07 May 2025, 07:34 [ UTC - 5; DST ]
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 13 Feb 2013, 10:55 |
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Joined: 12/10/07 Posts: 8108 Post Likes: +7828 Location: New York, NY
Aircraft: Debonair C33A
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Username Protected wrote: Gerry,
Why do you think bigger is more stable?
Tim Yeah, I don't undertand that one either. I've been bounced around in the back of a 747 like you wouldn't believe. AFIK, stability in turbulence has more to do with wing loading - i.e. the higher is the wing load, the more stable the plane will be. I suspect that Eclipse is more heavily wing loaded than TBM. Oh, and TBM is single engine. It's a consideration for a lot of people. Not to mention noise and vibration associated with the prop.
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 13 Feb 2013, 12:27 |
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Joined: 12/16/07 Posts: 18411 Post Likes: +28177 Company: Real Estate development Location: Addison -North Dallas(ADS), Texas
Aircraft: In between
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I've flow the Eclipse and looked into it quite extensively. Very happy Ted is enjoying it and I did have fun flying it.
When it came down to spending the kind of money a fully capable Eclipse would cost, I went to the KA. Several reasons as I've discussed. For the amount of money I could get a well equipped older KA for, I got an SUV with all weather capability which fit my requirements better. Last weekend I departed from the Denver area in a snow storm with reported icing in the climb. Same when I arrived in the Dallas area, no snow, but possible icing conditions in the descent down to an ILS approach. So, I want, need and use all weather capability. I want and need known ice (so a VFR Eclipse isn't in the cards for me). I need more room. The potty and other conveniences really can add to the comfort on a trip; especially, if one has little ones. KA is more stable.
I do agree, the Eclipse is very much like a baron with jet engines. Same general size exterior, one less seat, but no sizable nose compartment. There certainly is a place for it, and as y'all know, we each need at least three planes (g). For that 800 mile trip with a couple or two that isn't large and little baggage, it would fit and be fun.
I simply need more room and to be able to carry a larger load. I want all weather and use that. Always interesting to discuss. Eclipse is more like a jet sports car; I need an SUV.
I don't have any problem climbing to assigned altitude in Texas either and going direct. Sometimes Fort Worth approach steps me up or down a bit, but usually it's very good. In the NE and parts of the West Coast, it's very different.
I'm glad Ted's happy. Certainly is a place for that plane. Hope they can get everything straightened out. As with all planes, one has to adjust for their mission.
Best,
Dave
_________________ Dave Siciliano, ATP
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 13 Feb 2013, 14:15 |
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Joined: 12/29/10 Posts: 2736 Post Likes: +2574 Location: Dallas, TX (KADS & KJWY)
Aircraft: T28B,7GCBC,E90
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Username Protected wrote: I simply need more room and to be able to carry a larger load. I want all weather and use that. Always interesting to discuss. Eclipse is more like a jet sports car; I need an SUV. Same reason I have the 421, yet lust after a PC-12! Robert
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 14 Feb 2013, 21:06 |
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Joined: 12/17/10 Posts: 1626 Post Likes: +276 Location: Valparaiso, IN
Aircraft: Lancair Evolution
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Username Protected wrote: Chris, Yuri,
That was why I asked the question. I always thought stability in turbulance was primarly two factors. Wing loading and sheer mass; sail effect e.g. the surface area of the plane was a secondary factor. The larger the surface area larger amount of instability (usually this is offset by sheer mass). The more mass the more wind required also the higher the wing loading the stonger the wind must be locally to force the aircraft to move.
Tim There is a massive difference in stability between my V-tail and my B36TC. The biggest difference is the sheer size advantage the B36 has. Are you saying that the only real advantage is more wing loading? I thought someone tried to say before that the 36 bonanzas and 35 bonanzas have the same wing loading because they use the same wing. Then why is my 36 so much more stable???? I flew them both today and it was very turbulent down low. I was getting slammed in my 35 but in my 36 it wasn't too bad.
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 14 Feb 2013, 23:32 |
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Joined: 11/06/10 Posts: 12129 Post Likes: +3030 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: Chris, Yuri,
That was why I asked the question. I always thought stability in turbulance was primarly two factors. Wing loading and sheer mass; sail effect e.g. the surface area of the plane was a secondary factor. The larger the surface area larger amount of instability (usually this is offset by sheer mass). The more mass the more wind required also the higher the wing loading the stonger the wind must be locally to force the aircraft to move.
Tim There is a massive difference in stability between my V-tail and my B36TC. The biggest difference is the sheer size advantage the B36 has. Are you saying that the only real advantage is more wing loading? I thought someone tried to say before that the 36 bonanzas and 35 bonanzas have the same wing loading because they use the same wing. Then why is my 36 so much more stable???? I flew them both today and it was very turbulent down low. I was getting slammed in my 35 but in my 36 it wasn't too bad.
Gerry,
A quick Google search revelaed the wing area of the V-Tail is 178 square feet. The B36TC (assuming I read the article correctly) has a wing area of 181 square feet. Yet the gross weight between the plane is not the same. In the V-Tail you have about 2500 lbs which gives you a wing loading of around 14lbs per square foot. The B36TC would end up around 21lbs per square foot (asusmes 3800lbs MTOW).
Therefore the B36TC has a wing loading which is 50% greater. I would expect it to be much more stable. A Cirrus is even more stable; wing loading is just over 25lbs per square foot. My Aerostar has a wing loading of 38.5 (6852lbs MTOW / 178.5 square feet). A PC-12 is 37.5lbs per square foot (10450 MTOW / 278 square feet).
I think you get the idea. The more mass you have per square foot the harder it is to move and the better the plane rides turbulance.
Tim
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Post subject: Re: Eclipse jet to be built in Poland, $2.6-2.8 million Posted: 15 Feb 2013, 16:19 |
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Joined: 07/11/11 Posts: 1671 Post Likes: +465 Location: Redwood City, CA (KPAO)
Aircraft: 1967 Bonanza V35
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Username Protected wrote: I finally realized that most people who speak negatively of the aircraft have never flown one, never ridden in one, never even sat in one, probably never even seen one in person!
Ted, Great post... solid mythbusting. shoe
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