What was found
DURING ROUTINE C-CHECK INSPECTION, A TWO INCH CRACK WAS FOUND ON THE RIGHT WING LEADING EDGE PLATING AT STATION XFS376.000. REPAIR ACCOMPLISHED STOP DRILLING ENDS OF THE CRACK, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 57-22-1, FIGURE 2, 51-1-21 AND ENGINEERING ORDER 57-DC8-710.