As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C3, RADIOGRAPHIC (X-RAY) INSP DETECTED A CRACK ON THE FWD LEFT EMERGENCY OV OVERWING EXIT ON THE UPPER AFT JAMB CORNER APPROX .562 INCH IN LENGTH. NDT VERIFIED CRACK EXISTS IN INTERNAL DOOR PAN. TRIMMED EDGE OF INTERNAL DOOR PAN TO REMOVE CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. TRIM OUT FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0 FIG 6.