What was found
CRACKED LT AND RT INTERNAL DORSAL ANGLES BETWEEN JOIN OF VERTICAL STABILIZER L/E AND FUSELAGE SKIN BS 1418. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 5912188, REV BD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED LT AND RT INTERNAL DORSAL ANGLES BETWEEN JOIN OF VERTICAL STABILIZER L/E AND FUSELAGE SKIN BS 1418. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 5912188, REV BD.