The 737 was designed using light tables and slide rules, to use low-bypass turbofans and direct controls with avionics only on board to optionally aid the pilots.
The A320 was designed in CAD and using CFD, with full digital fly-by-wire, and designed from the start for high-bypass turbofans.
Both designs have been updated plenty since, but because the basic design is much more modern, the A320 is much more amenable to being updated. There are elements of the 737 design that still exist on every new MAX coming off the line that would completely doom the certification chances of any new design, but are still there because they got grandfathered in for 737.
The wonder is not that the A320 finally caught up in sales, it's that the 737 can still be legally sold.
What’s wrong with the 737 design that it wouldn’t pass today as a new aircraft? (Ignoring the disaster that was the MAX.)
So you have to constantly apply some controls to fly, done by software.
I love stupid car comparisons so imagine a car with a new engine that is more economical to run, but very heavy on the left so the car constantly want to turn left. But if you apply force to the steering wheel manually or the car does it for you with software, all good. Still a shit car though.
I think they added redundant sensors which should theoretically prevent this in future. IMHO, I think several issues compound here. They should have redesigned the fuselage. The engineering compromise is bad, but if handled with care, could have been done relatively safely. They opted for no additional pilot training re MCAS. This was a fatal mistake, compounded by them relying on a single sensor. Nothing in avionics relies on a single sensor for remaining in the air. That was insane. There MUST have been engineers screaming about safety who were ignored.
How anyone thought making critical decisions on a single sensor reading made sense is beyond me.
I remember when I first heard about the MCAS issue and thought "Why didn't the pilots just pull up?" and someone explained to me that MCAS worked by trimming, and it would trim nose-down so hard that even with full elevation to try to nose back up, it wasn't enough to overcome the extreme amount of nose-down from the trim.
And since pilots weren't trained on the new MCAS system, they weren't aware that the trim would have been automatically moved.
Not only that, but Boeing is actually limited in how much they can "modernize" the 737, because doing too much might exceed the limits of the 737's type certificate. This is the reason behind the current engine inlet overheating worries, which has led to an airworthiness directive for the 737 MAX (https://aerospacenews.com/faa-airworthiness-directive_boeing...) and is also one of the reasons for the delay certifying the MAX 7 and MAX 10. This would be a complete non-issue for other planes, because all modern designs have a switch position that only turns on the engine anti-ice system when it's needed, but the 737 MAX can't have that because the 1967 737 didn't.
I know that it's a complete nightmare to certify anything. However I apparently don't understand some underlying principle that allows to certify some things and not the others.
MCAS was implemented to make sure the control forces increase going into a stall, this is a requirement in the regulations. Without MCAS the control forces would drop on the way into a stall, which is an issue that would prevent certification of the aircraft.
(Was on a transatlantic one once. Never again.)
“By 1988, when Airbus launched its new A320 narrowbody jet, Boeing had already established a strong lead, having delivered around 1,500 of its popular jets”
So, Boeing sold about 1,500 767s in the first 20 years and over 10,500 in the < 40 years since. Airbus sold about 12,000 in the < 40 years since.
So, to catch up, Airbus produced about 15% more than Boeing did.
Well they did bet on the Dreamliner, fell on their nose and still recovered.