As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING FLAP CARRIAGE INSPECTION PER TBM SB 70-048, FOUND LT INBOARD CARRIAGE CRACKED AT LOWER WEB AREA (.5 INCH IN LENGTH). SUSPECT CAUSE IS INSUFFICIENT WEB STRENGTH AND/OR FLAP EXTENSION AT HIGH SPEEDS. REPLACEMENT WITH NEW STYLE CARRIAGE REQUIRED PER TBM MANDATORY SB 70-048.