As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACFT IS FOR A ESCALATION WORK WHEN THE FUSELAGE WAS FOUND CHAFED FROM CONTACT FROM A LANYARD INSIDE RT PYLON. MX INSTALL A DOUBLER OVER BLENDED AREA THAT WAS CHAFED FROM STRINGER 67 TO 68 IAW EC 5330-02698. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.