Thought I would chime in with our experience running ethanol car gas in our C172 for close to 5 years….. important to note it has a GM V8 fuel injected engine but most of the fuel system is stock up to gascolator. We used different testing methods, such as borescopes, oil analysis, computer engine logging and analysis, 40 micron filter elements, ECT…
Our goal was to find a cheaper, mostly mass produced composite solution, more environmentally friendly solution than legacy engines ( engines are biggest culprit of high op costs), and had to use different fuel types so it could be flown anywhere. Thus, the V8 engine was low laying fruit. Ethanol was a concern from early design due to mostly ancient air frame fuel systems and materials. Without boring anyone with engineering mumbo jumbo, we were especially concerned about leaks forming which would be significantly more dangerous in our pressurized fuel system than stock gravity feed system, for obvious reasons.
The engine wasn’t an issue as it was designed for ethanol, and controlled by essentially a computer and software, which could figure out most efficient mixture (and spark delivery) regardless of fuel type used, or combo thereof. But the c172 tanks, lines, fittings, valves, ECT… were an issue. I had considerable experience in the marine sector where ethanol is a real problem due to humidity ambient conditions, as well as systems within a structure that took a beating compared to car suspensions. I also spoke to many experimental guys using car gas and read what I could.
There is a lot of misunderstanding and in many cases ignorant know it alls without any related first hand experience voicing opinions. So here’s what I can add to this topic from experience with our c172 over close to 5 years…. We did, and do, run different fuel types, including AVGAS, and tested all in flight testing, but majority of time run low octane ethanol car gas now, mostly due to lower cost and emissions.
First off, when initially converting or using ethanol gas realize that it’s a real cleaning solution and will break up contamination in all parts of the system, even those existing for decades. Really important to clean the older system prior and monitor filters to know when it’s absolutely clean. This could take several days or even weeks if the plane remains mostly static as opposed to fuel swishing around in flight. It took about 2 weeks before we were confident all existing junk was out of system.
Realize the seals such as o rings in most aircraft may be decades old and/or not compatible with ethanol, and will cause leaks. We left some of the original o rings in place as a control to see effects…. after bout 5 months the original wing tank sump began leaking, and was also replaced with a Viton material o rings. But nothing that big of a deal. Since log books didn’t say how long the o ring was there, there’s no reliable way of knowing its condition, so leak may have occurred with AVGAS, but I don’t believe any such failure would be a safety issue anywhere in a gravity fed or low pressure systems. However, in a high pressure system, even a small leak on the pressurized side could be significant hazard, to say the least. We basically put an updated o ring and seal kit together (along with new cap seals ) that was part of the conversion kit. Easy solution. It’s important to remember, if the certified o ring in 1950 was basic rubber, that still may be the same material used in new replacements…. So don’t assume every such part is modern when it comes to certified parts.
My post getting long so will just add this RE water…… true, ethanol absorbs water from air, but it’s not a huge sponge as some will have you believe. Aircraft have more protection from water contamination than cars or boats due to tank and low sump drains. For our c172, if all seals are good the only air contact to fuel is the small vent tube. I wouldn’t use ethanol gas in humid environments if you rarely fly, especially if not hangered , but we’re talking 4 months or more (but ethanol evaporates quick compared to other heavier octane additives and thus octane rating decreases, so long storage or old fuel bring other potential concerns…but agin, no big deal for most users). If ethanol is a concern, there’s always non-ethanol REC gas locally available which is over 90 octane and slightly more cost than regular gas…. We use this if we know the plane won’t be flying much for a a while and it’s readily available at near by gas stations next to our airport.
With anything, there’s trade offs ……ethanol fuel for us has the pros well outweighing the cons….. our now high performance c172 went from about $78/hr to less than $24hr to fly…… a few friends used it to train and take check rides in, earning their certificates at a fraction of the cost of renting or flying own c172 which cost being their biggest obstacle in getting their licenses. A couple of local CFI s are building time flying it to air shows and can’t believe the same vintage c172 rents for $175/hr at their school, and happy they are not burning lead.
I was asked to write a technical paper about our c172 testing with ethanol a ways back, but free time is scarce, but will post a link here if I do. To sum it up, the hype of airframe fuel systems vs ethanol is just that, hype, in most cases. We didn’t test ethanol with the original O-320 engine, but expect any issues could likewise be mitigated as many use car gas in such engines, especially air boats and experimentals. …. But I have no first hand experience so not qualified to comment. Leaded AVGAS days are numbered, and as FAA loves creating legacy monopolies regardless of cost to GA, approved fuels will further increase costs…. I expect to see STC’d fuels to be $2 more than AVGAS in most markets, and continue higher once AVGAS is phased out….again, another FAA sponsored monopoly. Further decreasing GA market size, and accelerating higher costs as demand dwindles with fewer innovators wanting to invest in viable solutions based on such market projections.
Sorry for longer than needed post.