MAX’s Return Delayed by FAA Reevaluation of 737 Safety Procedures Mk II

[jimtx]

[QUOTE=Grebe;10645167]The length of this thread and its previous makes it difficult to refer to specifics and what the past and current semi- technical discussions have been- since most of the current questions have long since been addressed- discussed- ad naseasum

So I'm going to post a few links to different blogs- which if 0ne takes the time to read and figure out how to go to previous and following on the site(s) listed will at least provide mostly rational discussion.

https://www.satcom.guru/2019/10/flaw...-disaster.html

https://leehamnews.com/2019/11/29/bj...-crash-part-5/


https://www.moonofalabama.org/2019/0...g-737-ngs.html



B737 Max threads


And from a long ago post somewhere in prune news and rumours one can find the below






And re stick force found

https://www.satcom.guru/2019/03/taki...aiting-on.html

........ This aspect is essential in ensuring the pilot does not have to push the yoke to stop the plane from pitching up, which violates positive stick force per g as required in 25.255....

... stick force per g must be positive . ..

I think the slope of the stick force per G is positive. It's just not linear in the regime they are concerned with.