As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFING DAMAGE WAS DISCOVERED ON THE LH SIDE OF FRAME 4A BOX FRAME. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-4786, INITIAL REVISION DATED 24 JUN 2024 AND IS SUBSTANTIATED BY FAA FORM 8110-3 BY RYAN D. LEE, DER-Y # 905240204, DATED 26 JUN 2024 WITH DER SPECIFIC SEQUENCE # 24RL019AM.