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MAX’s Return Delayed by FAA Reevaluation of 737 Safety Procedures

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MAX’s Return Delayed by FAA Reevaluation of 737 Safety Procedures

Old 13th Dec 2019, 17:33
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Originally Posted by Water pilot
I had an incident in my brand new Audi Q5 yesterday that illustrates the differences between Boeing's "you don't need to know" approach to engineering and what I consider the correct approach.
Great example. I was trying to keep mine simple, but apparently it was too simple.
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Old 13th Dec 2019, 20:04
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Originally Posted by Takwis
David P. Davies' solution to a slight pitch up into a stall in the 707 used only the elevator, not the much larger horizontal stab, and the solution was safe, effective, and benign. The MAX uses the stab, and trims forward for up to 10 seconds at a shot. That's at least an order of magnitude, maybe two, larger trim input than Davies'. I refuse to believe that a correction that large is "only feel."
The 10 second time limit is for when a pilot ignores the increasing angle of attack and increasing control force and continues to pull the wheel farther back, It's not a full-shot on every excursion. A pilot should take the hint and stop pulling all the way to stall unless they are really dedicated to it because that mountain isn't budging or a plane has ignored the Tower and started to taxi across the active runway.

The accident aircraft problem was the AoA system failed and provided ridiculously large values and the pilots were unknowingly provoking it further. Had the AoA system been accurate, none of this would be happening today.

Which leaves the question - is the greater blame for an instrument that generates false information or for a user of that data, like the stick-shaker and MCAS and airspeed and the pilots, which believes it? Unfortunately the aviation industry has long accepted that some planes will generate false AoA data and pilots will be forced to go through checklists to realize it's a false alarm.
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Old 13th Dec 2019, 20:42
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Originally Posted by MechEngr
The 10 second time limit is for when a pilot ignores the increasing angle of attack and increasing control force and continues to pull the wheel farther back, It's not a full-shot on every excursion. A pilot should take the hint and stop pulling all the way to stall unless they are really dedicated to it because that mountain isn't budging or a plane has ignored the Tower and started to taxi across the active runway.

The accident aircraft problem was the AoA system failed and provided ridiculously large values and the pilots were unknowingly provoking it further. Had the AoA system been accurate, none of this would be happening today.

Which leaves the question - is the greater blame for an instrument that generates false information or for a user of that data, like the stick-shaker and MCAS and airspeed and the pilots, which believes it? Unfortunately the aviation industry has long accepted that some planes will generate false AoA data and pilots will be forced to go through checklists to realize it's a false alarm.
Just to be clear: There was no AoA indication on the accident airplanes.

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Old 13th Dec 2019, 21:11
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Originally Posted by MechEngr
The 10 second time limit is for when a pilot ignores the increasing angle of attack and increasing control force and continues to pull the wheel farther back, It's not a full-shot on every excursion. A pilot should take the hint and stop pulling all the way to stall unless they are really dedicated to it because that mountain isn't budging or a plane has ignored the Tower and started to taxi across the active runway.

The accident aircraft problem was the AoA system failed and provided ridiculously large values and the pilots were unknowingly provoking it further. Had the AoA system been accurate, none of this would be happening today.

Which leaves the question - is the greater blame for an instrument that generates false information or for a user of that data, like the stick-shaker and MCAS and airspeed and the pilots, which believes it? Unfortunately the aviation industry has long accepted that some planes will generate false AoA data and pilots will be forced to go through checklists to realize it's a false alarm.
The blame is in the user of the data, a user of the data should have a data validation, which is what Boeing is working for MCAS. You are also putting on the same level warnings (stick shaker and air speed) with the MCAS which actuates a flight control. In case of MCAS is not a false alarm!
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Old 13th Dec 2019, 21:29
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MechEngr The 10 second time limit is for when a pilot ignores the increasing angle of attack and increasing control force and continues to pull the wheel farther back,
I have not seen anything stating that the MCAS paid any attention to pilot input. The length of the MCAS trimming appears to be solely determined by Mach and altitude. Lower altitude, close to ten seconds. Nice try on blaming the pilots again, though.

