What was found
INSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01.