What was found
INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER NR 7 RIB LT NR 9 STRINGER. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-2. A STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER NR 7 RIB LT NR 9 STRINGER. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-2. A STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.