What was found
INSPECTION FOUND A .75 INCH CRACK IN CHORD FITTING AT AFT UPPER INBOARD CORNER OF RT WING INBOARD MID FLAP REAR SPAR, WBL 124.2. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN CHORD FITTING AT AFT UPPER INBOARD CORNER OF RT WING INBOARD MID FLAP REAR SPAR, WBL 124.2. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.