As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A CHECK ROUTING INSPECTION THE FOUR BOLTS (AN6-17) AT THE ATTACHMENT OF THE SHOCK ABSORBER OFTHE UPPER PART OF THE BARREL HAVE BEEN FOUND STRIPPED AND THE NUTS LOOSE. INSTALLATION OF THE BOLTS HAS TO BE CARRIED OUT IAW INSTRUCTIONS GIVEN IN THE MESSIER SB 470-32-708 AND MESSIER SB 470-32-709.