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-   -   Chieftain power setting (https://www.pprune.org/pacific-general-aviation-questions/579936-chieftain-power-setting.html)

Lead Balloon 9th Jun 2016 06:41

You were just testing to see if we were paying attention! :ok:

(If I had a buck for every mistake I make, I'd be the richest man on earth!)

Lumps 9th Jun 2016 12:40


Originally Posted by Jabawocky (Post 9403072)
Lumpy….pretty much :ok:

They probably need about 4 degrees of retard. Now ask the LAME how the CASa dude will cope with that concept :}

Heretic!

So with the (thankfully) retarded timing does the J2BD actually make 350bhp on the dyno - Or did the J series start life with separate mags and then no one checked when the single drives got introduced?

Walter Atkinson 9th Jun 2016 14:29

The J2BD does make rated power with the timing the way it is. Actually, the retarded effective timing helps it produce more power at TO power. Most engines can make more power with slightly retarded timing at TO. The rub is that with fixed timing this results in decreased power at cruise power settings. Hence, the timing "compromise."

Lumps 10th Jun 2016 02:28

bring on PRISM

makes you wonder how the engineers designing these engines arrived at the actual degrees BTDC:

A) Trying various timing positions and seeing what resulted in the optimum compromise, then certifying the engine with said timing position... in which case the difference between fixed and effective timing is of little consequence, as it was the effective timing that was being observed the whole time.

or

B) From theoretical principals i.e., 20°BTDC arrived at from piston velocity, CR.. god knows. seems hard) Without the knowledge that there was a significant delay in effective timing, in which case all these engines must be a bit hit and miss in their timing.

I hope A is closer to reality. Seems more practical and logical.

Jabawocky 10th Jun 2016 03:21

Interesting point to add to Walters comments, depending on load and RPM I have seen the actual spark with a 6 degree lag, but at typical cruise it is in the 4-5 range, so it should be noted that the numbers are always dynamic and one should not get hung up on a "fixed number" state of mind.

I suspect you are right Lumpy, option A is likely, old guys like Walter might know better. And when the independent mag came along nobody would have had reason to give it a second look would they?

Walter Atkinson 11th Jun 2016 15:58

I'm pretty sure they went with option "B", then refined with option "A" if things turned out differently than expected. Many times, the testing to find out if "A" was what they wanted was not attempted. They did "B", ran the tests and if everything was OK, moved on. That's the only thing that seems reasonable for the J2BD.

Lumps 12th Jun 2016 07:59

well that does surprise me. Thanks for your input fellas, will go out and fly the test card shortly!

James McIlvenny 29th Jun 2020 00:21


Originally Posted by Lumps (Post 9399041)
Can someone explain this to me:

In the Piper Chieftain POH, for 65% power (230BHP) it lists 'best economy' fuel flow as 30.8 GPH (both engines). Seeing as the POH specifically prescribes LOP setting, one has to assume that 'best economy' in this case is LOP.

Problem is, these are 7.3:1 CR engines, so using 230 bhp ÷ 13.5 you get 17 GPH, or 34 GPH both engines LOP. How does Piper do it!?

* My guess is the 65% power in the title of the chart refers to the Best Power column.. seeing as TAS is lower for best economy. But it's a guess

I'm about four years late, but I can give it a crack.
In my PA31-350 manual (early), it describes in the footnote for the cruise performance chart that at best economy power, power is reduced by 4.5%.
so 60.5% of 350 is 211.75 hp, using 13.5 to find hp, so that's<!--td {border: 1px solid #ccc;}br {mso-data-placement:same-cell;}--> 15.68 gallons or 31.37 total gph.
However, I have a feeling the best economy the manual refers to is NOT lean of peak, given this plane is from 1973 and the reference to LOP is an update to the flight manual. I bet if you sit on 1650 egt (on the original factory gauge, which really is TIT, based on where the jpi probe sits) you could probably get to 30.8 gph... as your JPI is screaming at you with egt's over 1680 and hot CHTs. I've never tried it, but somebody let me know how you go :)

