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 ACSN 0493 AT THE RH FRAME 4 INBOARD SKIN. THE DAMAGE MEASURES APPROXIMATELY 0.062” TALL BY 0.175” WIDE WITH A MAXIMUM DEPTH OF .032” (THRU THICKNESS). A DETAILED DESCRIPTION OF THE DAMAGE REPAIR AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-5652, INITIAL REVISION DATED 14 MAY 2026 AND IS SUBSTANTIATED BY FAA FORM 8110-3,