What was found
INSPECTION FOUND A 1 INCH CRACK IN SUPPORT CHANNEL AT BASE OF VERTICAL FIN. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN SUPPORT CHANNEL AT BASE OF VERTICAL FIN. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.