What was found
LWR FUSELAGE EXTERNAL SKIN HAS TWO CRACKS OF 0.250" AND 0.500", STA 60.000 L-35.8R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 08-02-07, EVA D853-00011 REV IR DATED 03-18-07, DWG AD79-53-103 REV IR DATED 07-19-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DWG AD79-53-103 REV IR. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. NO CRACK NOR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.063") FILLER (AL7075T6 0.050") AND INTERNAL FINGER DOUBLER (AL7075T6 0.032") IAW DWG AD79-53-103 REV IR. CLEANED, TREATED AND PRIMED AREA, FILLER, FINGER DOUBLER AND INNER FACE OF REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS