> "What's different is that at low speed, high thrust, and high angle of attack, the elevator of the MAX does not always have enough pitch moment to reduce the

> "What's different is that at low speed, high thrust, and high angle of attack, the elevator of the MAX does not always have enough pitch moment to reduce the angle of attack." It's my understanding that for the 737 NG as well, there are stall scenarios at particular speeds, levels of thrust and angles of attack where trimming the stabilizer is necessary to recover. That the difference between the NG and MAX is what those particular values are, not whether or not that scenario exists ever.