What was found
INSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2.