What was found
THE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING HMV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING HMV.