16 Jan 2026, 15:51 [ UTC - 5; DST ]
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 28 May 2017, 13:30 |
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Joined: 05/23/08 Posts: 6065 Post Likes: +719 Location: CMB7, Ottawa, Canada
Aircraft: TBM - C185 - T206
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For sure, put 300 hp more hp on an aircraft and it always performs better. Username Protected wrote: The Texas Turbine conversion makes the Caravan a much better performing aircraft, especially on amphibious and float planes.
_________________ Former Baron 58 owner. Pistons engines are for tractors.
Marc Bourdon
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 28 May 2017, 13:34 |
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Joined: 11/09/13 Posts: 1910 Post Likes: +927 Location: KCMA
Aircraft: Aero Commander 980
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Username Protected wrote: The other reason is reliability. From the data that I have seen Garretts are less reliable than a PT6 (at least the PT6-67s).
Can the rest of us see that data?
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 28 May 2017, 13:46 |
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Joined: 03/28/17 Posts: 241 Post Likes: +511
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Username Protected wrote: The Texas Turbine conversion makes the Caravan a much better performing aircraft, especially on amphibious and float planes.
I wasn't talking about just the higher horsepower, on amphibians/float planes the Honeywell out performs the Caravan EX (33 shp difference), due to the lag time for spool up on the P&W.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 28 May 2017, 14:40 |
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Joined: 07/23/09 Posts: 1135 Post Likes: +682 Location: KSJT
Aircraft: PC-24 Citabria 7GCBC
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Username Protected wrote: The other reason is reliability. From the data that I have seen Garretts are less reliable than a PT6 (at least the PT6-67s).
Can the rest of us see that data?
viewtopic.php?f=4&t=130028&p=1779834#p1779834
Steve, the PT6 data is good, but for the Honeywell that is the best I could find. If anyone else has better data, please share it.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 28 May 2017, 18:17 |
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Joined: 11/09/13 Posts: 1910 Post Likes: +927 Location: KCMA
Aircraft: Aero Commander 980
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That is for Garrett inflight shutdowns and seems to include any number reasons not associated with the core engine. Just in flight shutdown of the engine for any reason. It also include engines run up to 9000 hours before TBO.
It is not data just a comment.
Both of these engines are much more likely to be shut down because a line replaceable unit has failed than because the core engine failed.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 09 Oct 2017, 20:06 |
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Joined: 12/19/11 Posts: 3308 Post Likes: +1435 Company: Bottom Line Experts Location: KTOL - Toledo, OH
Aircraft: 2004 SR22 G2
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Username Protected wrote: Clearly the story on the Denali is going to be the engine. Too bad this didn't enter the market 5 or 10 years ago. Pilatus has already satisfied the bulk of the demand of this market.
_________________ Don Coburn Corporate Expense Reduction Specialist 2004 SR22 G2
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 09 Oct 2017, 21:14 |
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Joined: 07/23/09 Posts: 1135 Post Likes: +682 Location: KSJT
Aircraft: PC-24 Citabria 7GCBC
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Username Protected wrote: Pilatus has already satisfied the bulk of the demand of this market.
There are still lots of King Airs out there.  . I think the Denali is a defensive move by Textron to prevent losing overall turbroprop market share.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 11 Oct 2017, 00:21 |
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Joined: 12/03/14 Posts: 21089 Post Likes: +26525 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Sounds like they are 3D-printing this engine. That is way cool. :thumbup: Yeah, I want to be one of the first pilots to fly behind a 3D printed entirely new turboprop on a single engine aircraft. It wasn't good enough to be a new design, it also had to have an entirely new manufacturing method as well. It wouldn't surprise me if GE is being teased on this project so Textron can negotiate a lower price on a PT6 at the end. I'd bet my bottom dollar the plane is designed to work with either the GE or the PT6. If GE stumbles, expect a quick change of engines. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 11 Oct 2017, 00:26 |
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Joined: 04/04/14 Posts: 3467 Post Likes: +3024 Location: Boonton Twp, NJ
Aircraft: B757/767
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Username Protected wrote: Sounds like they are 3D-printing this engine. That is way cool.  Yeah, I want to be one of the first pilots to fly behind a 3D printed entirely new turboprop on a single engine aircraft. It wasn't good enough to be a new design, it also had to have an entirely new manufacturing method as well. It wouldn't surprise me if GE is being teased on this project so Textron can negotiate a lower price on a PT6 at the end. I'd bet my bottom dollar the plane is designed to work with either the GE or the PT6. If GE stumbles, expect a quick change of engines. Mike C.
Seen that in the Auto industry when I was an engineer. We had to make a part from a new concept, and there was no mistaking it was made to go back to the old part easily if we couldn't deliver. (GM Truck front axle disconnect actuators)
_________________ ATP-AMEL Comm- ASEL Helicopter CFI/II-H MEI/II A320 B737 B757 B767 BE300 S-70 B767 Requal 04/24
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 11 Oct 2017, 00:37 |
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Joined: 05/31/13 Posts: 1370 Post Likes: +725 Company: Docking Drawer Location: KCCR
Aircraft: C425
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I'm sure if Cessna absolutely had to switch last minute they could do it but I doubt very much they are doing twice the engineering at this point to drop either one in. Imagine all the interface work with the G3000, all the structural differences, all the flight testing and other certification tasks. And I don't believe for a second they are using GE to negotiate a better price from PWC so they can pull a bait and switch at the end. First, Cessna already has no doubt a sweet deal being the premier launch customer for GE. Second, Cessna is promoting the crap out of this engine. If they switched at the last minute with no good reason it would look ridiculous.
_________________ ATP, CFI-I, MEI http://www.dockingdrawer.com
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 11 Oct 2017, 07:24 |
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Joined: 11/08/12 Posts: 12837 Post Likes: +5280 Location: Jackson, MS (KHKS)
Aircraft: 1961 Cessna 172
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Username Protected wrote: It wasn't good enough to be a new design, it also had to have an entirely new manufacturing method as well Might be the only way to make it meaningfully better
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