Richard
Final Approach
Let's hear your opinion of this as applied to "shock cooling" of present day horizontally opposed piston engines on 'spam cans', whether it be a O-200 or -540.

Can't we just talk about treadmills or overhead breaks?
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Not from a design standpoint, but from a materials technology and production quality standpoint. They may look the same, but they are better constructed and inspected, and the metals are of better quality.What change? They're not making engines similar to what our fathers flew, they're making the engines our father flew.
Ya mean like this?Not from a design standpoint, but from a materials technology and production quality standpoint. They may look the same, but they are better constructed and inspected, and the metals are of better quality.

Actually, yes -- back when those engines were originally designed, they would not have been able to figure out what the problem was and now to fix it.
The improvements in materials technology have not changed the situation at all.
the things which could happen if the engine is abused still can.
If you slip with flaps deployed in a Cessna that's certain death, even if your motor somehow survives the shock cooling.
Let 'em. Despite the improvements in quality, the thermodynamic coefficients of the metals involved have not changed significantly, so the risk of extra cylinder/ring wear due to dissimilar cooling rates is also essentially unchanged. As for the risk of quench cracking, it never existed in the first place.I think that Superior, ECI would give ya an argument on that.
If you slip with flaps deployed in a Cessna that's certain death, even if your motor somehow survives the shock cooling.
I'm in!
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There is a jump plane at my airport that Jesse knows well.It takes off full gross, flies up to 10,000' full throttle, climb prop. They pull the throttle back (or run out of gas
) to full idle ( chop and drop) many times a day on weekends, all year long. Never had a problem, engine goes to TBO. Anecdotal evidence, but facts none the less.
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FWIW I don't generally go to idle until in the traffic pattern.There is a jump plane at my airport that Jesse knows well.It takes off full gross, flies up to 10,000' full throttle, climb prop. They pull the throttle back (or run out of gas
) to full idle ( chop and drop) many times a day on weekends, all year long. Never had a problem, engine goes to TBO. Anecdotal evidence, but facts none the less.
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Huh?![]()
I would say we have seen greater improvements/impacts in the oils we use today than material technology.The improvements in materials technology have not changed the situation at all. The things which really wouldn't happen before still won't happen, and the things which could happen if the engine is abused still can.
I'm in!
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There is a jump plane at my airport that Jesse knows well.It takes off full gross, flies up to 10,000' full throttle, climb prop. They pull the throttle back (or run out of gas
) to full idle ( chop and drop) many times a day on weekends, all year long. Never had a problem, engine goes to TBO. Anecdotal evidence, but facts none the less.
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Let's hear your opinion of this as applied to "shock cooling" of present day horizontally opposed piston engines on 'spam cans', whether it be a O-200 or -540.
And a local 182 jump operator considers a 600hour life before cracking on cylinders to be goodI think that is every jump operation. The 182 on our field goes to 11,000 and tries to be the jumpers to the ground and usually succeeds. I have seen him doing s-turns on final, so he wouldn't have to go around, because he was right behind someone.

They better not be running out of gas or the pilot launched without legal VFR fuel minima.![]()
(Or maybe you never posted that online? Ha...)

FWIW I don't generally go to idle until in the traffic pattern.
The typical jump run profile is as follows:
-Full power on takeoff, at gross weight.
-Climb at full power and full RPM for about 30 minutes with cowl flaps open
-Try to time things to where upon reaching 10,500 or 11,500 feet we're on the downwind side of the drop zone flying upwind. Pull power back to about 17" for the jump run.
-Fly straight and level for a few minutes, look around to make sure I'm not about to drop jumpers on some RV doing an overhead break, drop the jumpers
-Reduce power to 15" MP, and RPM to the bottom of the green arc, close cowl flaps
-Try to get the damn door closed
-Roll into a steep bank, peg the VSI going down
-Try to keep an eye on the traffic pattern and crazy rv drivers doing overhead breaks while making yourself dizzy and dealing with your ears wanting to explode
-Try to position yourself to where you can make an entrance into the traffic pattern that'll be safe
-At some point I pull the nose up, go to full flaps, carb heat on, and reduce the power to idle, then land.
It wouldn't surprise me if some of the jump pilots though just chop power to idle when they come down. But one can keep a little power in and still come down fast enough. So that's the SOP that people should be following.
We don't talk about it....... much.![]()
Somebody's having fun combining OWT's.Huh?![]()
Could well be. But oils don't change thermal coefficients, and uneven cooling is the issue with long, low-power, high-speed descents.I would say we have seen greater improvements/impacts in the oils we use today than material technology.
<snip> -Try to get the damn door closed
Seriously...kids these days...The last jumper out doesn't close the door behind him? Was he born in a barn?

And a local 182 jump operator considers a 600hour life before cracking on cylinders to be good![]()
They better not be running out of gas or the pilot launched without legal VFR fuel minima.![]()
(Or maybe you never posted that online? Ha...)
We have a FAA inspector who trolls facebook, fliker etc looking at skydive photos.
His goal?
Catch the jump plane in the background performing "aerobatic" manuvers