Re: Same old Ethanol question
Agreed. But there is a reason FAA rescinded the approval to use auto fuel in airplanes once ethanol was added. The initial testing that was done before ethanol showed up was extensive and resulted in supplemental type certificates issued to at least two organizations that accomplished the testing to satisfy the Feds. It was mostly around worries about how auto fuel would react to rapid changes in altitude among other things. These STCs covered a range of normally aspirated older design aircraft engines like the 300 CI Continental in my airplane. The aviation community ran auto fuel with no negative effects for many years. Then ethanol came along. After a number of engine failures due to negative reactions to components in the fuel systems (not the least of which was the swelling of neoprene tips on needle valves causing the affected airplanes to become gliders unexpectedly,) the FAA said the STC no longer applies to ethanol gas.
By this time the neoprene tips are gone but the Feds realized there are too many older airplanes out there with fuel systems that could be compromised. And you just can’t change a component in a certified airplane with something else even if it fixes a potential problem without FAA approval. Too much work.
The sad fact is, my engine runs better on auto fuel. There’s too much lead in 100LL. Plugs foul and valves stick. These engines were designed to run on 80/87 octane Avgas. That went away years ago. 100LL was supposed to replace that and the 100 octane that was used by higher performance engines. Unfortunately 100LL has eight times the lead that 80/87 had. So we use FAA approved TCP to help scavenge the lead. It’s like chicken soup “It couldn’t hurt”. If it does any good is anybody’s guess.
Rich
Agreed. But there is a reason FAA rescinded the approval to use auto fuel in airplanes once ethanol was added. The initial testing that was done before ethanol showed up was extensive and resulted in supplemental type certificates issued to at least two organizations that accomplished the testing to satisfy the Feds. It was mostly around worries about how auto fuel would react to rapid changes in altitude among other things. These STCs covered a range of normally aspirated older design aircraft engines like the 300 CI Continental in my airplane. The aviation community ran auto fuel with no negative effects for many years. Then ethanol came along. After a number of engine failures due to negative reactions to components in the fuel systems (not the least of which was the swelling of neoprene tips on needle valves causing the affected airplanes to become gliders unexpectedly,) the FAA said the STC no longer applies to ethanol gas.
By this time the neoprene tips are gone but the Feds realized there are too many older airplanes out there with fuel systems that could be compromised. And you just can’t change a component in a certified airplane with something else even if it fixes a potential problem without FAA approval. Too much work.
The sad fact is, my engine runs better on auto fuel. There’s too much lead in 100LL. Plugs foul and valves stick. These engines were designed to run on 80/87 octane Avgas. That went away years ago. 100LL was supposed to replace that and the 100 octane that was used by higher performance engines. Unfortunately 100LL has eight times the lead that 80/87 had. So we use FAA approved TCP to help scavenge the lead. It’s like chicken soup “It couldn’t hurt”. If it does any good is anybody’s guess.
Rich


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