$10 Million Approved For Unleaded Avgas Evaluation - AVweb

Congress has approved $10 million for testing and evaluation of unleaded high octane aviation fuels and all sectors currently involved in the effort can qualify for funding. According to AOPA, President Joe Biden signed the bill that funds the executive branch for the coming year on Dec. 29. "The bill also recognizes the collaborative industry-government effort to move general aviation to a fleetwide drop-in, lead-free fuel solution no later than 2030 by including $10 million for additional unleaded fuel testing and evaluation," AOPA said in a news release.


This is a companion discussion topic for the original entry at https://www.avweb.com/aviation-news/281862

I’m curious as to what the price per gallon is for the 100-octane unleaded?

As I’ve said, I DON’T NEED 100 octane in my aircraft.
Unleaded no-alcohol MoGas works for me and I have an STC already from the EAA.
Perhaps the easy economical solution is too reasonable? ( ͡° ͜ʖ ͡°)

As far as I know there are two FBOs selling Swift UL94. Both are located in the great lakes region. It is the same price as 100LL. AirNav had a comment regarding poor availability of UL94 at one of them which does not inspire confidence.

The easy, economical solution would have been to have less ridiculous certification standards and to make robbing manufacturers using legal chicanery punishable by imprisonment. Alternatives would doubtless have been presented decades ago.

You can have your not so economical mogas solution as soon as you pony up for a money losing pump everywhere you want to go. No whining about the cost of disposal for all the gallons that go bad because there isn’t enough demand.

I don’t think it’s the certification standards, really. Yeah, they were a little outdated in some ways, but they weren’t the primary impediment to so much of GA. I don’t even think it’s the requirements for production under Part 21 (which, don’t get me wrong, are still a pain).

Rather, I think the biggest problem is the requirement that private, non-commercial owner-operators of light airplanes must maintain their aircraft in strict conformance to approved type design over the entire life of the aircraft. Nearest I can figure, that came in because either (a) the FAA figured they needed standards for commercial aircraft, just made one set of “one size fits all” standard, and then has refused to change things on the basis of “we only have one set of rules so there can only be one set of rules”, or (b) they figure that every airplane could theoretically be used commercially, and therefore all airplanes need to be conformed at all times just in case. Either way, it’s my belief that the vast majority of these owner-operators do not find this requirement to always be in strict conformance to approved type design to be a major benefit to them, and would be perfectly happy to convert their airplane to another category that frees them from that requirement–even if it’s a permanent one-way conversion (the FAA thinks otherwise, but I think the market would value such aircraft more).

The FAA itself (in the Par 23 ARC report that eventually led to the Part 23 update) even realized this and proposed that older GA airplanes be released from that requirement (look up “primary non-commercial”) and more or less be treated like homebuilts. Unfortunately, the rest of the FAA has been slow to follow suit. I’m holding out hope that this MOSAIC thing eventually leads us down this path.

Swift is expensive AND will need it’s own pump.
UL-E0 MoGas is cheap and will need it’s own pump.
Choose.

My 125hp Tomahawk engine requires 100 octane fuel. Limited choices.

Yep, modified Tomahawk engine requires 100 octane fuel per that STC.

The Aerostar I fly needs 100 octane. Reducing the performance of the engine so it can run on lower grade of fuel is not an option on a piston twin. What little single engine performance there is now would go away altogether.

I will save my $100 for a veggie burger at 6B6. I feel their pain trying to start a new capital intensive distribution system is a daunting task. Mean while I will take the instant gratification and a great burger.

The Swift web site FAQ states the following:
“Will I need a separate tank at my airport for your 100-octane avgas to fully replace 100LL?
No, not according to our current Swift Fuels deployment plan. Our 100-octane unleaded avgas will be fully commingable with 100LL. This means that it can be stored in the same airport tank as 100LL and commingled into the aircraft fuel tanks with 100LL at any ratio. Our avgas deployment plan anticipates that all Swift Fuels products can work effectively with 100LL.”
Nonetheless, since use of Swift fuel requires an STC mixing the two in an airport tank will automatically exclude use of that fuel by any aircraft not having the associated STC. The tank will also therefore need to be clearly signed as “not” being 100LL.

That’s brilliant. I forgot that Swift was designed as a drop-in replacement for 100LL.
That being the case, WHY pay for an STC?

Personally I’d rather see Jet-A replace 100LL. Continental and Austro make diesel engines that burn only 5-6 gph. The DA-62 twin burns less than singles, and is faster. All new airplanes could be diesel.
Obviously the current fleet is limited to gasoline, but with STCs to replace the gas engines with diesel as they reach TBO, we can gradually phase them out.

You have to pay for an STC because the FAA won’t let you change fuels without it. Until they approve a new fuel through the PAFI program.

Here we go … AGAIN !! :frowning:

Give a million to George Braley

Frankly there isn’t a replacement fuel even close to the composition that will be necessary for use as a ‘drop-in replacement’ for all aircraft/helicopters in all operating conditions globally… People need to stop fixating on the narrow range of operations/types (fixed and rotary) that seem to be mentioned over and over and over with some key important combinations of engine type/operating environment/use, being overlooked. I predict that we are looking at least until 2030 before a suitable fuel is formulated and PROPERLY AND FULLY TESTED IN ALL CIRCUMSTANCES and in ALL possibly engine/airframe combinations in a robust way, as this is more critical than most people realise…

Which operations are being overlooked? What additional tests would you require?

There already is, and it has already gone through 10 years of testing. It’s called G100UL.

G100Ul is not compatible with mogas I have heard.