As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN FRAME AND FRAME FITTING AT STA 35 AND LONGERON 20 - 22. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED FITTING, TREATED AREA IAW DC8 SRM 51-1-8, RECEIVED PART AND INSTALLED IAW DC8 SRM 53-2-6, 53-1-0 FIG 1F. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.