As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 600-HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED AT THE CENTER OF THE LH AND RH X-FRAME. THE MAX DEPTH OF DAMAGE ON THE LH SIDE IS 0.018” WITH AN AREA OF 0.040” BY 0.035” THE MAX DEPTH OF DAMAGE ON THE RH SIDE IS 0.013” WITH AN AREA OF 0.020” BY 0.010”. THE DAMAGE WAS REPAIRED BY ADDING REPAIR DOUBLERS IAW AIR METHODS ENGINEERING AUTHORIZATION # 17-5300-EA-5371 REV. - DATE 15 DECEMBER 2025.