04 Feb 2026, 11:19 [ UTC - 5; DST ]
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 14:42 |
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Joined: 11/19/15 Posts: 1837 Post Likes: +1734 Company: Centurion LV and Eleusis Location: Draper UT KPVU-KVNY
Aircraft: N45AF 501sp Eagle II
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Username Protected wrote: All things being equal I think flying higher, faster, above weather, and safer is worth an extra cost. It's not as much more as people think.
Well, that's the problem - All things aren't equal! For example, in your case you have significantly more capital tied up in your plane than I do. I like the Citations a lot, but the "it just costs a little more" logic gets us into a Gulfstream pretty quickly... Robert
Robert,
I also have much lower fuel burn than other 501's and engines on program. So yes I have more into my plane than your KA. Although I have no idea what your plane cost or is worth.
I know it's not all equal. Thats why I said if all things are equal. If you take out the other variables the extra cost isn't as much as people think and in my opinion well worth it.
I know from personal experience that I often need to climb't have to wear my o2 mask in case of emergency. I often have to put my mask on to get over weather and glad I have that choice. So the higher flying plane wins the weather war often.
Mike
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 15:43 |
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Joined: 11/30/12 Posts: 4952 Post Likes: +5635 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: The turboprop will never see the 100 knot headwind, because it can fly at a lower altitude and lower headwind without having to be an OPEC member. This is wrong. I've flown both and know this.
The benefit of flying low is not more range, but faster speeds.
When you are getting a 100 knot headwind in the mid 20s, then you have equal range roughly at any lower altitude but faster speed.
Strictly in terms of range, it takes about a 100 knot headwind to make going lower worthwhile. But at about 50 knots headwind, I will start to consider flying at, say, FL210/220 and going in fast mode rather than economy mode. My range is still reduced, but the penalty for going faster is reduced. Sometimes there is a big difference in the wind direction or speed between FL210 and FL270, so that factors into the computation.
So my rough guideline is 0 to 50 knots, fly high, 50 to 100 decreasing penalty to fly lower...greater than 100 knots, fly lower.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 16:09 |
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Joined: 08/16/15 Posts: 3843 Post Likes: +5719 Location: Ogden UT
Aircraft: Piper M600
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I think the weather benefits of flying a jet are extremely overblown. In the last 2000 hours, I can only recall stopping once for Weather, and that was an intense squall line from hell that went all the way from Canada to Mexico, and even the airliners were diverting and stopping short. That was a wall up into the 40s. Yeah I spent the night in St. Louis, had dinner with the family and watched some incredible fireworks with my plane safely in the hanger. Even many times when the jet guys think that the weather below is terrible and they’re on top top, we turbo props are flying in between layers in smooth air. This was last week going into Denver at 29,000 feet. There were puffies going up 27/28,000 feet, which was the only reason I was at 29. Tops were in the high 30’s. But I was in clear, smooth air with reported, moderate mountain wave and moderate front range turbulence. Sunday there were Sigmets, not Airmets for severe turbulence, 18 to 41 and surface to 18,000. But I found smooth air at 26. There was impressive bellyaching from the jet crowd, the whole way from Denver to Santa Anna. For me, it doesn’t matter how high the head winds are. My fuel burn is so low, that the extra fuel burned is a rounding error. Attachment: IMG_0595.jpeg
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_________________ Chuck Ivester Piper M600 Ogden UT
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 16:56 |
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Joined: 05/03/14 Posts: 49 Post Likes: +55
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Username Protected wrote: I think the weather benefits of flying a jet are extremely overblown. Getting my popcorn out...hilarious statement.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 17:07 |
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Joined: 05/08/13 Posts: 588 Post Likes: +368 Company: Citation Jet Exchange Location: St. Louis
Aircraft: 58P C510 C525 Excel
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Username Protected wrote: I think the weather benefits of flying a jet are extremely overblown. Getting my popcorn out...hilarious statement.
I'll be eating my popcorn at FL450 looking down on you in the 20's on a sultry summer day with popcorn storms taking up 2/3 of the country.
Or just any big system. I still had to parallel the north edge of a really big system this June for a few hundred miles even at FL450. If I were in a turboprop I'd have called it a night, or gone 100s of miles further.
_________________ The Citation Jet Exchange www.CitationJetX.com CJs, Mustangs, Excels
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 17:41 |
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Joined: 11/30/12 Posts: 4952 Post Likes: +5635 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: I would agree the fuel burn on a legacy citation is more than a KA. Generally true, though perhaps not always for any given flight. My example flight above in strong headwinds used 438 gallons. I bet a King Air 200 would use as much if not more, and it would be a much worse experience being in the precip and turbulence than on top in the sunshine and mostly smooth air. You fly more in headwinds than you do in tailwinds. What that means is the faster airplane is better at fuel usage than it appears because it cuts through the wind much better. My MU2: 290 KTAS at 70 GPH at FL280: 4.14 nm/gal My C560V: 400 KTAS at 165 GPH at FL400: 2.43 nm/gal A KA200 (estimate): 265 KTAS at 100 GPH at FL280: 2.65 nm/gal It is pretty close, it won't take that much headwind to for the jet to be about the same. Mike C.
