What was found
FRAME TO LONGERON FITTING WAS CRACKED AFT SIDE, STA 820, ABOVE LONGERON 22 RIGHT. REPLACED FITTING IAW DC-8 DWG 4753360, SRM 53-1-0 AND 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME TO LONGERON FITTING WAS CRACKED AFT SIDE, STA 820, ABOVE LONGERON 22 RIGHT. REPLACED FITTING IAW DC-8 DWG 4753360, SRM 53-1-0 AND 51-1-20D.