What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LONGERON 35 LEFT SPLICE FITTING AT FUSELAGE STATION 450. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-53-059-98 AND ENGINEERING ORDER 53-DC8-796.