What was found
INSPECTION FOUND A .5 INCH CRACK IN LT DORSAL FIN PANEL ATTACH ANGLE. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT DORSAL FIN PANEL ATTACH ANGLE. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.