06 May 2025, 05:59 [ UTC - 5; DST ]
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Post subject: Re: Legacy Citation vs Turboprop Posted: 13 Dec 2023, 23:38 |
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Joined: 08/05/16 Posts: 3137 Post Likes: +2282 Company: Tack Mobile Location: KBJC
Aircraft: C441
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Username Protected wrote: Note that both the PT6 and TPE331 are reverse flow designs, which has nothing to do with which direction the engine happens to be bolted to the airframe. Sort of. The PT6 has the intake at the rear, exhaust at the front, so the OVERALL flow is reverse of plane direction (except in pusher configuration like the Piaggio). Ironically, the reverse flow combustor in the PT6 actually has the air moving front to rear. Attachment: cCw2d.png The only part of the TPE331 that is reverse flow is the annular combustor. Outside of that, the air generally moves front to back (except in pusher configurations like the MQ9 Reaper). Attachment: Garrett-TPE331-turboprop-engine-based-on-18-p-15-3-A-main-shaft-engine-shaft.png So it is correct to say they both have reverse flow COMBUSTORS, the PT6 is generally mounted so that it is overall reverse low and the TPE331 is generally forward flow. Mike C.
Reverse flow refers to the combustor design, so there’s no sort of.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 13 Dec 2023, 23:51 |
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Joined: 12/03/14 Posts: 19944 Post Likes: +25013 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Reverse flow refers to the combustor design, so there’s no sort of. What terminology distinguishes the general flow through a PT6 versus a TPE331? The flow is radically different, the PT6 is back to front, the TPE331 is front to back. What is the term you would use for that? I'd call it a "reverse flow engine". This will allow you to diligently maintain the terminology purity of "reverse flow combustor", which is just one part of the engine, not the overall engine itself. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 01:00 |
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Joined: 11/06/20 Posts: 1604 Post Likes: +1679 Location: Tulsa, OK - KRVS
Aircraft: C501SP
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Username Protected wrote: The light bulb just came on.
There is a requirement that the available mask must be one-handed quick donning. There is a requirement that we wear a mask solo above FL350.
There is no requirement that we have to wear the quick don mask above FL350.
We need two masks - one for long term comfort, and one for quick donning.
Who makes one? I’ve heard military masks designed for constant wear are much more comfortable than quick dons. Can we use those? My plane came with Aerox masks and they are quite comfortable. The key is that you can inflate or deflate the harness to get just the right tension. Highly recommend. https://www.aerox.com/4110-725-quick-do ... -headgear/
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 01:05 |
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Joined: 11/06/20 Posts: 1604 Post Likes: +1679 Location: Tulsa, OK - KRVS
Aircraft: C501SP
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Username Protected wrote: can you expand on this? what limitations are there on updating the interior on, say, a 501? seems like trimmer seats and lighter colors would add a lot of "open feel." My plane came with a fully redone interior. The seat backs are lower than others I've seen. It really opens up the cabin. Here's a picture I took when I replaced the overhead lights with LEDs so that was there I was focusing the shot. Attachment: IMG_20210915_1351337.jpg That upgrade also modernized the interior by having much brighter and cooler (both thermally and color-wise) interior lights.
Please login or Register for a free account via the link in the red bar above to download files.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 01:56 |
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Joined: 08/05/16 Posts: 3137 Post Likes: +2282 Company: Tack Mobile Location: KBJC
Aircraft: C441
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Username Protected wrote: Reverse flow refers to the combustor design, so there’s no sort of. What terminology distinguishes the general flow through a PT6 versus a TPE331? The flow is radically different, the PT6 is back to front, the TPE331 is front to back. What is the term you would use for that? I'd call it a "reverse flow engine". This will allow you to diligently maintain the terminology purity of "reverse flow combustor", which is just one part of the engine, not the overall engine itself. Mike C.
The PT6 and TPE331 both have the same folded combustor design. It’s referred to as a reverse flow engine (generally) or more rarely and verbosely as a reverse flow combustor design in all of the literature I have read.
