Posts by user "OldnGrounded" [Posts: 45 Total up-votes: 95 Pages: 3]

OldnGrounded
2025-06-17T13:44:00
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Post: 11904315
Originally Posted by ignorantAndroid
I'm honestly mystified by the obsession with TCMA. The FADECs control almost every aspect of the engines, so there must be numerous ways they could cause a failure or uncommanded shutdown. So, even if we assume that the engines failed due to faults in the FADECs, why assume that TCMA would be involved?
I think you may be inferring something that isn't actually true. It certainly isn't true in my case. Wanting to explore the details of a function known to be designed to shut down engines, in a case where unexplained shutdown of engines appears to be a likely cause or contributing factor, doesn't suggest that we are assuming TCMA is involved. It's just exploring the details of a a function that is designed to do that and doesn't put on a light, smoke and sound show, or produce obvious debris and residue, when it does.

I think those of us who are persistently trying to learn the details of the sensor inputs to and logic of TCMA (I prefer that characterization to "obsessed with") understand quite well the points you make here — at least those of us whose interest survives in this new thread. However, I at least, and I believe others as well, have also come to the tentative conclusions that (a) the accident aircraft had engines providing little to no useful thrust from nearly the first moments after rotation, and (b) the only possible reasons for that which have been considered here so far involve the sudden and approximately simultaneous shutdown of those engines, most likely by interruption of fuel flow (because that's one of the very few things we know that can do that without producing big bangs, flames and smoke, etc.).

Surely it's more logical to simply posit that some unspecified bug in the FADEC software caused the failure. That bug could be related to TCMA, but it could just as easily involve any one of the dozens of other subroutines that likely exist.
I don't agree that it's more logical to posit that something we don't know about has shut down the engines rather than something that we do know about that is intended to shut down engines. Do you know of other routines/subroutines in the FADEC that shut down fuel supply?

Various posters seem to assume that all it takes is an incorrect air/ground signal, and the engines would shut down.
I certainly don't assume that and I haven't seen posts from others (that I consider serious and reasonably well-informed) that "seem to assume" that.

But in fact it would also require the FADECs to read the thrust levers as being at or near idle... AND the engines failing to respond to closure of the fuel metering valve.
Yes, we know that.

I've read the entirety of both threads, and I haven't seen anyone even attempt to explain how a malfunction within the airframe could cause both of those things to occur on both engines (or even one engine!).
Right, and you won't see a serious attempt to do that until we know, at least, what specific sensor inputs the TCMA function uses to determine the air/ground state of the aircraft and the logic that uses those to make the determination.


Last edited by OldnGrounded; 17th Jun 2025 at 13:46 . Reason: Formatting

Subjects: Engine Failure (All)  Engine Shutdown  FADEC  Fuel (All)  Fuel Pumps  TCMA (Activation)  TCMA (All)

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OldnGrounded
2025-06-17T14:04:00
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Post: 11904324
Originally Posted by Musician
At this point, I feel we can only rely on information being official if it's published through an official website, or if there's independent reporting or a video clip from an official press briefing.

I do believe the accident was not caused by an animal strike, for many reasons.
But I wouldn't believe it based on unsourced reporting alone.
Yes, but . . .

In the world we live in, much information, especially early in an investigation like this one, comes from insiders/officials speaking on background or anonymously (for various reasons) to their media contacts. Even the most conservative and responsible publications have little choice but to base reporting, at least partly, on such sources. Whether or not to trust such reporting, and how much to trust it, is left to us to decide. Personally, I'm convinced that the Times trusts the sources of its reporting and typically applies good judgment and good journalistic practices in making such determinations.

Subjects: None

2 users liked this post.

OldnGrounded
2025-06-17T17:09:00
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Post: 11904475
Originally Posted by JPI33600
Question to avionics specialists again. Below is the main drawing of the TCMA subsystem, included in the patent document . I can't stop scratching my head about the link I have circled in red in the center of the image. AFAICS, this link shunts the internal RUN path of TCMA entirely : the RUN signal is supplied by the RUN contact of relay assembly 52, then goes through the common and RUN contacts of relay 22, then goes through the common and RUN contacts of relay 28, then exits TCMA subsystem 18 by wire 124, and... we're back to square 1, because of the link. So TCMA subsystem 18 doesn't actually control the OPEN relay 118 of the HPSOV, only the CLOSED relay 100, and in the case where relay 22 and/or 28 are activated, both coils of HPSOV could even be energized at the same time.

