What was found
LT LWR WING FRONT SPAR CAP AT L/E ATTACH HOLE SHOWS A 0.500 INCH LENGTH CRACK, STA XFE 523.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-7-09, EVA D857-00261 REV IA DATED 04-27-09, REPAIR SKETCH 200904200125 DWG J060232, JCT04316 REMOVED ACCESS DOORS TO PERFORM REPAIR ENCLOSED SMN FORM 242-2. CUT OUT DAMAGED SECTION IAW REPAIR SKETCH 200904200125 DWG J06232. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND AFTER CUT OUT ENCLOSED SMN-FORM 242-2, EVA DB57-00261 STEP 4. FABRICATED ECCENTRIC REPAIR BUSHING (7075 T6) IAW REPAIR SKETCH 200904200125. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DOS 9.45.36. INSTALLED ECCENTRIC REPAIR BUSHING IAW REPAIR SKETCH 20090420012S REFER TO NR 236109 FOR REMOVAL/REINSTALLATION OF LT WING CTR L/E.