What was found
DURING OP 16 MAINT CHECK, FOUND ON FUSELAGE UPPER AFT STOP HOLE HAD CRACK INDICATION .125 INCH LONG PER EDDY CURRENT, AT FWD ENTRY DOOR. INSTALLED DOUBLER AND REPAIRED PER DOUGLAS PRINT SRO 9530252-7001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, FOUND ON FUSELAGE UPPER AFT STOP HOLE HAD CRACK INDICATION .125 INCH LONG PER EDDY CURRENT, AT FWD ENTRY DOOR. INSTALLED DOUBLER AND REPAIRED PER DOUGLAS PRINT SRO 9530252-7001.