A380 Production Sadness

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Airbus slashes A380 superjumbo production

The worst bits are -

The A380 build rate will be reduced to eight jets a year in 2019, down from 15 this year and 28 in 2016, Airbus said Wednesday.

The A380 was already due to see production cut to one aircraft a month from next May, and the reductions mean that it is no longer breaking even on a per-plane basis. The company has long since given up on recouping the program’s €25 billion in development costs.


Even if you don't like the aircraft, this isn't good news for anyone.

Airline economics is such a fickle thing. Ask Mr Joyce who has more risk in world health presently than under his own control.......
 
I’m presuming Sprucegoose is talking about these guys?
I personally think it’s pie in the sky stuff

I guess they’re also going to be carrying Elvis. Won’t ever happen. Almost the worst possible aircraft choice for the supposed operation. And high density. Seriously? It sounds like the sort of thing you’d see on prune during school holidays.
 
Interesting article I just read...

 
Yes, that was said some time ago how they wanted to build an neo version of it which they felt would be a big step in viability. However, it required enough customer commitment rather than spending even more pre-commercial return. And that didn't happen so the whole thing fell down.
 
Interesting article I just read...


Blaming the engines. Love it. They had their issues, but if the aircraft had been brought into service when they promised, then the sudden advent of better engines would still have been some years away.

The biggest issue with the A380 was purely the fault of Airbus. The aircraft was far too heavy. Whilst they actually managed to extract very good performance from it, given the weight, they would have done hugely better if it hadn’t been obese to start with. The empty weight was almost 100 tonnes greater than that of the 747, but it was only realistically carrying another 100 passengers.

Looking at empty weights, the 747 weighted about .5 tonnes per passenger, but the 380 was actually heavier at .57 tonnes per passenger. So, you immediately have a penalty of about 15%. From that point, much of the cunning engineering that happened was simply trying to get that deficit back.

An A380 with an empty weight of about 245 tonnes would have been very impressive, and would almost certainly still be with us.
 
Which afaik was at least partially down to the oversized wing which was reportedly designed for a 380-900 sized aircraft, which Leahy also mentions.

But engines were definitely an issue.
As it is you've had 250 aircraft produced - so 1000 odd engines split between two manufacturers. I doubt either made much money on the program (particularly with the issues both had).

I wonder with hindsight whether the aircraft could have been designed around existing engines - say four A330 engines to reduce this cost of development, with perhaps a simpler path to shifting to a neo engine.
 
Which afaik was at least partially down to the oversized wing which was reportedly designed for a 380-900 sized aircraft, which Leahy also mentions.

As in all things aviation, if you change on thing, you end up changing many. There have always been claims that the wing was designed for the mythical -900, but I’ve never seen anything official that says that. It really makes very little sense, to compromise your design, for something that might happen in the future.

The aircraft’s performance was as good as it was, in large part because of the wing. It would never have been able to operate from the shortish runways that it could, had the wing been smaller. The large wing was also a factor in its ability to get up high, early in flights, which helped with fuel burn. Approach and take off speeds were relatively low, again because of that big wing. Make them higher, and you need more powerful engines, longer runways, and so on.
But engines were definitely an issue.

Engine reliability was an issue. Changes were happening far too often, though failures were rare.
I wonder with hindsight whether the aircraft could have been designed around existing engines - say four A330 engines to reduce this cost of development, with perhaps a simpler path to shifting to a neo engine.

That would give you an A340. Underpowered. Terrible performance. Probably unable to fly across the Pacific (west bound). It would have had approximately the performance of a 380 operating on three of the current engines...not nice. The aircraft would have been stillborn.
 
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As in all things aviation, if you change on thing, you end up changing many. There have always been claims that the wing was designed for the mythical -900, but I’ve never seen anything official that says that. It really makes very little sense, to compromise your design, for something that might happen in the future.

The aircraft’s performance was as good as it was, in large part because of the wing. It would never have been able to operate from the shortish runways that it could, had the wing been smaller. The large wing was also a factor in its ability to get up high, early in flights, which helped with fuel burn. Approach and take off speeds were relatively low, again because of that big wing. Make them higher, and you need more powerful engines, longer runways, and so on.


Engine reliability was an issue. Changes were happening far too often, though failures were rare.


That would give you an A340. Underpowered. Terrible performance. Probably unable to fly across the Pacific (west bound). It would have had approximately the performance of a 380 operating on three of the current engines...not nice. The aircraft would have been stillborn.
Were the A330 and A340 engines the same?
 
Were the A330 and A340 engines the same?
No. Whilst there were later models of the A340, did have engines in 50-60,000 lb class, they were initially introduced with engines of around half the size of the A330. In large part it was an attempt to circumvent the ETOPS rules as they existed at the time.
 
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