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JonesNL wrote:Interview from AviationWeek with A220 program leaders:
https://aviationweek.com/special-topics ... w-versions
Lots of known stuff about desire to increase current (non-linear due to supply chain) monthly rate of 6 to 10 by 2025 and required investments and added value of pre-FAL.
But there is some interesting comments of new versions:
- The A220-300 is currently certified for up to 150 seats, but Airbus is working on raising capacity to 160 passengers.
- New A220-500 would have more then 180 seats (not clear if comment of Airbus or writer).
- Airbus acknowledging that A32x is becoming A321 and thus implying cannibalization is not a problem when A225 competes against the A320.
- A225 launch probably not sooner then 2025.
- A220LR with 4000nm might cannibalize sales of A321XLR (also not clear if comment of Airbus or writer).
Recommended read...
GalaxyFlyer wrote:A friend who flies at JB says their dispatch reliability is horrible and they’re not getting expected range. No data, but interesting anecdotal evidence.
JonesNL wrote:- Airbus acknowledging that A32x is becoming A321 and thus implying cannibalization is not a problem when A225 competes against the A320.
ScottB wrote:JonesNL wrote:- Airbus acknowledging that A32x is becoming A321 and thus implying cannibalization is not a problem when A225 competes against the A320.
Eh, this really should be a matter of whether Airbus can achieve higher margins by expanding A32X production to sell A320neos or expanding A220 production to sell -500s.
wrongwayup wrote:In a world where production rates are constrained, Airbus is better pointing airlines to larger family members to get better pricing per unit. An A220-500 that cannibalizes an A320neo sale also frees up a production slot for a higher-priced/higher-margin A321neo. And considering the A220 lines do not appear to have the same level of constraints as the neo lines, Airbus isn't sacrificing much at all in terms of overall units with this strategy. Not rocket science from that point of view - the question becomes what engine to use, and is it worth the likely 10-figure develoment cost for the new variant?
JonesNL wrote:I am not sure they are going to do a neo with new engines. But I can imagine them doing a updated version with other suppliers to get the costs per unit down…
FLALEFTY wrote:Thanks for posting the article.
Neeleman is flinging route ideas at the "wall" hoping a few will stick. He may be pressing for a longer-ranged A223, but I bet he is the only customer looking for a 4,000 nm range variant. Once sticking aux tanks into the cargo hold and filling them up with Jet A, the much higher MTOW should make the A223LR a weaker performer than the stock A223. Also, there may be a need to strengthen the landing gear and surrounding structure. Then there is the extra weight of the ETOPs gear, catering, a bigger galley, perhaps the need for another lav, and figuring out how to do a crew rest in such a small plane. In a 2-class layout, premium-heavy, the pax load probably will max out at 120~123, but I can't imagine that a A223LR variant will be able to consistently carry a profitable load.
JonesNL wrote:- A225 launch probably not sooner then 2025.
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yyztpa2 wrote:GalaxyFlyer wrote:A friend who flies at JB says their dispatch reliability is horrible and they’re not getting expected range. No data, but interesting anecdotal evidence.
...but then they order 30 more over their orginal order. More than anecdotal.
http://mediaroom.jetblue.com/investor-r ... -150021707
JoseSalazar wrote:yyztpa2 wrote:GalaxyFlyer wrote:A friend who flies at JB says their dispatch reliability is horrible and they’re not getting expected range. No data, but interesting anecdotal evidence.
...but then they order 30 more over their orginal order. More than anecdotal.
http://mediaroom.jetblue.com/investor-r ... -150021707
Additional order or not, I can assure you jetblue is having issues with quality control, reliability, and to a degree, performance (they still don’t have the 2.3T MTOW increase that Airbus came out with, which is needed with that plane in B6’s config to really get the needed performance). The program started out ok initially, with standard growing pains and teething issues, but has since faced a lot of issues, and is still causing a lot of headaches. The fuel burn is great though. And the NPS scores are high. Once they figure out the QC/reliability issues, it should be a good plane, at least from a pax and bean counter perspective.
