What was found
RT WING UPPER L/E PANEL 616 ET INNER SURFACE HAS 3 EA CRACKED STIFFENERS. PANEL 616 ET REQUIRES SRM REPAIR IAW SRM 57-10-00, VOL I. MATERIAL VERIFICATION 7075-0 0.040, PO NR 657517.2. FORMED REPAIR STIFFENERS AND FABRICATED REPAIR STIFFENERS IAW SRM 57-10-00, FIG 23, VOL I. RECEIVED HEAT TREATED PARTS 7075-0 TO 7075-T6 IAW DPS 57.00, PO NR 677227.4, MOR 1112893. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED PARTS IAW SRM 51-31-01, VOL II.