Obviously enough, this isn't a real circuit diagram, but shouldn't this link be removed from the patent drawing?


Odd link in TCMA patent drawing
Good catch. When I quickly scanned the drawing, I stopped when I realized that it wouldn't tell me how the function actually works in the real world \x97 pretty normal for patent applications. Unless I misunderstand (it happens), I think you're right. That link doesn't make sense.

Subjects: High Pressure Shutoff Valve  TCMA (All)

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OldnGrounded
2025-06-17T20:23:00
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Post: 11904625
Originally Posted by DaveReidUK
The Indian AAIB successfully downloaded both FDR and CVR data from an Air India 787's EAFR relating to an incident in 2018, so your misgivings on that account are unfounded.
And they do have a new lab, as of this past April:

AAIB sets up flight recorders laboratory

New Delhi, Apr 9 (PTI) Aircraft Accident Investigation Bureau (AAIB) has set up a flight recorders laboratory that will help it in carrying out more effective probes into accidents.
Civil Aviation Minister K Rammohan Naidu inaugurated the laboratory in the AAIB premises in the national capital on Wednesday.
More at linked site. The lab opening is also featured in the slide show on the top page of the AAIB website, following a series of slides for International Yoga Day.

Subjects: AAIB (All)  AAIB (IDGA)  CVR  DFDR  EAFR  FDR

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OldnGrounded
2025-06-18T03:19:00
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Post: 11904867
Originally Posted by 25F
Once upon a time. I've had my own words in a Wikipedia edit [1] crop up in a Sunday Times biographical article a couple of weeks later, copy-and-paste. The worrying thing about this is that the Sunday Times article then becomes the "cite" that validates the initial claim.

[1] because I had got fed up with the inaccuracies. You may also thank me for correcting nonsense about fuel levels on Apollo 11, just before the 50th anniversary articles all started using Wikipedia as their starting point.
I don't find your experience with the Times overly surprising. Sloppy research and reporting makes its way into the best news publications, which is why I was careful to use the modifier "generally" in the post you quoted. Copying and pasting from Wiki without attribution is certainly egregious. Still, I feel comfortable with the assumption that the Times/Sunday Times does indeed generally follow good journalistic practices. I accept that the reporter(s) did speak with "Indian authorities" and that those authorities did tell the reporter(s) that a bird strike had been ruled out.

As I said, I'm also pretty confident that the Indian authorities are competent to determine whether there was a bird strike. It would be fair to ask whether I'd be confident in that if they told the reporters that there was a bird strike or that they hadn't ruled it out. I'd have to admit that I'd probably have some difficulty with that, given that I think it would be obvious to us , even with as little evidence we have so far, if birds had taken out those engines. But I hope I wouldn't be too sure that I'm right and they were wrong.

And yes, thanks for correcting those fuel levels. I'd want them to be right if I consulted that Wiki entry. I often use Wikipedia as a starting place, but I remember that it's an encyclopedia and if I have more than a passing interest in the material of an entry, I follow and assess the cited sources there before reaching any conclusions.

Subjects: Bird Strike

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OldnGrounded
2025-06-18T11:54:00
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Post: 11905176
Originally Posted by Lead Balloon
Yet the (a?) patent application for the TCMA addition to the EEC was filed by Boeing.
Yes, and Boeing specifies at least some of the functionality required in the FADECs.

Subjects: TCMA (All)

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OldnGrounded
2025-06-18T12:15:00
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Post: 11905190
Originally Posted by syseng68k
Lead Balloon:

The requirement for TCMA may have been specified by Boeing, but that doesn't tell us who designed and built the solution in this case, though it must have been a collaborative effort between the two parties.
Yes, but Lead Balloon's posts on this were in response to your post suggesting that "you can't blame Boeing" because the engines and FADECs were built by GE. The real-world question might be who can't blame Boeing? I think the answer is probably that everyone who thinks blaming Boeing is advantageous would at least try to do so. And specification and collaboration would likely be and adequate basis for trying.

Again, I'm not suggesting that TCMA is causal or contributing in this accident, and I understand that there are multiple reasons why that is unlikely even if the air/ground determination was erroneous. I just still want to know what the air/ground inputs and logic are, because there just aren't many things we know about so far that could cause what most believe was at least an important contributing factor.

Edit: As Lead Balloon points out, it was the FAA that required TCMA. The fact remains that Boeing patented at least one version of the function and specifies/collaborates in implementation with the engine manufacturers — more than enough participation for anyone seeking to blame Boeing for (purported) failures.

