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OldnGrounded
2025-06-17T13:44:00 permalink Post: 11904315 |
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 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.
Various posters seem to assume that all it takes is an incorrect air/ground signal, and the engines would shut down.
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.
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!).
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) 5 users liked this post. |
OldnGrounded
2025-06-17T14:04:00 permalink Post: 11904324 |
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. 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 permalink Post: 11904475 |
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 Subjects: High Pressure Shutoff Valve TCMA (All) 3 users liked this post. |
OldnGrounded
2025-06-17T20:23:00 permalink Post: 11904625 |
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. Subjects: AAIB (All) AAIB (IDGA) CVR DFDR EAFR FDR 2 users liked this post. |
OldnGrounded
2025-06-18T03:19:00 permalink Post: 11904867 |
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. 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 2 users liked this post. |
OldnGrounded
2025-06-18T11:54:00 permalink Post: 11905176 |
Subjects: TCMA (All) 2 users liked this post. |
OldnGrounded
2025-06-18T12:15:00 permalink Post: 11905190 |
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) 2 users liked this post. |
OldnGrounded
2025-06-18T15:28:00 permalink Post: 11905332 |
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.
https://www.wsj.com/business/airline...QPg1BBGQ%3D%3D Subjects: APU Generators/Alternators RAT (All) |
OldnGrounded
2025-06-18T18:04:00 permalink Post: 11905429 |
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. 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 permalink Post: 11905438 |
Subjects: None 2 users liked this post. |
OldnGrounded
2025-06-18T23:16:00 permalink Post: 11905612 |
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 permalink Post: 11905632 |
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.
Subjects: None |
OldnGrounded
2025-06-19T00:13:00 permalink Post: 11905634 |
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!
Subjects: None 1 user liked this post. |
OldnGrounded
2025-06-19T03:23:00 permalink Post: 11905696 |
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. Subjects: TCMA (Air-ground Logic) TCMA (All) |
OldnGrounded
2025-06-19T13:06:00 permalink 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 permalink Post: 11906035 |
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 permalink Post: 11906038 |
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 permalink Post: 11906042 |
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 permalink Post: 11906985 |
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.
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) 1 user liked this post. |
OldnGrounded
2025-06-21T02:34:00 permalink Post: 11907450 |
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 |