>Just like 95% of airliners. In fact the Max engine thrust line is higher and closer to the datum than most. Correct. >The Max's problem is not thrust line, i

>Just like 95% of airliners. In fact the Max engine thrust line is higher and closer to the datum than most. Correct. >The Max's problem is not thrust line, it is additional lift generated by the forward-mounted engine nacelles at high AoA which reduces stick-load and makes pitch-up to a stall likely. Nothing to do with thrust. Nothing you've written here contradicts what I wrote previously, so I'm not sure if you're just aggressively agreeing with me, but I'll assume that this is the case. Yes, the aircraft is dangerous at high AoA, as I wrote in my previous comment.