Originally Posted by
Zeffy
I second the thanks!
On first read-through, problematic dodging, bobbing and weaving are apparent. Seems like a lot of CYA effort that no informed reviewer taking a hard look would be likely to quietly accept.
Example from page 14 of the document:
I'm going to guess that means that countering single unintended MCAS activation by "elevator alone" applies to a single, max. 2.5 unit movement of the stabilizer, not to the combined effects of multiple (presumably pilot-interrupted) movements caused by unintended activation. Unless, of course, Boeing is confident that "elevator alone" recovery is possible after MCAS has run the stab to the stops.
Also, from page 35:
Discussed but not documented and then . . . not referenced.
There's a lot more in the document. I'm sure others will find and share.