Not a lot is being said about how far they are pushing the technology here. I started out on the P/WJT8-D-9 and 11 on the DC-9. These engines were designed in the 50's and had a compression ratio of about 15 and a bypass ratio of less than 1. The LEAP engine has a bypass ratio of 11.1 and an overall compression ratio of 22.1, which is huge. Consider that this 22.1 ratio is accomplished only with aerodynamic means. The internal airflow aerodynamics must be very complex and this engine will most likely require FADEC that flies the engine like the flight control computers on a stealth airplane.
The CFM-56 is reliable and works just fine. Put oil and gas in it and away you go. I hope they get this one worked out. They are really stretching the technology here.