Quoting EPA001 (Reply 56): But since the big twins are closing in on efficiency (though there is a lot more to civil aviation then efficiency alone) it might be something worth to think about. Airbus initially wanted a wing with a span of about 84 meters. Now new technologies have been developed, and maybe that wing span is not necessary anymore, but if Airbus will consider a major overhaul for the next generation A380's, it might be worth their while to investigate this option. Along with other improved aerodynamics, new engines and weight optimisations.
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Certainly. And another thing I keep thinking about...
The 380F...
Given a choice on where to deploy engineering resources, could airbus look into removing the need for the main deck/upper deck floor? As of now, it is structurally integral to the frame, and this does take a lot away from it capability wise, as it renders the airframe pretty much only useful as a parcel or can carrier. But if that floor were no longer necessary, you
would have something at least equal to the 748f capability wise WRT outsized cargo.
I'm not going to address what I think the market might be for this, since I have truly no idea. But the 380 as an outsized cargo carrier would work in terms of sheer lift for distance. As well, it can overcome the disadvantage of not having Nose Loading simply by adding an Aft Ramp, a la 124, C5, and a few others. I understand that wouldn't be the easiest undertaking, but if there were eventually a market for at least 75 - 100 such beasts world wide, I can see that that would indeed be worth the engineering effort to get after.
Now we just need to Keesje to come out of retirement and make us some drawings,

Quoting art (Reply 60): Simply (and I mean crudely and basically) it gives a ball park capability for aircraft in terms of cost. Was A340 not eclipsed by 777 because 777 cost was lower for similar capability? Similarly was 744 not eclipsed by A340 on a cost basis?
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Not really, no. The 744 was only ever really supplemented, not replaced by any 340 series. Especially where the -600 is concerned, most operators that purchased or leased the 346 held onto their 744s; indeed one carrier still operates the later and not the former (though that will not last forever based on their going away from quads in general).
As for the 777, we'd have to be more clear
which 777 vs which 340 are we talking about. A 77A is much more efficient, but nowhere near as capable as a 346, while the same can be said of a 343 vs a 77W.
But generally, the reason we see more 777s than 340s today does have as much to do with capability as with cost. And in the case of things like climbout performance (which is a contributor to operational cost and a big part of the reason why 4-eng aircraft really can't hope to compete on cost for segments in the mid-short haul range), there are advantages to twins that quads would have to bring a lot of capability to the table to stay relevant.
There are still things that a 346 can do that a 77W can't, like a MTOW take off from
JNB let's say, that keep the type very useful to some operators. IIRC, even the 744 had trouble with that one, which was why SAA went with 346s over their 744s.
Quoting cmf (Reply 64): However, engines are only one part of maintenance. |
The most
expensive part. To the point that unless there is a very compelling reason, two are always better than four.
Quoting cmf (Reply 64): Let's count high and say it is half. |
Honestly, I'd say that's more likely low than high, even for a twin. In addition to much higher per-unit/kg costs for most components, you also have much more frequent inspections, and shorter on-wing times than just about any airframe component there is.
Quoting cmf (Reply 64):
How is this a clinching argument? It is a small segment. You should not expect a constant flow of orders. |
Not a constant flow, like 50- 100 per year, no. But a few more years like the last few, especially where the 748i is concerned, and we can see that it really is an issue of where the future is headed and less of quad VLAs being a "niche" product.
Quoting cmf (Reply 64): With a few years backlog I don't see how it is time to call the undertaker.
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Indeed so. While the future may not be rosy, they aren't dead yet.
Quoting EPA001 (Reply 70): Like for example an A80-900 and/or an A380-1000, the famous SUH version. .
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Really, if they're serious about that road (and for the record I do have doubts about that one), they really should just skip right ahead to the 1000. At least with that, the economics of scale really do start to help out. Given that the subtype development cost would be the same, I see Airbus doing better with that, but that's my opinion.
Quoting art (Reply 75): I suppose he would need Doric to order to get close to that number. |
Wouldn't hurt, but my read was that Leahy is not factoring this and has 25 other orders.
Quoting Scipio (Reply 85):
Everything else equal, a modern 4-engined plane will have nothing like a 30% cost disadvantage versus an equally modern 2-engined plane. |
Why not? It isn't just the fuel penalty. There are a lot of factors that work against, not for, quads.
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