Skywatcher wrote:JoseSalazar wrote:yyztpa2 wrote:
...but then they order 30 more over their orginal order. More than anecdotal.
http://mediaroom.jetblue.com/investor-r ... -150021707
Additional order or not, I can assure you jetblue is having issues with quality control, reliability, and to a degree, performance (they still don’t have the 2.3T MTOW increase that Airbus came out with, which is needed with that plane in B6’s config to really get the needed performance). The program started out ok initially, with standard growing pains and teething issues, but has since faced a lot of issues, and is still causing a lot of headaches. The fuel burn is great though. And the NPS scores are high. Once they figure out the QC/reliability issues, it should be a good plane, at least from a pax and bean counter perspective.
I wonder if these issues are Mobile AB specific or the whole project?
JoseSalazar wrote:yyztpa2 wrote:GalaxyFlyer wrote:A friend who flies at JB says their dispatch reliability is horrible and they’re not getting expected range. No data, but interesting anecdotal evidence.
...but then they order 30 more over their orginal order. More than anecdotal.
http://mediaroom.jetblue.com/investor-r ... -150021707
Additional order or not, I can assure you jetblue is having issues with quality control, reliability, and to a degree, performance (they still don’t have the 2.3T MTOW increase that Airbus came out with, which is needed with that plane in B6’s config to really get the needed performance). The program started out ok initially, with standard growing pains and teething issues, but has since faced a lot of issues, and is still causing a lot of headaches. The fuel burn is great though. And the NPS scores are high. Once they figure out the QC/reliability issues, it should be a good plane, at least from a pax and bean counter perspective.
wrongwayup wrote:JonesNL wrote:I am not sure they are going to do a neo with new engines. But I can imagine them doing a updated version with other suppliers to get the costs per unit down…
The question that gets talked about a lot is exactly how much range (and therefore MTOW) is required, and therefore will the PW1525G be enough or will they have to use a 1200 derivative given the higher weight.
There are two possible outcomes - a "simple stretch" (i.e. the Bombardier legacy approach) with the same engines and a bit of a range penalty vs the smaller versions, or the two engine subfamily (i.e. the Embraer Ejet legacy approach) with a higher range and payload for the larger variants.
If I'm a betting man I think it's the former they go for, a nominally 160 (up to 180) seat simple stretch with a maxed-out PW1500G and a range in the 3000nm bracket instead of the ~3400nm the current members have.
JonesNL wrote:wrongwayup wrote:JonesNL wrote:I am not sure they are going to do a neo with new engines. But I can imagine them doing a updated version with other suppliers to get the costs per unit down…
The question that gets talked about a lot is exactly how much range (and therefore MTOW) is required, and therefore will the PW1525G be enough or will they have to use a 1200 derivative given the higher weight.
There are two possible outcomes - a "simple stretch" (i.e. the Bombardier legacy approach) with the same engines and a bit of a range penalty vs the smaller versions, or the two engine subfamily (i.e. the Embraer Ejet legacy approach) with a higher range and payload for the larger variants.
If I'm a betting man I think it's the former they go for, a nominally 160 (up to 180) seat simple stretch with a maxed-out PW1500G and a range in the 3000nm bracket instead of the ~3400nm the current members have.
I also was thinking of an updated wing and engine optimized for slower mach number and shorter stage lengths to go with the A225…
JonesNL wrote:wrongwayup wrote:JonesNL wrote:I am not sure they are going to do a neo with new engines. But I can imagine them doing a updated version with other suppliers to get the costs per unit down…
The question that gets talked about a lot is exactly how much range (and therefore MTOW) is required, and therefore will the PW1525G be enough or will they have to use a 1200 derivative given the higher weight.
There are two possible outcomes - a "simple stretch" (i.e. the Bombardier legacy approach) with the same engines and a bit of a range penalty vs the smaller versions, or the two engine subfamily (i.e. the Embraer Ejet legacy approach) with a higher range and payload for the larger variants.
If I'm a betting man I think it's the former they go for, a nominally 160 (up to 180) seat simple stretch with a maxed-out PW1500G and a range in the 3000nm bracket instead of the ~3400nm the current members have.
