Engine thrust related nose up forces would be less on the MAX as the engines are closer to the CG and CL. What is being compensated for is the change of the ce

Engine thrust related nose up forces would be less on the MAX as the engines are closer to the CG and CL. What is being compensated for is the change of the center of lift as the AoA changes because of where the engine nacelle is and how big it is. Also, the data that you are expecting the FAA to report on was not being collected by the FAA. You will also note the FAA did not provide any data on how frequently the TOGO switch is used in the Atlas Air investigation, because just like MCAS it is a system that may be activated on normal flights.