What was found
APPROX TWO 2.25 INCH CRACKS AT NR 1 LEADING EDGE SLAT CHORD WHERE OUTBOARD AND INBOARD UPSTOP PAD MOUNTS. REMOVED AND FABRICATED NEW SLAT CHORD AND INSTALLED IAW SRM 51-10-2 PAGE 4, 51-20-1 FIG 7, 51-30-2 PAGE 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
APPROX TWO 2.25 INCH CRACKS AT NR 1 LEADING EDGE SLAT CHORD WHERE OUTBOARD AND INBOARD UPSTOP PAD MOUNTS. REMOVED AND FABRICATED NEW SLAT CHORD AND INSTALLED IAW SRM 51-10-2 PAGE 4, 51-20-1 FIG 7, 51-30-2 PAGE 1. (M)