What was found
CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1.