Posts about: "Fuel Cutoff Switches" [Posts: 802 Pages: 41]

DaveReidUK
July 17, 2025, 17:30:00 GMT
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Post: 11924532
Originally Posted by ex FE Hoppy
And the FAA responded by issuing a notice that the switches are fine in response to the Indian report which brought up an unrelated issue as if to muddy the facts.
FAA confirms that they didn't certificate the 787 with potentially dangerous fuel control switches ...
JustusW
July 17, 2025, 17:30:00 GMT
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Post: 11924533
Originally Posted by BrogulT
And (correct me if I'm wrong) I believe you've dismissed the notion of hiding the suicide and making it appear to be an accident, murder, someone elses fault, etc. I think that notion might be more common than you would think (after all if they are successful you wouldn't know...) and probably reflects a significantly different sort of mental issue. A depressed narcissist? IDK.
I fear we could discuss comorbidities until we're blue in the face. But no, I wouldn't dismiss the possibility of it being suicide, no. I just consider it to require any kind of actual prove instead of prove by the inability to come up with better explanations. As for the topic of concealment: It's obviously a grey area but the previously quoted 10-30% prevalence is based on studies trying to figure out exactly that. I certainly wouldn't feel comfortable opining on that number.

Originally Posted by BrogulT
IDK whether you've addressed this earlier, but I'd point out that people with suicidal thoughts are often indecisive .
Originally Posted by ferry pilot
Suicide is often impulsive. A sudden, unplanned leap from a balcony, bridge or precipice is a single motion with almost guaranteed terminal result. Unfortunately an airplane in the hands of a depressed or mentally unstable pilot can also be a single, impulsive motion away from instant, painless death. As demonstrated, a couple of flicked switches and a very short wait.
Unlike previous pilot suicides that took deliberation and often aggressive action, this appears to be a passive event that could have been conceived and executed in the same impulsive instant. Followed almost immediately by regret, denial and even a futile attempt at reversal.
Originally Posted by za9ra22
There's lots, psychologically speaking, wrong with this scenario too. I'd be much more convinced that this was an impulsive act or a psychotic one than that it was a planned suicide, meant to happen this way.
Suicidal ideation does frequently present with both imagined as well as examined scenarios. Especially in more severe cases many victims have a history of attempts. The impulsive variants are typically in lesser severities of depression and are actually more common in people with lower levels of suicidal ideation. It would certainly be the most likely scenario for a suicide that I could come up with. It's especially prone to happen in cases with sudden traumatic events on top of an existing baseline condition but can occur in any other condition as far as I know. It would also fit somewhat with an unremarkable history as a person suffering from mild to moderate depression might consider being able to cope on his or her own. And then obviously be less prepared for a spontaneous urge. The troubling part here is that it would be indistinguishable from an action slip without additional evidence as to the pilots state of mind. The observable scenario would be something like this: Immediately upon reaching v2 the Captain moves both fuel cutoff switches to their off state in quick succession. When queried by the FO he denies having done so and remains passive until impact.

This is a plausible scenario, but also one that would be impossible to determine causally. Try for yourself, but you can use either rationalization for the behavior and even use the same rationalization for the opposite behavior. There is no way to predict how anyone would react in that situation and no way to determine either way what that behavior indicates. Not even moving those switches back into the on position by himself would give a reliable clue as to his state of mind. The report would probably default to Human Error in this case, as the intent could not be determined.
The resulting suggestions, ironically, would be basically the same as well. Ease access to mental healthcare, improve training for avoidance, and most importantly: Improve resilience of systems against this type of action.

Based on the numbers available to us right now I can almost guarantee that if you have taken more than 10 flights in your life one or both of your pilots or colleagues on the other seat suffered from symptoms of moderate to severe depression. And you will with almost absolute certainty never actually know. The true question people need to ask themselves is "Do I want my depressed pilot to have access to psychotherapy or not?"
EDML
July 17, 2025, 17:46:00 GMT
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Post: 11924539
Originally Posted by Triskelle
An interesting quotation from this: "She highlighted a similar incident during which one of the engines suddenly shut down midflight on an All Nippon Airways Boeing 787 during its final approach to Osaka, Japan, in 2019.

Investigators later found that the aircraft’s software had mistakenly interpreted the plane as being on the ground, triggering the thrust control malfunction accommodation system, which automatically moved the fuel switch from “run” to “cutoff” without any action from the pilots."

Is it also interesting that this incident occurred at the time of ground-to-air transition?
Totally wrong.

The TCMA shuts down one or more engines - but it doesn't move the switches to cut-off in any magical way. TCMA directly operates the fuel valves - but the switches stay on.
Of course there is no entry for the switches being operated on the EAFR when TCMA shuts down an engine!
MedicAn
July 17, 2025, 17:56:00 GMT
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Post: 11924544
Originally Posted by Musician
Assumed: a pilot moved both fuel switches to CUTOFF, and that caused the accident.

Argument against intent:

6. The airline stated that the captain's medical records were found "unremarkable".



Not a strong argument against; the majority of completed suicides examined by the US military didn't have indicators of serious MH issues (or suicidal ideation) in either the medical record, nor was family aware.

The study of suicidality is interesting, when it comes up against the examination of an event like this (whether murder/suicide is a possible explanation, why it might or might not be). Non-medical people will often focus on something that's a red herring because it seems strange in the context of a potential suicide, but in terms of the "natural history" of suicide, it might be a pretty common thing. I've been inv with suicide investigation as part of my work, and in some ways it's as frustrating to try to inform laypeople about what norms exist in that field as I imagine it must be for the professional pilots to have dilettantes like me opine on throttles and CRM.



