What was found
DURING C-CHECK INSPECTION, FOUND FRAME FITTING CRACKED AND CORRODED FS 940 ABOVE LONGERON 24 RT. REMOVED DAMAGED FITTING, CUT NEW FITTING, DRILLED NEW FITTING, SPLICES AND INSTALLED IAW DC8 SRM 53-2-0 FIG 8, 51-1-8, 51-1-21, 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND FRAME FITTING CRACKED AND CORRODED FS 940 ABOVE LONGERON 24 RT. REMOVED DAMAGED FITTING, CUT NEW FITTING, DRILLED NEW FITTING, SPLICES AND INSTALLED IAW DC8 SRM 53-2-0 FIG 8, 51-1-8, 51-1-21, 51-1-20D.