> According to a detailed FAA briefing to legislators, Boeing will change the MCAS software to give the system input from both angle-of-attack sensors.
> It will also limit how much MCAS can move the horizontal tail in response to an erroneous signal. And when activated, the system will kick in only for one cycle, rather than multiple times.
> Boeing also plans to update pilot training requirements and flight crew manuals to include MCAS.
> These proposed changes mirror the critique made by the safety engineers in this story. They had spoken to The Seattle Times before the Ethiopian crash.
> The FAA said it will mandate Boeing’s software fix in an airworthiness directive no later than April.
After the fixes are implemented I wouldn't worry too much about it. Lots of planes have had terrible design flaws that were fixed. The pre-MAX 737 included.
Sure, but none of those planes (in the last 30 years or so) had two full hull losses within month of each other with brand new planes.
I'd be more concerned by the regulatory capture that permitted this to happen than the specific model of aircraft.
My uninformed assumption is that once a suitable issue is isolated some sort of remediation (training/software/airframe/cockpit) all under the onset of various international gov bodies. No idea if the is a 1 year or 5 year process.
There are big PR risks in that approach, though.
Ignoring all other issues pointed out in TFA, two really stand out: The use of a single AoA sensor for a "Hazardous" component seems flat out wrong to me. The ability of MCAS to cause maximum deflection of the trim, rather than some limit (2.5 vs 0.6 is a quibble compared to 2.5 vs unlimited) also seems bad.