What was found
INSPECTION FOUND A .5 INCH CRACK IN FORWARD RT OVERWING EXIT LOWER PRESSURE PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, PAGE 1, 51-10-2, PAGE 1, AND 51-30-2, PAGE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FORWARD RT OVERWING EXIT LOWER PRESSURE PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, PAGE 1, 51-10-2, PAGE 1, AND 51-30-2, PAGE 1.