Originally Posted by
ktcanuck
When all is said and done, the one common indicator is the AoA reading on the Cap's side. Debate everything else till your heart's content.
Why did it flip to ~75deg at 150kn? More interestingly, why did it flip back to "normal" for a moment just before end of flight before flipping back to error?
I assume the slowly diverging altitude readings relate to the AoA stuck at 75 while pitot static reads ok...
Boeing's proposed fix includes shutting off the "required" MCAS when AoA disagrees so this is kind of important.
Whisky Tango Foxtrot guys? What's happening to that vane or the electrons/code behind it?
Maybe it is just simple plain old grounding also why the other sensor messed up , combined with a very bad qa at boeing trying to push more and more of the planes out of the factory more mistakes made
Both incident planes had issues within months of delivery i would love to see the issues on the other 380 they had delivered