I’ll ask my instructor but not gonna see him for awhile thought I’d ask here. Is it possible to kill the engine by mistake by going full rich??
Yes, but you have to be pretty high DA for that to happen. Below 5,000' DA it won't happen directly, but it could happen indirectly as being so rich can foul the plugs in flight which can cause rough running and loss of power.
Also.. if you had an engine failure would one of the first things you’d do is turn on the electric fuel pump? Check the fuel selector? Make sure it’s on both? Then try and start it? If one tank is dry one is 1/2 full and it’s on both will it suck air? Just trying to understand it all %100. Better to learn now. Thanks
It depends on the airplane, so follow the POH procedures for engine failure in flight. If the engine fails in flight you don't know the cause - could be too much fuel, could be too little, could be loss of spark (bad plug or magneto), could be a bird stuffed itself into the air intake. Or 100 other things.
It's worth mention that the ONLY time to use full rich is when using full power at sea level. Or more generally, when using 70+% power (even that doesn't require full rich, but just rich of peak power). As soon as you pull the power back you can lean it. And you should! Even at sea level. If you don't, all you're doing is wasting gas, creating unnecessary pollution, gunking up the spark plugs and valves.
... The point is for high-altitude takeoffs, lean for best performance.
Personally, I'm not sure why that is not the SOP at all altitudes. Potential detonation when the engine can produce 100% power?
Good question. Here's my take on it:
With common standard performance engines that are correctly timed, detonation is not a big risk. Consider that for most of these engines, the STC to run 87 or 91 octane mogas is either paperwork only, or modifications that reduce the risk of vapor lock. Nothing about detonation, so these engines don't need anywhere near 100 octane gas.
The main reason we don't lean for peak RPM at sea level, and when at high DA we set mixture for peak RPM and then a few turns rich of that, is cooling. These engines are primarily air cooled. When climbing, there is less airflow through the cowl because the airspeed is slower than cruise and the angle of the cowl to the air is subobtimal. Yet we're at full throttle producing max power and heat. So we run a bit rich of peak power to have a little extra fuel to help with cooling. When you level off for cruise it resolves both problems, airflow should be sufficient, and you don't need the extra fuel anymore.