What was found
APPROX .375 VISIBLE BRANCHING CRACK AT LEFT WING NR 2 SLAT WHERE INBOARD UP STOP PAD MOUNTS. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED EXTRUDED ANGLE REPAIR PER 51-4-4 FIG 3. INSTALLED PANELS PER 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
APPROX .375 VISIBLE BRANCHING CRACK AT LEFT WING NR 2 SLAT WHERE INBOARD UP STOP PAD MOUNTS. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED EXTRUDED ANGLE REPAIR PER 51-4-4 FIG 3. INSTALLED PANELS PER 51-30-2.