What was found
INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01.