GOD how I love common sense !  Need a days worth of conversation!  Thanks Mark 

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> On Nov 18, 2021, at 10:43, Mark Langford <m...@n56ml.com> wrote:
> 
> Here's another argument against header tanks that occurred to me yesterday 
> as I was struggling to access some wiring on a plane with a header tank.  All 
> of the space that a header tank (mounted in the "forward deck") occupies 
> gobbles up a lot of valuable space that could otherwise be used for battery, 
> coils, voltage regulator, system electrical bus, and most 
> importantly.....easy access to all of this stuff.  Future additions, 
> alterations, repairs, panel upgrades, electrical bus connections, 
> troubleshooting....all of that stuff is a lot easier to access, with that 
> space available if the fuel is out in the wings instead, in low vertical CG 
> voids that are normally empty anyway!  And if you make the front deck easily 
> removable with piano hinges like I did, access is about 30 seconds away from 
> the decision to open it.
> 
> The unattractive alternative is often to put some of this engine-related 
> stuff on the engine side of  the firewall, which really starts crowding 
> things out there, and subjects the components to constant heat (requiring 
> cooling) and perhaps oil contamination....and will likely result in much more 
> difficult access, and perhaps less opportunity for inspection and 
> troubleshooting.
> 
> See the photo at http://www.n56ml.com/electrical/index.html for what all I 
> had under the front deck, long before I ever even flew the plane.  At first 
> flight it had a lot more out there, like the EIS static/pitot sensor, 
> transponder altitude encoder, fuel pumps and regulator fastened to the aft 
> side of the firewall, etc,  and nowadays it could have all the ADS B stuff 
> under there....with very easy access.
> 
> I've said this before and I'll say it again, I'm not a big fan of "gravity 
> feed" fuel systems.  The head pressure (and therefore fuel pressure supplied 
> to the carburetor) varies depending on the level of fuel in the tank, how 
> well the tank is vented  (plugged by an insect), and even on what kind of 
> maneuvers the plane is doing (stick back or forward).  Some carbs are more 
> sensitive than others to these pressure changes.  A fuel pump and regulator 
> solves this problem by providing constant pressure and flow rate, and also 
> adds the potential for an electric primer without introducing a potential 
> fuel leak (a mechanical primer) into the panel.  A backup battery and a 
> double-pole double throw switch adds redundancy to a level that I consider to 
> be quite adequate....it swaps out both ignition system and fuel pumps to a 
> backup battery that is always fully charged by the alternator, and isolated 
> (one-way) with a 40A diode.
> 
> And most of all, if I were to tear a plane up in an off-airport landing 
> (although I'm sure that would never happen to me......), I'd much rather have 
> the wings on fire than the cockpit, especially surrounded by a hundred "hot" 
> electrical wires right in front of me!
> 
> See http://www.n56ml.com/electrical/index.html
> 
> Mark Langford
> m...@n56ml.com
> http://www.n56ml.com
> Huntsville, AL
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