I would bet that it is far more complicated and really can`t be put into laymans terms because to do so would open the explanation open to never ending (noob) questions that require a more advanced knowlwdge than the average ATOT member would have at their disposal!Since we're all family here, give us your take on the issue so us laymen can understand more clearly.
Also giving an automated system unlimited horizontal stabilizer and thrust authority was clearly a blunder in hindsight. Correcting an incipient stall needs a light touch, not a ham robot fist.
Oh, and any sensor disagree warning shouldn't be in a list of optional equipment...
well DUH....The automated system does not have unlimited horizontal stabilizer and thrust authority. It can ba shut off at any time. RECOGNIZING what the problem is IS the problem.
You're confusing unlimited with absolute or irrevocable. It appears, in fact, that the MCAS system was able to max out the stab trim in full nose down position, without predefined limitations.The automated system does not have unlimited horizontal stabilizer and thrust authority. It can ba shut off at any time. RECOGNIZING what the problem is IS the problem.
But to fit the new LEAP-1B engines, Boeing had to make some changes to the general design of the 737. To sum up the changes, Boeing added new split tip winglets, a new tail cone, revised APU and exhaust inlet. The Seattle based manufacturer also removed the aft-body vortex generators.
Additionally, Boeing included a higher nose gear and new display screens for the pilots. While these changes don’t seem to be very radical, their eventual impact would be very significant.
The new nose gear put up the aircraft’s nose higher than usual. With the new engines generating a lot more power, the nose went up even more. After conducting various tests, Boeing realized that their new jet is a bit too prone to encountering stalls in certain situations.
The decision to move the engines, change the CG, and use MCAS to compensate was fine. (Although these are still links in the error chain that lead to the failure)
For catastrophic failures system design should generally be two fault tolerant. At the bare minimum one fault tolerant with the second level of fault tolerance coming from human or software intervention.
The main egregious design failure as near as I can tell was assuming that two sensors made the system one fault tolerant. Sure it may work to swap from a failed sensor to a good sensor but this was apparently sensor disagreement. Without three sensors in a voting logic scheme it’s extremely difficult to determine which sensor has drifted and which is still true.
What should have happened was upon the two sensors disagreeing the system should have stopped functioning and/or alerted the pilots to take action.
Of course the disagree light was not included on the base Max8.
As it was the system was 0 fault tolerant to a catastrophic hazard.
Which is the second egregious failure. These hazards should have been identified and they weren’t, in part because the FAA allowed Boeing to perform the oversight function.
I’m sure this whole thing is going to be taught in hazard analysis training for years to come.
Any explanations (or rather, theories) as to why we haven't seen this problem with US-Based airliners yet?
Maybe they paid for the disagree light? Or they are just better trained pilots?
You're confusing unlimited with absolute or irrevocable. It appears, in fact, that the MCAS system was able to max out the stab trim in full nose down position, without predefined limitations.
Apparently I also have a complete lack of understanding of basic airplane characteristics, because I don't know why that would happen. Unless the engines are mounted too low under the wings. Hm, maybe the root problem is they couldn't redesign the aircraft to mount the engines higher?Obviously this poll is tongue-in-cheek, but the first option shows your complete lack of understanding of basic airplane characteristics. More thrust increases nose-up pitch and excaberbates stall - the condition trying to be avoided in the first place.
A button to modify the gravitational constant of the universe. You people are amateurs.
There needs to be an option in the poll for not letting executives make engineering decisions
True, but Boeing also made a deliberate strategic move to focus on shareholder value, and lifted and shifted a lot of work from Puget Sound to Charleston, mostly to circumvent the unions. From a stock standpoint, they’ve been wildly succesful. From an engineering, quality and ethical standpoint...Easier said than done. The overall project is always coming from management. You will always find an element of budget pressure and schedule pressure in any engineering failure.
Remove management pressure and these kind of failures will almost never happens.
Mostly because no project will ever complete without budget and schedule pressure.
The mitigation for this is an independent or external safety review organization. Normally that’s the FAA. Instead, because all regulations are bad, we let Boeing regulate itself.
Is Boeing getting sued yet? This is so disturbing and negligent its unbelievable, quite frankly they shouldn't exist as a company anymore for withholding such key information.
Obliviously aviation is complicated, as a passenger I would like to know that the pilot has 100% control of the plane when they need it, there has to be an easier way to kill automated systems and go full manual control.
Any explanations (or rather, theories) as to why we haven't seen this problem with US-Based airliners yet?
Maybe they paid for the disagree light? Or they are just better trained pilots?
