Fuel capacity of the C919 is 24,917 L while A320neo is 29,659 L.
The A320neo carries 19% more fuel. And it has 17% more range. Big whoop.
Just to clarify - this fuel capacity in the A320neo requires the use of 2 cargo hold ACTs (auxiliary fuel tanks), the base aircraft actually carries about 1000l *less* fuel than the C919. Yet, even without the ACTs, it has longer range, likely due to lower empty weight.
See:
The first C919 airplane is scheduled to be delivered to China Eastern Airlines in December. China Eastern Airlines is set to receive its first (and the world's first commercial) C919 at Shanghai Hongqiao International Airport this Friday, 9 December 2022.
www.sinodefenceforum.com
(the data for the A320neo is without ACTs)
Still, I'd agree it's not a huge problem.
It is still baffling how it is worse when the A320 is basically a 1980s airframe though.
Generally speaking airframe technology has not advanced as much as engine technology since the late 1980s, especially if you forgo things like composite wings and fuselage like the C919 does. Some lot of the remaining gains can be retrofitted (e.g. newer winglets & re-sculpting the wing body fairing to compensate the effect of the bigger engines on wing pressure distribution, both of which Airbus did). So if the engines are the same two aircraft will perform quite similarly in terms of fuel burn, because that's where the vast majority of the efficiency improvement comes from.
More specifically, the C919 wing seems to owe a lot to the A320neo anyway. It has different wing tip devices and a smooth transition in TE sweep rather than a kink, but otherwise is very similar down to minor details like these:
The other, more interesting questions are (as others have mentioned) reliability and maintenance cost in service.