Last edited by OldnGrounded; 18th Jun 2025 at 13:02 . Reason: Clarification after noticing Lead Balloon's correction.

Subjects: FAA  TCMA (All)

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OldnGrounded
2025-06-18T15:28:00
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Post: 11905332
Originally Posted by OPENDOOR
It could equally refer to the APU which some have suggested either started or was in the process of starting.
Yes, but it's clear from context that the WSJ story is referring to the RAT and whatever they may understand from their sources is connected to it.

The emergency system is known as a ram air turbine. It is a small propeller that drops from the bottom of the 787 Dreamliner\x92s fuselage to serve as a backup generator.
The story is paywalled, so the link that pops up for me may not work for you, but in case it does:

https://www.wsj.com/business/airline...QPg1BBGQ%3D%3D

Subjects: APU  Generators/Alternators  RAT (All)

OldnGrounded
2025-06-18T18:04:00
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Post: 11905429
Originally Posted by FullMetalJackass
Do you recall the issue with the hydraulic PCU in 737s?. If you don't, they had a design flaw which led to the loss of two 737s including crew and passengers and even then, it took YEARS before the root cause was identified.

The time between the introduction of the 737-200 and the first crash due to the rudder reversal was around 24 YEARS. Then it was another 3 years until the second repeat occurrence which led to another crash. And only after another incident happened in yet another 737 in 1996 where the crew were able to land their stricken craft and tell the tale, could they finally identify the root cause.

This is the first crash / hull loss of the 787. Taking the design flaw of the Boeing 737 as a baseline and the time taken to identify it, to claim that "if there was a design fault, we'd know about it" is premature, to say the least.
Emphatically yes. This is both correct and important to understand. The first rudder hardover crash, UA 585, was in 1991. The second, USAir 427, was in 1994. The first NTSB report concluding that the probable cause was the PCU servo was not issued until 1999, in the USAir investigation. As FMJ says, that only happened because the Eastwind 517 PCU servo issue resolved (what? spontaneously? independently?) and the crew was able to recover control and land safely. The whole story is fascinating, enlightening and sobering.

Sometimes it's really, really difficult to determine the cause(s) of a catastrophic failure of a complex system and it may take a long time.

Subjects: NTSB

8 users liked this post.

OldnGrounded
2025-06-18T18:12:00
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Post: 11905438
Originally Posted by N8477G
We test and re-test modern aircraft for every imaginable failure mode during the design, certification, and production process.
Sadly, we don't really do that. No one could. The tests can be only for those failure modes already known and those that are anticipated or imagined at any given time. In systems as complex as modern airliners, there will almost certainly always be others no one imagined before they appear on in-service equipment.

Subjects: None

2 users liked this post.

OldnGrounded
2025-06-18T23:16:00
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Post: 11905612
Originally Posted by sycamore
As an ex-tp, I would consider those cut-off switches a danger, and they should have guards either side of each.
Shirtsleeves/watches etc. can get caught, lift switch.
Very poor design. Would not pass `military-muster.`
They're guarded by the switch design/operation itself. To move one of them, the toggle handle has to first be pulled outward.

Subjects: Fuel (All)  Fuel Cutoff

6 users liked this post.

OldnGrounded
2025-06-19T00:08:00
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Post: 11905632
Originally Posted by Kraftstoffvondesibel
But what about whats inside and behind the switches? How is the signals from them transmitted to the valves? Analog? Digital? Software? They seem to be part of the same LRU, what does it look like on the inside? same multi-cable harness too? Same multi-connector? I believe this has not been touched upon.
I don't know. We can look.

Subjects: None

OldnGrounded
2025-06-19T00:13:00
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Post: 11905634
Originally Posted by 25F
I've done a quick search and found articles in the Guardian, the Independent, the Mail (and no doubt many more) with the same misleading (if not wrong - depends how strict you are) information that I felt the urge to correct in the Wikipedia page. Mostly from 2020 or so, predating my update but at least one Guardian article from late 2023. But these could then become cites to "correct" the page back to its original form!
OK. I don't doubt that you can find such articles, probably all the time. But that's not actually relevant as a response to the part of my post that you quoted. Nor are any of those newspapers the one we were talking about earlier. Personally, I can't imagine seriously trusting the Daily Fail. And there's a reason the Guardian is affectionately known as the Grauniad \x97 and it's not merely because of typos.

Subjects: None

1 user liked this post.

