What was found
INSPECTION FOUND A .75 INCH CRACK IN LT INBOARD MID FLAP TRAILING EDGE INBOARD CUTOUT AT AFT FLAP EXTEND/RETRACT ROD. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN LT INBOARD MID FLAP TRAILING EDGE INBOARD CUTOUT AT AFT FLAP EXTEND/RETRACT ROD. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.