As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UNDERSIDE OF LH ELEVATOR INTERFACE IS CHAFED. REMOVED CHAFING IAW SRM 51-12-00-001-001-A01. PERFORMED U.T. THICKNESS ON L/H ELEVATOR LEADING EDGE REWORK AREAS IAW NDTM PART 01 51-20-004-270-A01. LOWEST REMAINING THICKNESS TO BE .043" OR GREATER. MEASUREMENTS RECORDED ON THE PART. PERFORMED REPAIR BY COMPLYING WITH MHI REO 670-55-21-165 REV-- DATED 7-15-25.