Return-Path: Received: from imo17.mx.aol.com ([198.81.17.7]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA24260 for ; Fri, 16 Oct 1998 23:43:26 -0400 Received: from Sky2high@aol.com by imo17.mx.aol.com (IMOv16.10) id 8HVGa04133 for ; Fri, 16 Oct 1998 23:34:49 +2000 (EDT) From: Sky2high@aol.com Message-ID: <1910d0fc.36281059@aol.com> Date: Fri, 16 Oct 1998 23:34:49 EDT To: lancair.list@olsusa.com Subject: 3x0 fuel systems, an observation X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Since sending a description of my simple system (automatically keep the header tank full) to this interchange, it has, subsequently, been most interesting to read about the many systems proposed and those operating ones described. My observation is that most contributors laid out systems that were un- neccessarily complex even though a claim was made that they were "simple". I have read about crossfeeds, fuel selectors, serialized pumps, direct wing feeds, large fuel lines, tada, tada, tada... The contributors' basis for complexity was often obscure, but the theme that comes thru is: I WANT A SYSTEM THAT, REGARDLESS OF FAILURE MODE, WILL ALLOW ME TO COMPLETE MY FLIGHT AS PLANNED! This is an unsafe goal. As a long time subscriber to "Aviation Safety", it always amazes me to see the large number of "pilot failed to manage fuel system properly" as the reason for "prematurely terminated" flights. High among these are failures to position the "selector" valve properly (wrong tank, not in detent, off, etc.) which led me to eliminate any thoughts about incorporating a "selector valve" into the system. A high number of "fuel exhaustion" problems reinforced my desire for an accurate fuel use and quantity reporting system. And, since most problems are a result of a mental lapse, the fuel system had to be simple, but automatic. Note: the only flight in which I relied on using the manual system (fuel pump switches) to alter trim by wing fuel weight, I managed to pump several gallons overboard via the header tank vent by not devoting full attention to the filling process (this did provide useful fuselage air flow data by tracing the blue stain). In addition to safety, I have often heard of problems with interconnected wing tanks, such as non-level parking draining fuel towards the low wing side, etc.... Lancair's design of the 3x0 fuel system is very simple and quite good. It only requires that you hold this truth to be self evident: KEEP THE HEADER TANK FULL AND YOU WILL BE OK! It doesn't matter whether you do this manually or automatically, but if the header is full, you will have the proper reserve (about 1 hour of flight) to find a place to land. In a 320, that could easily result in a range of 200 miles. If the fuel supply system is your concern, always plan the flight path to be within 200 miles of a weather-usable landing site from your present position. The objective of any "major" problem should be to get to the ground quickly and safely so that the problem can be fixed. That's the way one breaks the chain of cascading problems. Since I keep my header full, the fuel transfer pumps are NOT connected to my "essential bus" because if a have a serious electrical problem, I'm heading for the nearest airport. Scott Krueger N92EX