What was found
RUDDER 1 IS CHAFED 5.75" FROM UPPER HINGE LOWER CUT OUT & 5.75" FROM RT EDGE OF LE PANEL. REPAIRED DAMAGE IAW ERS-EM-55MR-426.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RUDDER 1 IS CHAFED 5.75" FROM UPPER HINGE LOWER CUT OUT & 5.75" FROM RT EDGE OF LE PANEL. REPAIRED DAMAGE IAW ERS-EM-55MR-426.