What was found
DURING ANNUAL INSP, A DETAILED ULTRA-SONIC INSP OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT AFT FITTING'S VERTICAL OTBD FLANGE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ANNUAL INSP, A DETAILED ULTRA-SONIC INSP OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT AFT FITTING'S VERTICAL OTBD FLANGE.