What was found
FUSELAGE SKIN CORRODED STA 700.00 STA 708.000 L-32L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER STRAP (ALCLAD 7075 T6 0.090”), REPAIR TRIPLER STRAP (ALCLAD 7075 T6 0.100”), PLATING SEGMENT (ALCLAD 7075 T6 0.125”) IAW SEMAN DWG ED-3961. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3961, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-3-1 PAGE 1, DC-8 SRM 51-3-0 PAGE 1.