Someone posted:
- Flying club member accidentally destroyed engine by running the temps too hot during their long flight.
- The A&P says the damage caused from long periods of excessive leaning and the flight data reflects dangerously high EGT's during that one members flight that would cause such damage.
I saw that post, and I call BS - On the part of the A&P.
I've had a bunch of A&Ps tell me that I was gonna kill my engine running it LOP. I noticed that they were the same ones telling me I'd never make TBO in my IO-550 regardless of mixture setting.
I'm 500 hours over TBO now, and I don't listen to those guys any more.
I take off full rich unless I'm in the mountains. I lean in the climb (I have an EGT gauge with a helpful little green range marked "Climb" that's great for this), though that is still ROP. After leveling off and accelerating to cruise, I leave the throttle wide open (unless I'm on a low/short flight), pull the prop back to 2300, and lean until all 6 cylinders are LOP at a normal cruise altitude around 8-10K. If I'm higher, I'll lean closer to peak, if I'm in the oxygen altitudes I'll be rich of peak just to get more power.
Can someone explain to me what is excessive leaning?
Well, if the engine quits, you have leaned excessively.
Anything below 50-100 degrees LOP is going to stop detonating (my understanding), so you cannot lean any more.
And in this case we're not talking about the bad "detonation" or "pre-ignition" or any of the damaging stuff, we're literally talking about making power at all. Yes, more than 100 LOP you're probably pretty close to the engine quitting if it hasn't already by then.
Also, how can a lean engine on a long flight overheat and be destroyed? I thought leaning was better for the engine.
Starting from full rich, leaning is good, and then it's bad, and then it gets good again. Running at high internal cylinder pressures and high cylinder head temperatures is what's bad for the engine. That 50º ROP range that lots of people and documents recommend is about the worst place to be.
If you want to learn everything you need to know about running a piston engine, start here:
https://avweb.com/features/john-deakins-engine-related-columns/
It mystifies me why we all quote Mike Busch as the authority and not Lycoming and Continental, who have serviced and warrantied far more engines than Busch will see in his lifetime.
I was gonna type this all up but
@Roger Wilco did it for me (quoted below). The guy who did the research is George Braly, and along with his friends John Deakin (author of the columns linked above) and Walter Atkinson they brought those findings to the rest of the community. Busch merely took that and ran with it. Braly is the only one of the original three who's still alive, so I'm glad someone (Busch) is still doing it.
I’m not a SavvyAviation customer, and everyone here should know by now that I have a low IQ.
Operating LOP is not a “Busch thing.” It’s a technique that has been researched and utilized at least as far back as WWII. A few decades back, George Braly developed a set of balanced fuel injector nozzles, tuned to each individual engine, so that LOP operation can be accomplished safely. Braly, at GAMI, built a test cell and has accumulated thousands of hours of data (not anecdotes). The Red Box (Busch calls it the “red fin”) was developed from that test data. Braly, along with Walt Atkinson and John Deakin, developed a roadshow they called Advanced Pilot Seminars that served as a training class to teach pilots how to operate LOP safely using GAMI injectors and an engine monitor, based on the data and lessons learned from testing and development. Busch seems merely to have adopted Braly’s research and operating principles. It’s worth noting that Busch’s SavvyAviators has collected and analyzed tens of thousands of hours (probably much more) of data downloads from customers’ engine management instrumentation*. My impression is that Savvy relies on that data when advising customers regarding engine issues.
If anything, GAMI and Savvy may be the most data-driven engine operation resources that GA has ever had. Now, tell me about the anecdotes you spoke of, and please dumb it down so that a low IQ person such as yours truly can grasp your point.
*Edit to add thousands of borescope images from customers’ engines.
I should add, go read Deakin's columns and then we can talk. There's plenty of reasons not to like Busch, but he's not wrong, and Braly backs it up with real data.
I agree. Busch is a maintenance guy. Anything he says WRT engine operating parameters is either anecdotal or second hand. I'm much more inclined to listen to Lycoming, Continental, and/or other researchers who do long term work with these engines on the dyno.
Braly has done a lot of "long term work with these engines on the dyno."
My absolute favorite engine monitor feature is % HP.
It's not that hard to determine even if you don't have it.
One way is that if you're normally aspirated, you can't be at more than 75% power above about 8,000 feet, and you can't be at more than 65% power above 11,500 feet. There's simply not enough air left at those altitudes to develop any more power than that.
If you're rich of peak, your power is limited by mass air flow; if you're lean of peak your power is limited by fuel flow. There's the old GPH * 14.9 = HP for lean of peak, so for my 280hp engine, 65% power is 182hp or 12.2 gph. For rich of peak, you can use (Actual MP/29.92)*(Actual RPM/Max RPM) to calculate the percentage of airflow compared to maximum. If you're at 25 squared on an engine with 2700 RPM max, (25/29.92)*(2500/2700) = 0.774 or 77.4% power.
This is how the engine monitors do the calculation, anyway... But neither formula is perfect. If you're way out at either extreme, you can affect the speed of the burn to the point where it's no longer as effective at being converted to mechanical power. For example, if you go to 100ºF LOP, you're probably borderline in terms of developing any power at all, and you'll certainly be less than 50%, but you'll still be pumping more fuel through the system than the formula would indicate.
Actually it’s really easy to design a 6 cylinder aircraft without cowl flaps that provide proper cooling in at low speeds, it’s keeping the engine at proper temperature in cruise flight without cowl flaps that is the issue.
FWIW, my M20R Ovation is a 6 cylinder aircraft without cowl flaps that does quite well with cooling at most speeds. I do tend to climb with faster airspeeds most of the time, but that's just because I want to go fast and Vy to altitude isn't fast. My Vy is 105 KIAS, book cruise climb speed is 120 KIAS, and in lower altitudes I usually climb at "Vz" which is 138 KIAS in my plane and still do over 1000 fpm.