What was found
PIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01.