MechEngr A pilot should take the hint and stop pulling all the way to stall unless they are really dedicated to it because that mountain isn't budging...
The pilots of neither airplane got anywhere close to a stall...and in fact were pulling with all their might because the 'mountain' (rising terrain, ocean) wasn't budging.

Strike two.
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Old 13th Dec 2019, 21:52
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Originally Posted by Takwis
I have not seen anything stating that the MCAS paid any attention to pilot input.
Absolutely right. Certainly it didn't pay any attention to pilots pulling the yoke -- in fact, it specifically and deliberately overrode that column cutout switches -- secretly.

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Old 13th Dec 2019, 22:04
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I have not seen anything stating that the MCAS paid any attention to pilot input.
You mean other than MCAS ceasing to trim when the PF activated manual electric trim...
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Old 13th Dec 2019, 22:09
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Originally Posted by Icarus2001
You mean other than MCAS ceasing to trim when the PF activated manual electric trim...
MCAS 1.0 doesn't cease trimming on MET input. It merely pauses. And I hate to keep harping on this little detail but . . . it was a secret.
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Old 13th Dec 2019, 22:32
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And also, Grebe #4453

just a guess from this SLF- after turning them( cutout switches PRI and B/U off, they could not move trim wheel, and pulling on yoke did not work asit used to on the NG. But with switches on, at least the electric switches worked- not knowing that HAL ( MCAS ) would overrule them.
Electrical trim beats MCAS until stopped + 5 seconds.
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Old 13th Dec 2019, 23:26
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Originally Posted by OldnGrounded
I think we were imagining an MCAS with a shutoff switch. There is no procedure that I can see that would make MCAS 1.0 reasonably safe.

And about that trim wheel . . . I mean, what about that trim wheel?
Well- simply by pullling hard back on the yoke due to muscle memory while under negative g ( with no effect ) - then all you need to do is lean forward, unlock handle, and with about 20 to 30 lbs force tangential to wheel thruout the full revolution(s) simply crank about 10 turns per degree from near neutral trim while the mountain or cows or sailboats are getting bigger- isn't that what the manual infers when things go fubar. Yeager survived a mixup in 360 degrees of pitch, roll, and yaw- starting at about 60K feet- while with a broken rib. I guess the manual forgot to mention that any ' average' pilot should have been able to do all that by instinct with less than 100 hours in type . ...

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Old 14th Dec 2019, 00:49
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MCAS 1.0 doesn't cease trimming on MET input. It merely pauses.
Which is the whole point. MCAS DOES respond to pilot input. That is why the Lionair aircraft was able to continue flying, it was only with the change of PF and the lack of required "back" trim that the issue escalated. Ten seconds of back trim then turn off the trim and climb to a safe altitude.
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Old 14th Dec 2019, 00:50
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Originally Posted by OldnGrounded
MCAS 1.0 doesn't cease trimming on MET input. It merely pauses. And I hate to keep harping on this little detail but . . . it was a secret.
A secret to who? The Brazilian Certifying Authority knew about it and had it as a Cat B training item. Might be other countries also. It appears the FAA knew about it and bought off on not including it as a training item.

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Old 14th Dec 2019, 00:55
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This is a great analogy and discussion.
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Old 14th Dec 2019, 01:14
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Originally Posted by Icarus2001
Which is the whole point. MCAS DOES respond to pilot input. That is why the Lionair aircraft was able to continue flying, it was only with the change of PF and the lack of required "back" trim that the issue escalated. Ten seconds of back trim then turn off the trim and climb to a safe altitude.
My understanding is MCAS change of stab movement was at a much faster rate than the manual electric rate. This may have been another factor that surprised the crews as it did not move like a trim motor would.

So twenty seconds of "back" trim may have been required before turning off the trim.

How MCAS mk 2 will move (as in motor speed) has not been released.
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Old 14th Dec 2019, 01:22
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Brazilian Certifying Authority

It's very odd about that page. I think I saw the picture of it on Quora, but possibly another PPRuNer a while before. I can't remember. But whatever, it is such a few words in a tiny column given it's such a huge subject. A 47 feet, 1 inch subject. With what we know now, it should have had a page to itself, and been in bold red in every similar publication worldwide.
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Old 14th Dec 2019, 01:24
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Originally Posted by jimtx
A secret to who?
Almost everyone. This is really not a matter of question or dispute.

