As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON INFLATION OF THE UNIT, UPPER TUBE IS NOTED WITH TEAR ON THE FABRIC ABOUT .25 INCH LOCATED CLOSE TO PRESSURE RELIEF VALVE. HOLE GOES THROUGH ON TOP AND BOTTOM PART OF THE UPPER TUBE. THE PRESSURE RELIEF VALVE BAND CLAMP SCREW IS NOTED WITH SHARP EDGES THAT CUT THROUGH THE CLAMP COVER AND UPPER TUBE FABRIC. INSPECT PRV SCREW FOR SHARP EDGES AND REPLACE AS NECESSARY.