What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE FUSELAGE SKIN AT STATION 10.000, BETWEEN LONGERONS 28R AND 29R. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION, AND INSTALLATION OF REPAIR FILLERS, AND A REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING ORDER 53-DC8-443 AND FAA DER APPROVED DRAWING 853-021-97.