As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION WAS FOUND AT FASTENER HOLES ON THE LOWER FUSELAGE EXTERNAL SKIN FS 422 WHERE THE LOWER FUSELAGE TO WING FAIRING ATTACHED TO THE FUSELAGE. AFTER REMOVAL OF THE CORROSION AND EVALUATION THE AFFECTED AREAS THE REMAINING SKIN THICKNESS WAS FOUND TO BE BELOW THE REQUIRED IMINIUMS PER THE CL-350 SRM. ENGINEERING ASSISTANCE WAS REQUESTED. AQRD SUPPLIED REPAIR INSTRUCTIONS AWQRD ERO-982039 REV A DATED NOV 01, 2024.