As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C/CK, CENTER FUSELAGE LONGERON TO FRAME ATTACH FITTING CRACKED AT STA 902 LONGERON 19 RIGHT. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATION OF NEW FITTING DONE ON AWR 197067.33 OP NR 50025. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.