What was found
ON POST-FLIGHT INSPECTION, FOUND 1 EACH .50 INCH CRACK AND 1 EACH 5.50 INCH CRACK IN OTBD SIDE OF NR 1 PYLON AT YN 225.279. STOP DRILLED CRACK ON PYLON PANEL. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED AND SEALED IAW DC-8 SRM TR 54-2-2, FIGURE 6, PAGE 20, PARA. 2 AND SEALED PYLON PANEL IAW DC-8 SRM 51-1-16.