In some installations of either engine, it is installed with the intake in the rear and the exhaust in the front, or out the side (helicopter). Saying this is also “reverse flow” overloads the term and is confusing. I suppose you could say “reverse flow installation in this specific installation of this reverse flow combustor design” but seems much easier and less confusing to just say the engine is installed backwards.
It’s a term I let annoy me more than I should, like referring to all star systems as Solar systems, or old timer’s disease, the non-existent word nucular, and airplane hangErs.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 11:48 |
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Joined: 11/22/12 Posts: 2813 Post Likes: +2767 Company: Retired Location: Lynnwood, WA (KPAE)
Aircraft: Lancair Evolution
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Username Protected wrote: What terminology distinguishes the general flow through a PT6 versus a TPE331? The flow is radically different, the PT6 is back to front, the TPE331 is front to back.
just say the engine is installed backwards. But it's not, it's installed as designed. An inaccurate and misleading term is not an improvement over an overloaded one. BTW, while the 'intake in back' airflow seems odd to modern eyes, in the piston world P&W came from, it was the norm. Air entered through the carburetor (inlet) in the back and went forward through the supercharger (compressor) to the cylinders (burner cans) and was exhausted out the sides, just as in the PT6Attachment: sectioned R2800.jpg
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 15:37 |
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Joined: 11/06/20 Posts: 1604 Post Likes: +1679 Location: Tulsa, OK - KRVS
Aircraft: C501SP
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Username Protected wrote: Hey Chris, anyway you can publish your LED bulb part numbers as a service to humanity. Hi Mike! Happy to help. I bought them from here: https://aircraftlighting.com/products/l ... ing-light/It's the L1309W (W is for warm). I believe they also have a cooler color option but my wife likes her lights on the warm side (decries pure white or blue tinged as being too "Battlestar Galactica"). I replaced all of the cabin lights plus the two that shine on the instrument panel from above and just behind the flight deck seats. I never figured out how to open the two at the front of the flight deck ceiling next to the air vents but have never used those lights anyway so stopped trying.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 14 Dec 2023, 15:42 |
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Joined: 08/31/17 Posts: 1743 Post Likes: +703
Aircraft: C180
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She must be cool if she knows Battlestar Galactica.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 15 Dec 2023, 16:23 |
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Joined: 12/03/14 Posts: 19944 Post Likes: +25013 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: "Under $500" is an apt description, only the smallest engines are meaningfully far away from that number. The rate of rise is particularly alarming, 5 X inflation. It doesn't take long at that rate to reach some huge numbers. CJP reached out to Williams and the answers they got are concerning. They foretell a pretty sizable increase in 2025. Williams had the usual litany of excuses. Labor, materials, vendors increasing. Oddly, they mentioned carbon steel going up in price (that's under $1/lb, can't be more than $300 of it in an engine). Raw materials is a red herring. Williams said they had hoped the increase in 2023 would have been sufficient to avoid a big increase in 2024, but obviously that wasn't true. They said in hindsight they should have increased prices more in the past so this year wouldn't be so large. Basically, they apologized for not raising prices earlier. Gee, thanks. Williams said the increase for 2024 was going to be larger but Textron pressured them to make it lower. Can you guess what that means for 2025? Yup, another large increase if Williams thinks they are already being generous in 2024. Textron views the TAP program price as a potential negative factor in sales, and they should. They also said there is nothing they can do, they have to remain profitable. This is incongruent with the fact Textron got them to moderate somewhat, so there is something they did do. The "nothing we can do" excuse falls flat and is posturing in the discussion. I would expect all FADEC FJ44 engines to be over $500 in 2025. Maybe the smallest non FADEC ones will be just under, but only barely. My prediction is a 14% increase. That would make the rates: CJ: $477 CJ2: $529 CJ2+: $524 CJ3+: $536 CJ4: $559 I would also budget out increases at about 3X inflation for the foreseeable future. 2024 was 5X inflation. The Williams contract used to have a CPI escalator clause, that payment increases would be limited to CPI-W. As you might expect, that went bye bye very quickly after Williams enticed the OEMs to use their engines. Every 5 years, Williams can change your contract terms. They never move in your favor. If you don't like them, your only option is to stop payments and "lose" all the "value" you paid into the program. The Williams program was never structured as a balance unlike some programs (ProParts at Textron, or even some engine programs). It is money that instantly vaporizes relative to your account. CJ3+ engine pair over a full overhaul period (5000 hours) at 2025 rates will be about $2.7M. That's a lot to pay for two HSI and two OH. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 15 Dec 2023, 17:38 |
