Yes, certainly. There were a number of changes, some of which were not directly related to the accident. There were some discoveries with respect to the need to separate some wire bundles to prevent some common failures. A lot of the work was done with respect to software changes to the flight control computer, specifically with MCAS, to limit the power and the frequency in which MCAS can fire. MCAS can only fire once per flight now.
The use of the electric trim switch on the control column can actually disable MCAS, which was not the case before. Its authority in terms of the degree and the rate to which it can change the angle of the horizontal stabilizer is limited to allow the pilot to overcome that input. There are some features added that allow a comparison between the left and right AOA sensors that will prevent the propagation of errors through to the following systems.
A lot of it, in addition to those changes to the flight control computer, involved changes to the procedures to allow for improved pilot awareness—in other words, situational awareness in failure modes or failure scenarios that can still occur. One of the key findings of the accidents and our post-accident investigation was the degree to which the pilots in general were not prepared and not trained to deal with the types of failures that are deemed possible. That's a common theme.
We also discovered that the simulators that were used for training were not programmed to demonstrate the faults that actually occurred in the accidents. That has been fixed.
Then, of course, Transport Canada went above and beyond and recognized that the erroneous firing of the stick shaker, which is part of the stall warning system, is deemed to be extremely distracting and definitely a negative in respect to pilot workload. The failure case, which is still possible within the aircraft, trips off a number of what we call “cockpit effects” that the pilot has to deal with. In our judgment—and the EASA agreed with us—the ability to disable that erroneously firing stick shaker was a required improvement to reduce the pilot workload in these foreseeable failure scenarios to an acceptable level.
That's a sort of very high-level summary.