What was found
INSPECTION FOUND A 3" CRACK IN L-ANGLE AT L/H SIDE OF FUSELAGE STA 1106 TO RUDDER JUST BELOW VERTICAL STABILIZER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3" CRACK IN L-ANGLE AT L/H SIDE OF FUSELAGE STA 1106 TO RUDDER JUST BELOW VERTICAL STABILIZER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.