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Joined: 05/23/13 Posts: 7814 Post Likes: +10198 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: Why doesn't Pratt make a similar engine and sell it as an STC for 525's? Because they can’t build enough engines as it is, we have a client with a new Phenom 300E with an engine problem, it’s been down for months, they just got the loaner last week and we were lucky to get it.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 15 Dec 2023, 18:45 |
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Joined: 12/03/14 Posts: 19944 Post Likes: +25013 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Because they can’t build enough engines as it is, we have a client with a new Phenom 300E with an engine problem, it’s been down for months, they just got the loaner last week and we were lucky to get it. Meanwhile, back in JT15D land, we're not having those kind of problems. The Mustang fleet is having loaner shortages as well. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 15 Dec 2023, 19:57 |
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Joined: 01/07/21 Posts: 404 Post Likes: +391
Aircraft: M20J/R, Sr22, SR20
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Username Protected wrote: "Under $500" is an apt description, only the smallest engines are meaningfully far away from that number. The rate of rise is particularly alarming, 5 X inflation. It doesn't take long at that rate to reach some huge numbers. CJP reached out to Williams and the answers they got are concerning. They foretell a pretty sizable increase in 2025. Williams had the usual litany of excuses. Labor, materials, vendors increasing. Oddly, they mentioned carbon steel going up in price (that's under $1/lb, can't be more than $300 of it in an engine). Raw materials is a red herring. Williams said they had hoped the increase in 2023 would have been sufficient to avoid a big increase in 2024, but obviously that wasn't true. They said in hindsight they should have increased prices more in the past so this year wouldn't be so large. Basically, they apologized for not raising prices earlier. Gee, thanks. Williams said the increase for 2024 was going to be larger but Textron pressured them to make it lower. Can you guess what that means for 2025? Yup, another large increase if Williams thinks they are already being generous in 2024. Textron views the TAP program price as a potential negative factor in sales, and they should. They also said there is nothing they can do, they have to remain profitable. This is incongruent with the fact Textron got them to moderate somewhat, so there is something they did do. The "nothing we can do" excuse falls flat and is posturing in the discussion. I would expect all FADEC FJ44 engines to be over $500 in 2025. Maybe the smallest non FADEC ones will be just under, but only barely. My prediction is a 14% increase. That would make the rates: CJ: $477 CJ2: $529 CJ2+: $524 CJ3+: $536 CJ4: $559 I would also budget out increases at about 3X inflation for the foreseeable future. 2024 was 5X inflation. The Williams contract used to have a CPI escalator clause, that payment increases would be limited to CPI-W. As you might expect, that went bye bye very quickly after Williams enticed the OEMs to use their engines. Every 5 years, Williams can change your contract terms. They never move in your favor. If you don't like them, your only option is to stop payments and "lose" all the "value" you paid into the program. The Williams program was never structured as a balance unlike some programs (ProParts at Textron, or even some engine programs). It is money that instantly vaporizes relative to your account. CJ3+ engine pair over a full overhaul period (5000 hours) at 2025 rates will be about $2.7M. That's a lot to pay for two HSI and two OH. Mike C.
Mike, thank you for this update, it is really informative.
The one question I have for owner operators, and flight departments. Would you rather pay now to a healthy Williams, or pay later if they are not solvent, not able to provide the services of the plan when you go to use them years later. You know, kind of like Social Secruity!
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