As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON A LONGERON SPLICE FITTING BETWEEN FUSELAGE STATION 220 AND 240 AT LONGERON 29 RT. REPAIR ACCOMPLISHED BY REMOVAL OF SPLICE FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH ENGINEERING ORDER 53-DC8-432 AND SRM 53-1-0 AND FAA DER APPROVED DRAWING 853-08-97.