As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 R1 AFT LOWER DOOR JAMB CORNER HAS CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE FOUND BY EDDY CURRENT INSP. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSP AFTER DAMAGE REMOVAL IAW DOUGLAS NDT SPM 06-10-01.001, NO CRACKS NOTED. FABBED DOUBLER TRIPLER & FILLER IAW DC8 SRM 53-2-0 FIG 14.