| > was unstable No, it was not unstable. It just behaved differently enough that some additional pilot training would have been needed without MCAS. > rather than design an inherently safe All jetliners are unstable and require active augmentation. > they apparently were attempted No, they were not. The procedure is: 1. trim to normal with the electric trim switches 2. turn off the stab trim switches. That's it. https://theaircurrent.com/wp-content/uploads/2018/11/B737-MA... The LA crew never turned off the trim after trimming to normal. The EA made a different mistake - turning off the trim when it was too far from neutral. Neither the Seattle Times nor The Guardian are reliable sources on aviation. Aviation Week is a lot better. The Times author apparently did not read the EAD he cited. I'll quote from it the relevant bit: https://theaircurrent.com/wp-content/uploads/2018/11/B737-MA... "Initially, higher control forces may be needed to overcome any stabilizer nose down trim already applied. Electric stabilizer trim can be used to neutralize control column pitch forces before moving the STAB TRIM CUTOUT switches to CUTOUT. Manual stabilizer trim can be used before and after the STAB TRIM CUTOUT switches are moved to CUTOUT." Note that the flight data recorder showed that both crews had moved the trim back to normal with the trim switches, and neither thought to then turn it off. |
Quoting Boeing with my own emphasis:
> MCAS, or Maneuvering Characteristics Augmentation System, is a flight control law implemented on the newer models of the 737 to provide consistent airplane handling characteristics at elevated Angles of Attack in certain unusual flight conditions only.
Which, to be clear, means it's intended to stabilize the plane ("consistent") in circumstances where the physical design of the plane would render the plane unstable (inconsistent) in certain operating environments.
> The EA made a different mistake - turning off the trim when it was too far from neutral.
Do you have a specific citation for this? I'm digging through the ECAA report and am not able to find this specific mention. https://web.archive.org/web/20200310004955/http://www.aib.go... (original site is timing out)
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It seems you're generally suggesting that the instructions provided by Boeing were sufficient for the plane to remain airworthy without further mitigation; this was contradicted by the ECAA and others. Is this what you're suggesting?