I also was thinking of an updated wing and engine optimized for slower mach number and shorter stage lengths to go with the A225…
JonesNL wrote:ScottB wrote:JonesNL wrote:- Airbus acknowledging that A32x is becoming A321 and thus implying cannibalization is not a problem when A225 competes against the A320.
Eh, this really should be a matter of whether Airbus can achieve higher margins by expanding A32X production to sell A320neos or expanding A220 production to sell -500s.
Not completely, the A32x line is production constrained. So, every A225 they sell is revenue they would miss out on as deliveries are constrained. Of course this is under the assumption that the A32x line stays production constrained and that the A225 can contribute a positive margin…
N757ST wrote:JonesNL wrote:wrongwayup wrote:
The question that gets talked about a lot is exactly how much range (and therefore MTOW) is required, and therefore will the PW1525G be enough or will they have to use a 1200 derivative given the higher weight.
There are two possible outcomes - a "simple stretch" (i.e. the Bombardier legacy approach) with the same engines and a bit of a range penalty vs the smaller versions, or the two engine subfamily (i.e. the Embraer Ejet legacy approach) with a higher range and payload for the larger variants.
If I'm a betting man I think it's the former they go for, a nominally 160 (up to 180) seat simple stretch with a maxed-out PW1500G and a range in the 3000nm bracket instead of the ~3400nm the current members have.
I also was thinking of an updated wing and engine optimized for slower mach number and shorter stage lengths to go with the A225…
If you touch the wing add a couple billion to the program. Besides, some larger operators like B6 would likely want a 225 to stretch its legs on transcons and island flying.
JonesNL wrote:N757ST wrote:JonesNL wrote:
I also was thinking of an updated wing and engine optimized for slower mach number and shorter stage lengths to go with the A225…
If you touch the wing add a couple billion to the program. Besides, some larger operators like B6 would likely want a 225 to stretch its legs on transcons and island flying.
I agree, but it was commented by Airbus a couple of times that the wings are one of the biggest cost drivers for the plane. That’s why I only imagine it being tackled if Airbus can get the design and production in house to cut production costs considerably. The gained efficiency would be a bonus, not the main goal…
CRJ900 wrote:Bombardier published images of the CS700 and CS900 many years ago, they looked like simple fuselage stretches with existing wings and engines. Seat map showed 170 and 190 all-economy seats, IIRC. Wonder how much of that Airbus can use...
ikolkyo wrote:CRJ900 wrote:Bombardier published images of the CS700 and CS900 many years ago, they looked like simple fuselage stretches with existing wings and engines. Seat map showed 170 and 190 all-economy seats, IIRC. Wonder how much of that Airbus can use...
I feel like I remember those being fan made, I have a hard time seeing the aircraft being stretched to such a length.
Polot wrote:JonesNL wrote:N757ST wrote:
If you touch the wing add a couple billion to the program. Besides, some larger operators like B6 would likely want a 225 to stretch its legs on transcons and island flying.
I agree, but it was commented by Airbus a couple of times that the wings are one of the biggest cost drivers for the plane. That’s why I only imagine it being tackled if Airbus can get the design and production in house to cut production costs considerably. The gained efficiency would be a bonus, not the main goal…
That will take billions and eat any savings you might get from producing in house vs having Spirit AeroSystems produce it as currently done. If there are even any savings- I’m not sure why you think in house production would cost considerably less.
Airbus would only do that if there was a considerable efficiency gain, which is unlikely as the A220’s wing is very modern as is.
GalaxyFlyer wrote:A friend who flies at JB says their dispatch reliability is horrible and they’re not getting expected range. No data, but interesting anecdotal evidence.
In the meantime, the A220-500 could hand Airbus a 13% efficiency advantage over the Max 8 on a per-seat basis, according to Addison Schonland, an analyst at AirInsight Group. That’s a considerable saving at a time when fuel prices remain high and airlines are under pressure to slash emissions.
