What was found
INSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11.