What was found
CRACK ON LT VERTICAL STABILIZER DORSAL ANGLE. ANGLE DORSAL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW ANGLE DORSAL WAS DRILLED AND ADJUSTED IAW SRM 51-10-4, NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT VERTICAL STABILIZER DORSAL ANGLE. ANGLE DORSAL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW ANGLE DORSAL WAS DRILLED AND ADJUSTED IAW SRM 51-10-4, NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.