As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE LH UPPER AND RH LOWER FRAME 5 MEDICAL INTERIOR MOUNT LOCATIONS. THE CRACKS WERE LESS THAN 1.5” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-135-53-048-19, ISSUE B DATED 20 NOV 2019. THE REPAIRS WERE CARRIED OUT PER THIS GUIDANCE WITHOUT DEVIATION.