What was found
INTERNAL FUSELAGE, STRINGER 11R FRAMES 23-23D FLAW INDICATIONS FOUND TO BE CRACKS. REPAIRED PER ATR72 SRM 530000-300-826-A01 REV. 122.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE, STRINGER 11R FRAMES 23-23D FLAW INDICATIONS FOUND TO BE CRACKS. REPAIRED PER ATR72 SRM 530000-300-826-A01 REV. 122.