As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE WAS FOUND ON THE COCKPIT FLOOR PANEL IN THE FORM OF IMPACT DAMAGE AND CORROSION. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2026-24444A DATED 16 JUL 2026, AIR METHODS ENGINEERING AUTHORIZATION 23-5321-EA-5737 INITIAL REVISION DATED 22 JUL 2026, AND AIR METHODS ENGINEERING AUTHORIZATION 23-5321-EA-5741 REV. 1 DATED 27 JUL 2026. FOR ALL OTHER INFORMATION PLEASE REFER TO WORK ORDER MG #759 ON FILE AT CRS#2A6R933B.