OldnGrounded
2025-06-19T03:23:00
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Post: 11905696
Originally Posted by EXDAC
The issue with 5G was the potential for interference with some models of radio altimeter. I think we have been told that RA is used in 787 air/ground logic. We have also been told that air/ground state is used to enable TCMA.

I think it very unlikely that 5G interference was a contributing factor but I can see why someone would be interested in asking the question.
I think the cellphone interference concern is indeed partly focused on radio altimeters, and also on some voice comms. 5G shouldn't be problematic for the altimeters though. Modern ones operate at around 4.2-4.4 GHz, IIRC, and that's pretty far from any of the three bands 5G uses. I seem to remember reading that EASA tested for 5G interference and that it permits 5G use in the cabin. Whether that's true or not I don't know. And it wouldn't be easy, or even realistic, to police it in an airliner cabin.

Subjects: TCMA (Air-ground Logic)  TCMA (All)

OldnGrounded
2025-06-19T13:06:00
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Post: 11906009
Mods, feel free to remove this if you think it's not contributing.

Folks, the exchange here about the cutoff switches ("fuel control switches") is exactly the kind of discussion that contributes meaningfully to our collective understanding of one possible causal or contributing factor in the accident. Smart, well-informed people politely considering and evaluating the suggestions of others. No snark or sniping. Love it.

Subjects: Fuel (All)  Fuel Cutoff

16 users liked this post.

OldnGrounded
2025-06-19T13:51:00
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Post: 11906035
Originally Posted by bbofh
Has anybody the skill, knowledge, hands-on system familiarity or diagrammatic access to examine the
Ground/Air,
gear-handle,
gear doors
gear position lights
emergency extension,
Throttle lever position and
W.o.W. circuitry - in any sanguine detail?
I hope/wish. I accept that it's not at all likely that TCMA is the/a culprit in this crash, but it is, like the cutoff switches, one of the few things designed and intended to shut down an engine in a very big hurry. It would be good to know as much as possible about how it determines the aircraft's ground/air state.

And add the radio altimeter(s). I think, but don't know, that they provide inputs to the FADEC TCMA function also.


Last edited by T28B; 19th Jun 2025 at 14:38 . Reason: brackets completed

Subjects: FADEC  Fuel (All)  Fuel Cutoff  Gear Retraction  TCMA (Activation)  TCMA (All)

1 user liked this post.

OldnGrounded
2025-06-19T13:55:00
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Post: 11906038
Originally Posted by retiredCSE
I have read that TCMA can not activate unless TL set to idle.
I'm pretty sure that's not true. Everything I've found or read, and authoritative posts by tdracer, indicates that the required condition is thrust, as measured at N2 IIRC, higher than thrust lever position commands. The lever(doesn't) hsve to be at idle.

Subjects: TCMA (All)

1 user liked this post.

OldnGrounded
2025-06-19T13:59:00
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Post: 11906042
Originally Posted by LGB
Any indication from known videos as to what height the RAT comes on, around 400' AGL, or well before reaching 400' ?
I haven't seen any videos, or heard of any, that might tell us when the RAT deployed. It was definitely below 400' AGL, because the airplane never got that high.

OK, enough quick, consecutive, posts from me for now. Off to do required chores.

Subjects: RAT (All)  RAT (Deployment)

OldnGrounded
2025-06-20T13:45:00
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Post: 11906985
Originally Posted by soarbum
Thanks to tdracer's explanation on TMCA (albeit 747 not 787), we know that TMCA is a logic block within the FADEC whose only external inputs are a logic signal from the aircraft that indicates whether it is on the ground or not and throttle position as determined by two independent resolvers per throttle side.
Emphasis added.

Do we know this? If we do, I've missed it. And whether the FADECs receive signals independently from the sensors used to determine the air/ground state of the aircraft \x97 radio altimeters, WoW switches, something else I don't know about \x97 or receive a predetermined state or forwarded signals from another source is crucial to understanding possible failure conditions and the likelihood of simultaneous shutdown by TCMA in both engines. I think.

Subjects: FADEC  TCMA (All)

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OldnGrounded
2025-06-21T02:34:00
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Post: 11907450
Originally Posted by FrequentSLF
SLF here,

With what might be a stupid question, however let me ask.
Why the ground logic does not incorporate the wheel up command?
Well, in the context of the systems we're talking about here, why would it? The requirement is to "know" the actual air/ground state of the aircraft. The position of the gear lever doesn't help with that and might, if part of the voting, contribute to misidentification of that state.

Subjects: Gear Retraction