What was found
INSPECTION FOUND A 3 INCH CRACK IN LT WING NR 2 SLAT CHORD ANGLE BELOW WHERE INBOARD STOP PAD MOUNTS. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN LT WING NR 2 SLAT CHORD ANGLE BELOW WHERE INBOARD STOP PAD MOUNTS. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-01.