What was found
INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN NR 2 ENGINE INBOARD ENGINE COWL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2. TWO REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN NR 2 ENGINE INBOARD ENGINE COWL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2. TWO REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-0.