What was found
LT WING UPPER L/E PANEL 516 ET HAS 3 EA INNER STIFFENERS CRACKED. RECEIVED MATERIAL ID 7075-0 0.040 TO FORM 3 REPAIR STIFFENERS AND HEAT TREAT TO 7075-T6 0.040 IAW SRM 57-10-00, PG 83, VOL I. FABRICATED 3 REPAIR STIFFENERS IAW SRM 57-10-00, PG 83, VOL I. APPLIED ALODINE AND PRIME IAW SRM 51-21-01, VOL II. INSTALLED THE 3 REPAIR STIFFENERS IAW SRM 57-10-00, PG 83, VOL I.