Xeptu 29th Jun 2020 12:53

Used to fly these PA-31-350 for a few years about a hundred years ago, I'm surprised there are any still flying lol.
Basic facts from memory, where, 31 inches, 2200 rpm, 50 degrees "rich" of peak, I think 1650 (Fahrenheit) sounds about right quoted previously.
fuel burn 150 litres per hour cruise, 180 litres per hour block, over two thousand hours never cracked a cylinder.
From memory, lean of peak came around the time of the mojave when inter coolers were introduced, didn't fly one.
If it's not a turbine why would you even bother :)

machtuk 30th Jun 2020 03:09


Originally Posted by Xeptu (Post 10824464)
Used to fly these PA-31-350 for a few years about a hundred years ago, I'm surprised there are any still flying lol.
Basic facts from memory, where, 31 inches, 2200 rpm, 50 degrees "rich" of peak, I think 1650 (Fahrenheit) sounds about right quoted previously.
fuel burn 150 litres per hour cruise, 180 litres per hour block, over two thousand hours never cracked a cylinder.
From memory, lean of peak came around the time of the mojave when inter coolers were introduced, didn't fly one.
If it's not a turbine why would you even bother :)

yeah about the same for me when driving the old girls a hundred years ago. I remember one owner whom I did the odd charter for said ROP at all times, like you +50 or two divisions, no probs doing that they donks run like Swiss watches👍LOP was a no no back in my day!

Blueskymine 30th Jun 2020 20:45

The complexities of a light piston twin. To complex for an airline pilot.

James McIlvenny 9th Nov 2021 02:48


Originally Posted by machtuk (Post 10824894)
yeah about the same for me when driving the old girls a hundred years ago. I remember one owner whom I did the odd charter for said ROP at all times, like you +50 or two divisions, no probs doing that they donks run like Swiss watches👍LOP was a no no back in my day!

For about the last 1200 hours I ran the chieftain LOP, burning 120 lph instead of 160 lph as I did previously. This was at about the same speed, or faster. When it came time for overhaul, they told me the engines could have run another 500 hours easily. At local fuel prices 40 litres is about $88 Aussie dollars an hour ($65 usd today), about $105,000 AUD in fuel for no apparent damage.
Not to mention there were a huge number of jobs I did that I COULDN’T have completed otherwise, the extended range or greater useful load was a huge plus.
(sorry for the delay, wanted to see how the engines looked after the overhaul before making any statements!)

Lead Balloon 9th Nov 2021 07:05

Who knew that the practical reality would be consistent with science and the data!

holdingagain 10th Nov 2021 07:30

JM, was that achieved with just you flying or multiple pilots

Lead Balloon 10th Nov 2021 07:41


Originally Posted by holdingagain (Post 11139956)
JM, was that achieved with just you flying or multiple pilots

Let me guess: You're worried that JM flew only a few of those 1200 hours and the rest were flown by pilots who 'saved' the engines by running them ROP?

Checkboard 10th Nov 2021 09:28

I would imagine that it’s more: If it was achieved by multiple pilots, then the procedure is not only cheaper, but also robust in terms of engine damage. If was achieved by one, then some specific training may be required to make it that safe, and if you are renting a plane to multiple pilots then it might be best to require ROP ops to avoid damage. $100k over 1200 hours is great, but easily soaked up by a ham fisted pilot detonating an engine.

43Inches 10th Nov 2021 10:04


I would imagine that it’s more: If it was achieved by multiple pilots, then the procedure is not only cheaper, but also robust in terms of engine damage. If was achieved by one, then some specific training may be required to make it that safe, and if you are renting a plane to multiple pilots then it might be best to require ROP ops to avoid damage. $100k over 1200 hours is great, but easily soaked up by a ham fisted pilot detonating an engine.
If they can't read basic instructions on how to run LOP, they probably will fail at setting it properly ROP. Incorrect leaning either side of peak will cause issues on these types of engines, and it's more a lack of basic engine knowledge that is the issue here rather than leaning procedure. If you can't trust them to lean it properly, why are they flying it, you will either have an expensive donk replacement or a hull loss when they run out of fuel mismanaging it.

Lead Balloon 10th Nov 2021 10:09


Originally Posted by Checkboard (Post 11140012)
I would imagine that it’s more: If it was achieved by multiple pilots, then the procedure is not only cheaper, but also robust in terms of engine damage. If was achieved by one, then some specific training may be required to make it that safe, and if you are renting a plane to multiple pilots then it might be best to require ROP ops to avoid damage. $100k over 1200 hours is great, but easily soaked up by a ham fisted pilot detonating an engine.

Most 'big' piston engines will run happily and healthily in a state of mild 'detonation' at most high power settings.

'ROP ops' might 'avoid damage', provided the engine is far enough ROP. But if it's not far enough ROP, that's where the biggest risk of damage arises.

holdingagain 10th Nov 2021 20:24

No Leady you guessed wrong. I was just interested.

Lead Balloon 10th Nov 2021 21:18

Roger. We'll both be looking forward to JM's response, then.


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