THE FRAME, PERFORMED HFEC INSPECTION, FABRICATED REPAIR FRAME SEGMENT, HEAT TREATED TO T62 AFTER FORMING; FABRICATED OTHER REPAIR PARTS AS REQUIRED AND INSTALLED IAW EGAT EI: T2012A53B-087.