N225X BE35 at Cambridge Bay Airport. Aircraft was travelling to Eureka. 
From the FAA, Installed temporary fuel system resting on plywood supporting on existing aircraft structure. Plywood base is installed to facilitate even load distribution. Aircraft floor loading limits are not exceeded the ferry system consists of 1 aluminum tank. The tanking system total capacity is 50 U.S. gallons. Tanks are constructed from .090 5052-H34 aluminum welded at all seams, internal baffles are installed and welded into place. Construction of tanks meets the standards of U.S. Coast Guard 33 C.F.R. 183.580 specifications. tanks are pressure and leak tested in accordance with FAR 23.965a(1) at point of manufacture: Williams Manufacturing, Tracy, CA. all tanks are securded to seat tracks with cargo tie downs. These tie down straps are of identical type that have been utilized in previously FAA approved tanking systems. Straps, (2 each) secure the tanks longitudinally and laterally. Ferry fuel tanks are electrically bonded to the airframe to facilitate static discharge, and are vented to the atmosphere, as outlined in AC43-13-1b. The ferry tanking system is plumbed into the aircraft fuel system as noted on the aircraft fuel system schematic. This is co-located with, and is a part of the ferry fuel management details locate in attachment 1 of the tanking installation package. Aircraft ferry fuel system operation and management details is outlined in attachment 2. Continuous airworthiness compliance not applicable due to temporary installation. <a rel="nofollow" class="external text" href="http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=225X">FAA Registry N-Number Inquiry Results</a>
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