“Talking now is perfect,” Aboulafia says. “You want airlines to do their fleet-planning with the A220 in mind. It’s the Max 8 with shorter range and better economics, lighter, thinner and with a really great engine.”
https://www.air-journal.fr/2022-07-22-airbus-a220-douzieme-pour-air-france-et-version-500-5237457.html
Aucune date de lancement de l’A220-500 n’est cependant annoncée vu les problèmes industriels actuels ; « il ne s’agit pas de protéger l’A320neo » selon Christian Scherer, qui estimait en décembre que les clients tentés par les A220 ne seraient « de toute façon pas intéressés » par la famille supérieure, dont les délais de livraison sont en outre très longs en raison la demande.
Ziyulu wrote:Is this aircraft 2-3 seating? Is it longer than the 737?
FLALEFTY wrote:Optimizing an engine for the A220-500 will be a challenge. The current PW1500g tops out at 23K lbs. of thrust, it has a 73 inch fan diameter and weighs 4,800 lbs., which are important dimensions when it comes to the basic design of the A220 in general. The upgrade option would be the PW1100g engine used on the A320NEO, which has roughly 27K lbs. of thrust, but has an 81 inch fan diameter and weighs 6,300 lbs.. The A220 would require engine mounting mods, a taller landing gear and structural mods to accommodate the larger engines. The end result for the A225 would be a much heavier OEW & increased drag.
FLALEFTY wrote:Optimizing an engine for the A220-500 will be a challenge. The current PW1500g tops out at 23K lbs. of thrust, it has a 73 inch fan diameter and weighs 4,800 lbs., which are important dimensions when it comes to the basic design of the A220 in general. The upgrade option would be the PW1100g engine used on the A320NEO, which has roughly 27K lbs. of thrust, but has an 81 inch fan diameter and weighs 6,300 lbs.. The A220 would require engine mounting mods, a taller landing gear and structural mods to accommodate the larger engines. The end result for the A225 would be a much heavier OEW & increased drag.
JonesNL wrote:The A220 misses scale to to make the 500 version viable. The backlog at current rate is 14 years plus (750/53). They are probably losing sales due to this fact. Airbus needs to solve this first before thinking about a A220-500.
When launched it will probably garner 500 orders at launch without any troubles. This means a rate of 200 per year is needed at minimum to make the backlog an acceptable 6-7 years...
They seem to really struggling with this as both A32x and A22x line have been stagnant since 2019...
MIflyer12 wrote:Also in 2025, the aircraft program is expected to reach an operating profit for the first time. Once that milestone is in sight, Airbus will look at the next potential steps—longer ranges and a stretched version that would essentially match the size of a 737-8 or A320neo.
That's a 'look at it' in 2025, not have the engineering done, not have Board approval to offer, certainly not begin commercial production.
LAX772LR wrote:MIflyer12 wrote:Also in 2025, the aircraft program is expected to reach an operating profit for the first time. Once that milestone is in sight, Airbus will look at the next potential steps—longer ranges and a stretched version that would essentially match the size of a 737-8 or A320neo.
That's a 'look at it' in 2025, not have the engineering done, not have Board approval to offer, certainly not begin commercial production.
In your desire to analyze carefully, you've ironically missed the massive wiggle-room that such a statement grants.
It does NOT say "look at it in 2025," it says "once that milestone is in sight"......
Well, what does "in sight" mean?
ANSWER: whatever they want it to.
That could signify any point from the day that this was written, onward.
All they have to do, is see the program trending toward profitability, and the "in sight" threshold is thereby met.
Thus, for all we know, they could indeed be working on the engineering/approval/etc requirements, with an eye on starting in 2025. Or any other time: the article postulates 3-4yrs thereafter, but that's in no way official. We'll just have to wait and see what prompts them to pull the trigger, to know when.
MIflyer12 wrote:You can parse my writing any way you want,
MIflyer12 wrote:but you may not be familiar with the French method of executive/investor relations methods of communications: Use lots of words to commit to absolutely nothing. This is no stronger than a politician saying 'We will look at XXX at the appropriate time.'