The Brazilian Certifying Authority knew about it and had it as a Cat B training item.
That's right, as we know from digging around for documentation. Maybe some of the pilots at Gol or whichever other companies bought it knew about it, too, but I've never seen any evidence of that.

Might be other countries also.
Yup, might be. Again, no evidence. But lots of evidence from companies and air crews who had no bloody idea.

It appears the FAA knew about it and bought off on not including it as a training item.
Well, that's alright then . . . Wait. Actually, no, it's not. That fact is at the center of the firestorm over this massive screwup by Boeing and the FAA that is well on its way to resulting in a year-long worldwide grounding -- in the wake of two hull losses and 346 splattered human beings. A screwup which, just by the way, has resulted in major damage to US leadership and prestige in civil aviation.

Seriously, folks, we are far beyond the point where it is even marginally-credible to blame the pilots for these crashes or to defend Boeing and the design and implementation of MCAS 1.0. Nobody is buying that narrative, certainly nobody who has conducted an investigation or is responsible for civil aviation safety, pretty much anywhere around the world.


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Old 14th Dec 2019, 01:26
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Originally Posted by Loose rivets
It's very odd about that page. I think I saw the picture of it on Quora, but possibly another PPRuNer a while before. I can't remember. But whatever, it is such a few words in a tiny column given it's such a huge subject. A 47 feet one inch subject. With what we know now, it should have had a page to itself, and been in bold red, and in every similar publication worldwide.
Yes, a couple of us posted it here. It's in this thread, somewhere. And you have described its appearance in the table quite accurately -- you have to read carefully to find it and it's easy to miss.
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Old 14th Dec 2019, 03:21
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Originally Posted by OldnGrounded
Almost everyone. This is really not a matter of question or dispute.



That's right, as we know from digging around for documentation. Maybe some of the pilots at Gol or whichever other companies bought it knew about it, too, but I've never seen any evidence of that.



Yup, might be. Again, no evidence. But lots of evidence from companies and air crews who had no bloody idea.



Well, that's alright then . . . Wait. Actually, no, it's not. That fact is at the center of the firestorm over this massive screwup by Boeing and the FAA that is well on its way to resulting in a year-long worldwide grounding -- in the wake of two hull losses and 346 splattered human beings. A screwup which, just by the way, has resulted in major damage to US leadership and prestige in civil aviation.

Seriously, folks, we are far beyond the point where it is even marginally-credible to blame the pilots for these crashes or to defend Boeing and the design and implementation of MCAS 1.0. Nobody is buying that narrative, certainly nobody who has conducted an investigation or is responsible for civil aviation safety, pretty much anywhere around the world.
It is a question of dispute. Who do you allege was trying to keep it a "secret"? What is a fact is that Boeing did not realize who they were selling airplanes to.
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Old 14th Dec 2019, 03:48
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There is no dispute. Boeing Technical pilot Mark Forkner asked and got the FAA to agree that MCAS wouldn't be included in the pilot's manuals. He succeeded, and, in his own words, used "Jedi mind tricks" to convince other regulators to do the same. Apparently the Brazilians are more resistant to Jedi mind tricks. Later, MCAS was modified to work at low speed and altitude, giving it more trimming authority, surprising even Forkner, who complained about not being given that information, but the FAA was not informed about the changes. These are all well documented events.
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Old 14th Dec 2019, 03:52
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It is a question of dispute. Who do you allege was trying to keep it a "secret"? What is a fact is that Boeing did not realize who they were selling airplanes to.
Nope -They knew exactly who they were selling to- the MAX had to be' the same ' as the NG other than cheaper to fly, and a few new shiny objects. And NO extra sim time. SW who was a major customer said if sim time. cut us a check for 1 Million per plane.

The most egrious issue was allowing a single sensor to take control from the pilot. And no mention, no flags, and no change relating to that issue in the paperwork. All else flows- follows from that choice. AS to pilots- ' average' doesn't cut it - west half of the bell curve always applies.
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