What was found
IN THIS CASE, FOUND THAT THE B-NUT CONNECTING TO THE FUEL CONTROL FROM THE SPIDER WAS LOOSE. IT WAS NOT LEAKING, BUT REQUIRED A THIRD OF A TURN TO TORQUE DOWN TO PROPER TORQUE. NO OTHER WORK HAS BEEN DONE TO THE SPIDER OR FUEL CONTROL BECAUSE I HAVE DONE THE WORK SINCE NEW ON THIS AIRCRAFT. TT 228.8. REMEMBER FINDING A LOOSE FIREWALL FITTING ON THE FIRST INSPECTION. THIS IS THE SECOND INSPECTION DONE ON THIS AIRCRAFT. IT WAS CERTIFIED 11/11/2004. (K)