What was found
INSPECTION FOUND A .25 INCH CRACK IN AFT FUSELAGE LEFT VERTICAL STABILIZER ATTACH ANGLE. THE ANGLE WAS REPLACED IAW EA 5340-01012.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN AFT FUSELAGE LEFT VERTICAL STABILIZER ATTACH ANGLE. THE ANGLE WAS REPLACED IAW EA 5340-01012.