What was found
INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB CORNER CRACKED AT FASTENER HOLE EXTERNAL FUSELAGE SKIN LENGTH APPROX .25 TO .3125 INCH LONG. FOUND BY EDDY CURRENT. REPAIRED DOOR JAMB IAW DC8 SRM 53-2-0 FIG 16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB CORNER CRACKED AT FASTENER HOLE EXTERNAL FUSELAGE SKIN LENGTH APPROX .25 TO .3125 INCH LONG. FOUND BY EDDY CURRENT. REPAIRED DOOR JAMB IAW DC8 SRM 53-2-0 FIG 16.