13 Dec 2025, 10:43 [ UTC - 5; DST ]
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 08:05 |
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Joined: 11/09/13 Posts: 1910 Post Likes: +927 Location: KCMA
Aircraft: Aero Commander 980
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Look at a
Beech Sundowner or piper Cherokee
Boeing 737 or a Airbus 320
DC-9 or a FK-100
Clean sheet designs that are very similar.
It's just how it is unless you step outside the norm. Like the cirrus jet. Which is still a questionable design.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 08:14 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13086 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: Ok me too. So where does 285 come from? if the Cessna does an honest 285 on less fuel, bigger cargo door, Garmin avionics, more comfortable pilot seats, and lower purchase price what's not to like? Pilatus killer. Sean Botts is the only Pilatus pilot only the planet flying by the torque chart.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 08:31 |
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Joined: 04/24/10 Posts: 9169 Post Likes: +7543
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Username Protected wrote: Look at a
Beech Sundowner or piper Cherokee
Boeing 737 or a Airbus 320
DC-9 or a FK-100 Then look at a V tail Bonanza compared to a ... Nothing. There is no comparison. Iconic. Timeless...
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 08:36 |
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Joined: 01/28/13 Posts: 1102 Post Likes: +291 Location: Salzburg, Austria
Aircraft: PA-18
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I still do not get the logic of the "Denali" name.. Quote: ….Shortt said Textron was well aware of the Denali name as used in GMC’s Denali line of luxury pickup and SUV automobiles, as well as American Champion’s Denali Scout taildragger. “We made a concerted effort in our naming. We wanted it to reflect back to the product’s rugged, refined beauty in a high-end airplane, and the Alaskan heritage link is intentional,” she said….. https://www.aopa.org/news-and-media/all-news/2016/july/25/textron-unveils-denali-single-engine-turbopropOK, as we could imagine also here on BT in previous threads the airplane will be a new variation on the PC-12 theme..new engine, maybe a bit more performance than the present PC12NG version ( although Pilatus probably will not rest on their laurels in that department).. approximately same price.. but why not at least from a marketing point of view come up with a unique new name…? if a "concerted effort" just produced a name which already is used by another GA manufacturer and also a car manufacturer, that does not strike me as much of an effort….
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 11:32 |
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Joined: 07/13/11 Posts: 2755 Post Likes: +2188 Company: Aeronautical People Shuffler Location: Picayune, MS (KHSA)
Aircraft: KA350/E55/DA-62
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Username Protected wrote: SHAWN Botts is the only Pilatus pilot only the planet flying by the torque chart.
LOL well we have 6 pilots flying 4 PCs all flying torque charts, technically you know of 6. Our highest time pilot, has about 6000 hours in PCs. The TEST PILOTS for Pilatus fly torque charts, the SALESMEN do not.
_________________ The sound of a second engine still running after the first engine fails is why I like having two.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 11:42 |
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Joined: 01/16/11 Posts: 11068 Post Likes: +7098 Location: Somewhere Over the Rainbow
Aircraft: PC12NG, G3Tat
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Username Protected wrote: LOL well we have 6 pilots flying 4 PCs all flying torque charts, technically you know of 6. Our highest time pilot, has about 6000 hours in PCs.
The TEST PILOTS for Pilatus fly torque charts, the SALESMEN do not.
Shawn, can you explain that clearly. I use the torque charts when in cruise, meaning..... when torque limited, fly the torque settings when temp limited, keep below 780 ITT
_________________ ---Rusty Shoe Keeper---
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 12:27 |
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Joined: 01/16/11 Posts: 11068 Post Likes: +7098 Location: Somewhere Over the Rainbow
Aircraft: PC12NG, G3Tat
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Quote: If your engine cant stay below 780 in cruise when flying on the torque charts, adjustments need to be made, something isn't right. Ours runs around 760-765 when set on the torque charts. Ok, no chance my engine is correcto then. When it's hot, I'm always temp limited, meaning my torque settings are below the charts if I am to be keeping the ITT below 780. I thought (maybe incorrectly) that is why you monitored either or. You are either torque limited (normally when cold) or temp limited (normally when hot)....... Coming out of Telluride the power setting would be way over 780 ITT with the torque at book settings, I mean WAY over.
_________________ ---Rusty Shoe Keeper---
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 13:57 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13086 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: [ LOL well we have 6 pilots flying 4 PCs all flying torque charts, technically you know of 6. Our highest time pilot, has about 6000 hours in PCs.
The TEST PILOTS for Pilatus fly torque charts, the SALESMEN do not. The downside to cruising the way I do?
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 14:09 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13086 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: My understanding at least in the Meridian that also flies Torque is that Pratt pretty much guarantees being able to make book performance to TBO. Meaning that if you follow the torques charts for a given OAT you will have book power available up to TBO. Fly by ITT's and the engine won't make book in its later years, meaning that your performance tables no longer apply. Additionally HSI's and TBO costs will probably be higher. 780C vs 760C 780C is still so far below redline on the Pilatus. I guess if my performance falls off in 10 years I'll be flying at the speed all the guys flying the torque charts are flying every day.
Last edited on 26 Jul 2016, 14:10, edited 1 time in total.
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 14:09 |
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Joined: 01/16/11 Posts: 11068 Post Likes: +7098 Location: Somewhere Over the Rainbow
Aircraft: PC12NG, G3Tat
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Username Protected wrote: [ LOL well we have 6 pilots flying 4 PCs all flying torque charts, technically you know of 6. Our highest time pilot, has about 6000 hours in PCs.
The TEST PILOTS for Pilatus fly torque charts, the SALESMEN do not. The downside to cruising the way I do?
Got a great explanation from Shawn, we'll discuss at Osh......based on my convo with Shane, I agree with him.
Run the numbers by torque and then ensure that NG/ITT is within the acceptable ranges.
We'll get some feedback from Pilatus and P&W on it.
Charles posted echoed what Shawn says.
_________________ ---Rusty Shoe Keeper---
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Post subject: Re: CESSNA DENALI SINGLE ENGINE TURBOPROP Posted: 26 Jul 2016, 14:11 |
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Joined: 01/16/11 Posts: 11068 Post Likes: +7098 Location: Somewhere Over the Rainbow
Aircraft: PC12NG, G3Tat
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Username Protected wrote: My understanding at least in the Meridian that also flies Torque is that Pratt pretty much guarantees being able to make book performance to TBO. Meaning that if you follow the torques charts for a given OAT you will have book power available up to TBO. Fly by ITT's and the engine won't make book in its later years, meaning that your performance tables no longer apply. Additionally HSI's and TBO costs will probably be higher. 780C vs 760C 780C is still so far below redline on the Pilatus. I guess if my performance falls off in 10 years I'll be flying at the speed all the guys flying the torque charts are flying every day.
If I run torque settings when temp limited (below 780) then my temp goes past 780......
_________________ ---Rusty Shoe Keeper---
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