You can make any plane look bad if you use estimates.
The following numbers are averaged from all my recorded flights at a given flight level in the B200, using older stock engines.
FL180, ISA+7, 286 kts @115 gph. 2.49 nm/gal
FL220, ISA +9, 282 kts @ 100 gph. 2.81 nm/gal
FL240, ISA +7, 280 kts @ 95 gph. 2.93 nm/gal
FL280, ISA +7, 277 kts @ 83 gph. 3.33 nm/gal.
FL310, ISA +7, 273 kts @ 75 gph. 3.64 nm/gal
FL330 ISA +7, 266 kts @ 67 gal/hr. 3.97 nm/gal
The B200 uses more fuel than an MU-2, but it uses much less than a jet.
Last edited on 27 Nov 2023, 17:53, edited 1 time in total.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 17:51 |
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Joined: 05/03/14 Posts: 49 Post Likes: +55
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Username Protected wrote: As above, I’m still trying to figure out how this Jets gonna get me places more reliably from a Weather standpoint than a turboprop. For every trip that I could’ve made in a jet, I bet I’ve made five that I couldn’t do in a jet due to constraints. Whether short field constraints, high and hot contraints, ormsnow and ice contaminated runway constraints. I stopped short on one flight in over 2000 hours of flight time that I can recall. And I have never been in a situation that made me uncomfortable if it’s dangerous I’m not doing it. On a convective day, we all have to deal with convection in and out of the terminal the same exact way. So we’re basically just talking about enroute weather. There is not much weather of concern in the upper 20s. You’re mainly just talking about convection, and with minor changes in timing, and routing there is almost always a way around that. I disagree and feel that just about every part of what you said is false or incorrect. Im sure others will chime in, but I went from Meridian, to Mustang, to Ultra...the jets can do all of the missions the turboprop did and many the turboprop could not. The weather considerations are vastly easier to deal with in many, many ways and the comfort level, weather concerns or not is far superior. Why do people need to try to make the case that what they have is "THE BEST". If I could afford a Gulfstream thats what I'd be flying. I can't, but I fly the best airplane that reasonably fits my budget and mission. Im not going to spend hrs of time typing pages of rationale trying to say that my Ultra is better or more capable than a Gulfstream...give me a break. Who are you kidding?
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 18:53 |
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Joined: 12/03/14 Posts: 21247 Post Likes: +26774 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Strictly in terms of range, it takes about a 100 knot headwind to make going lower worthwhile. But at about 50 knots headwind, I will start to consider flying at, say, FL210/220 and going in fast mode rather than economy mode. My range is still reduced, but the penalty for going faster is reduced. Sometimes there is a big difference in the wind direction or speed between FL210 and FL270, so that factors into the computation.
So my rough guideline is 0 to 50 knots, fly high, 50 to 100 decreasing penalty to fly lower...greater than 100 knots, fly lower. Perfect analysis for my strategy with the MU2. When the winds picked up to about 50 knots, then you could fly lower with less penalty. At 100 knots, there wasn't any penalty. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 19:04 |
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Joined: 12/03/14 Posts: 21247 Post Likes: +26774 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: I think the weather benefits of flying a jet are extremely overblown. I used to believe that. No more. Icing, IMC, enroute weather are mostly non existent at FL400+. Yesterday was a good example. A turboprop would be solid IMC, in precip, in turbulence, for a solid 1.5 hours. I was in sunshine, no precip, and mostly smooth. When you get into the low 40s, you can often find gaps in lines of storms. The air can't be lifting everywhere, so the tops of storms tend to separate at that altitude. And you can see them generally, not like being embedded in the 20s and relying on you weather systems. Even in the terminal area, the ability to climb crazy fast gets you out of stuff quickly. Lastly, a 100 nm diversion in a jet is very tolerable if you have to do it. Speed gives more options, including a larger radius for alternates, too. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 19:12 |
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Joined: 12/03/14 Posts: 21247 Post Likes: +26774 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Or... P180 makes the trip at FL400 in 2+29 on 1375lbs fuel... at least right now. You win on fuel, no doubt. I suspect if you had flown it "for real", your time would have been ~2:40 and fuel ~1500 lbs since we were not direct and not given unabated climb. Also, can it do it with 1200 lbs on board? That was my cabin load, 6 people and baggage. I suspect it can since the trip wasn't particularly long range. Quote: Some turboprops aren't so bad. ;) Piaggio is unique and impressive. I wonder if other costs, like inspections, will erode some of the advantages. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 27 Nov 2023, 19:15 |
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Joined: 11/30/12 Posts: 4952 Post Likes: +5635 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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I don't own a jet. I've never flown a jet. I haven't even flown a jet on MSFS. I sat in one with Chip recently - that's about as close as I've been. I've topped several lines of weather in the B200 and have been able to go VMC between the buildups in many more. And yet I am solidly in the "If there's weather to deal with, I want a jet" category. It's just common sense. 
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