What was found
(CAN) DURING 300 HR INSPECTION THE FLAP BELLCRANK ATTACHMENT BRACKET ATTACHMENT BOLTS WERE FOUND LOOSE. NO DAMAGE WAS NOTED AND HARDWARE WAS RE-TORQUED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING 300 HR INSPECTION THE FLAP BELLCRANK ATTACHMENT BRACKET ATTACHMENT BOLTS WERE FOUND LOOSE. NO DAMAGE WAS NOTED AND HARDWARE WAS RE-TORQUED.