What was found
LT WING PRESSURE DECK ANGLE CRACKED IN Y AND X AXIS. E/C PERFORMED AMO 46-90 IAW NTM NED OF CRACK MARKED IN X AXIS CRACK EXTENDS BEYOND FASTENER IN Y AXIS END OF CRACK MARKED. RIVET REMOVED FOR ROTOTEST INSPECTION IAW SRM 51-25-01. E/C HFEC & ROTO TEST PERFORMED AMO 46-90 IAW NTM NO CRACK IN FASTENER HOLE NO CRACKS ON ITEMS. RIVET INTALLED IAW SRM 51-25-01. PRC APPLY ON BOTH CRACKS IAW DO/TS-333/08-9783 COMPLIED WITH EC/TC DO/TS-333/08.