What was found
INSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT RT DORSAL FIN LOWER FORWARD ACCESS PANEL. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT RT DORSAL FIN LOWER FORWARD ACCESS PANEL. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.