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Originally Posted by nnn
(Post 30973476)
If using electric trim inhibits MCAS until five seconds after electric trim is released, and the ET pilots used electric trim before the last MCAS activation before the crash, do we know why the pilots wouldn't have used the electric trim to bring the plane all the way back to in-trim? Or did they? I'm confused by that. Also why they wouldn't have hit the cutouts again right after releasing the electric trim.
It appears they did re-engage the electric trim (which it appears did reengage MCAS inputs) What is not clear is whether manual trim inputs were effective and that is why the electric trim was re-engaged or if the plane was flying too fast and manual trim was difficult? IDK |
Originally Posted by mduell
(Post 30974940)
Pilot error is the most obvious possibility.
Talked to some ("first world") pilots today and most of them agree that the single sensor AOA sensor design should have never made it into a commercial airliner and that the AD is very badly written. The one thing that is stressed there is to set the switch to "CUTOUT" and keep them on "CUTOUT". By the time they would find out that manual trimming does not work, it is already too late to reactivate electric trimming, which will also reactivate MCAS. |
Originally Posted by worldclubber
(Post 30974990)
No, it is not!
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Originally Posted by mduell
(Post 30975436)
Took too long to identify the problem (putting them way out of trim) and then turning electric trim back on after disabling it (not found in the runaway trim procedure) suggests pilot error to me.
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Originally Posted by worldclubber
(Post 30974990)
No, it is not! It is rather an aircraft design that forces pilots to jump through a number of (previously unknown) hoops to keep the MAX from crashing due to a flawed system that will happily fly the plane nose first into the ground.
Talked to some ("first world") pilots today and most of them agree that the single sensor AOA sensor design should have never made it into a commercial airliner and that the AD is very badly written. The one thing that is stressed there is to set the switch to "CUTOUT" and keep them on "CUTOUT". By the time they would find out that manual trimming does not work, it is already too late to reactivate electric trimming, which will also reactivate MCAS. |
Originally Posted by prestonh
(Post 30975816)
I believe there are 2 aoa sensors on the max. At least that is what the FDR output shows.
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Originally Posted by mduell
(Post 30975823)
Indeed. One is used at a time for all Flight Control Computer and MCAS functions, same as the prior 737s.
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Originally Posted by worldclubber
(Post 30975846)
One at a time is not good. Prior 737s had no MCAS.
At the end of the day, the 737 is not a fly-by-wire aircraft; it can be flown with all pilot assist systems turned off. Boeing needs to address the tendency of the MAX to put the pilot into a dangerous situation more frequently than other models do, and they appear to be doing so. However, at the end of the day, the control belongs to the pilot. I have no wish to speak ill of the dead, but given the preliminary details that have come out so far, I believe responsibility will ultimately be shared between the plane and the pilots. I also think there is little to be gained by continuing to try to figure out exactly what percentage of blame belongs where when the investigations are still underway. I think it is far more productive to wait and to see what is done to address the problem and to certify the updated plane. At this point, until new information is available (and possibly not even then), I don't think anyone is going to change anyone else's minds. |
Hey Everyone - I asked this back on post #1061 and didn't see an answer so if anyone could help me out here, that't be awesome. I just don't understand all the forces involved; here's my question:
"Pardon my ignorance with the next question as I am not an ATP or even multi-engine pilot. If you lockout the stab in full "nose-down" deflection, then hold the yoke as far back as possible, all other forces being equal, would you be able to fly the aircraft at least somewhat nose level ? Or, once that stab is fully deflected down, is your 737 "going down" as well ?" |
Originally Posted by worldclubber
(Post 30975846)
One at a time is not good. Prior 737s had no MCAS. |
Article in USA Today - probably not very informative [for us] but it is bringing up more doubts and questions to the general public: https://www.usatoday.com/story/news/...em/3378703002/
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Originally Posted by jsloan
(Post 30975914)
I have no wish to speak ill of the dead, but given the preliminary details that have come out so far, I believe responsibility will ultimately be shared between the plane and the pilots.
However, I believe that the plane contributed a lot to make the holes in the Swiss cheese align.
Originally Posted by prestonh
(Post 30976025)
AF 447 flew straight into the ocean with input from 3 ADIRUs and the crew couldn't figure out how to get control of that plane either.
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Originally Posted by worldclubber
(Post 30976894)
Nice try to direct attention away from the flawed MAX. ^ |
Originally Posted by halls120
(Post 30976923)
It's a relevant comparison. The co-pilots flying that aircraft didn't know how to respond to a series of anomalies and put the aircraft in a stall from which it couldn't recover. We don't know the final outcome of the two MAX crashes at this time, but in addition to the Boeing design failures, I suspect there will be findings similar to AF 447, which cited a lack of experience of both co-pilots is hand flying the aircraft and poor training.
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Originally Posted by PVDtoDEL
(Post 30976930)
I don't know why you would suspect that there will be similar findings - the preliminary report seems to indicate that the pilots were well trained and followed all procedures until they were stuck in an unrecoverable situation. From the report, they seem competent - expecting anything more is both unreasonable and unrealistic.
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