What was found
FUSELAGE SKIN CORRODED AT STA 980.000 L-29R TO L-30R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-06-08, EVA D853-00045 REV IR DATED 02-22-08 SEMAN DWG ED-4711-1 DATED 02-14-08. REMOVED FASTENERS IAW SRM 51-1-20D, SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW EVA D853-00045 REV IR. PERFORMED NDT INSP IAW EVA D853-00045, DPS 4.707-1. NEITHER CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.050") REPAIR TRIPLER (AL7075T6 0.080") AND FILLER (AL7075T6 0.125") IAW SEMAN DWG ED-4711-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW EVA D853-00045, SEMAN DWG ED-4711-1, SRM 51-3-0, SRM 51-3-1 (TORQUE).