What was found
INSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 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 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2.