What was found
PIT - DURING C-CHECK, FOUND 2.25 INCH CRACK ON SKIN AT RT WING LEADING EDGE BETWEEN NR 2 AND NR 3 SLAT PANELS UPPER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER MD-80 SRM 57-06B PAGE 11, FIG 4. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING C-CHECK, FOUND 2.25 INCH CRACK ON SKIN AT RT WING LEADING EDGE BETWEEN NR 2 AND NR 3 SLAT PANELS UPPER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER MD-80 SRM 57-06B PAGE 11, FIG 4. (M)