1stspotter
July 17, 2025, 18:26:00 GMT
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Post: 11924560
Originally Posted by EDML
Totally wrong.

The TCMA shuts down one or more engines - but it doesn't move the switches to cut-off in any magical way. TCMA directly operates the fuel valves - but the switches stay on.
Of course there is no entry for the switches being operated on the EAFR when TCMA shuts down an engine!
This is just *one * example of dozens of factual incorrect statements made by Mary Schiavo about aircraft accidents. I am surprised that any journalist still takes her seriously.
nrunning24
July 17, 2025, 18:52:00 GMT
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Post: 11924570
Originally Posted by syseng68k
Musician:

The lack of technical rigour and curiosity in this thread is disappointing. Long diatribes about switches, as if they were the only thing in the chain that could have cut off the fuel. Rumours and News, fine, but would expect a higher level of hard analysis here, especially considering the limited information presented in the initial report.

It may indeed be that the tragedy was intentional, but there is no hard evidence to show that at this stage. While there are pointers suggesting that in the report, that is how if has been written, intentionally. Here, the crew are blameless until proven at fault, beyond reasonable doubt. Call that naive if you will, but science is about gathering and following the evidence, not jumping to conclusions.
Pilots are blameless??? What are we even doing here. The evidence shows that outside a 10^(crazy number) event happening, the pilots are 100% to blame. How could you read the report and conclude any differently. As far as we can tell they flew a perfectly working airplane into a building.
Sailvi767
July 17, 2025, 19:39:00 GMT
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Post: 11924609
Originally Posted by EDML
Totally wrong.

The TCMA shuts down one or more engines - but it doesn't move the switches to cut-off in any magical way. TCMA directly operates the fuel valves - but the switches stay on.
Of course there is no entry for the switches being operated on the EAFR when TCMA shuts down an engine!
The displayed EICAS messages are very different when an engine is shut down via the fuel cutoff switch vice other reasons. The EAFR records those messages. I am quite sure they have eliminated the TCMA as a problem in this accident.
za9ra22
July 17, 2025, 19:47:00 GMT
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Post: 11924614
Originally Posted by WillowRun 6-3
I'd suggest some consideration about the use of certain terms in reference to the actions being attributed to the pilot who is said to have turned the fuel control switches off......
First, apologies for snipping almost all your post - it's not that I disagree with a word, but that we seem decreasingly able to read and properly digest what gets posted here, so I'd rather people read your actual post than my quote of it.

Secondly, even outside the question of legal definitions and legal liability, I've become increasingly concerned with the use of some terminology which doesn't just ascribe motives, but goes far enough to personally accuse a dead professional of many years standing, on the basis of no factual evidence so much as a wish to point the finger.

It's also rather ironic to participate in a Professional Pilot forum where non-pilots are criticised for their lack of knowledge and experience, then witness (presumed and apparent) professional pilots discussing human psychology and behavioural science as if they've been studying it all their lives.

I hope the mods can work out a framework by which this can be discussed without infringing on human decency and professionalism, but I can't see much sign without it that pprune would be a suitable place to further discuss the issues involved. The ad hoc editing done so far really isn't enough, despite the tough job they're doing.
ignorantAndroid
July 17, 2025, 20:08:00 GMT
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Post: 11924625
Originally Posted by Sailvi767
The displayed EICAS messages are very different when an engine is shut down via the fuel cutoff switch vice other reasons. The EAFR records those messages. I am quite sure they have eliminated the TCMA as a problem in this accident.
Indeed, there are dedicated parameters for TCMA:

Eng1_TCMA_Shutdown_Local_EEC_A
Eng1_TCMA_Shutdown_Local_EEC_B
Eng2_TCMA_Shutdown_Local_EEC_A
Eng2_TCMA_Shutdown_Local_EEC_B




OldnGrounded
July 17, 2025, 21:33:00 GMT
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Post: 11924681
Originally Posted by za9ra22:
I suspect it is written as it is because at this point, there is no evidence the investigation can provide as to how the switches 'transitioned', let alone why.
Originally Posted by OPENDOOR
You mean other than the glaringly obvious fact that they are switches designed to be switched from one state to another by a human hand?
As has been previously pointed out, there's a lot of confusion in these threads about what evidence is and is not. Staying away from legal dictionaries, because we aren't engaged in a lawsuit or criminal trial here, I like this, from Oxford:

"the available body of facts or information indicating whether a belief or proposition is true or valid."
The fact that "they are switches designed to be switched from one state to another by a human hand" is not evidence indicating how the switches "transitioned" in this incident. It tells us how they are intended to be operated and it tells us a way that they could have been "transitioned" and that's all it tells us. By itself, the fact of the intent of the designers tells us nothing valuable about what happened on this tragic Air India flight. It doesn't help us to decide, based on evidence, whether human hands actually did move those switches or, if they did, how or why those hands moved those switches. It just isn't evidence for answering those questions, one way or another.

These threads are dominated by posters who are either certain they know how the fuel control switches were "transitioned" by human hands (and increasingly why) and by others who continue to explore and posit possible mechanical or system failures (although those posts seem to be fewer than they were). And then there are a few of us who continue to point out that we simply don't have sufficient evidence to know or decide what actually happened. I think there would be more of us with that view if more of us were more careful in considering what actually is evidence in this case and, if something is evidence, what it may be evidence of.

Last edited by OldnGrounded; 17th July 2025 at 21:36 . Reason: Typo
tdracer
July 17, 2025, 21:52:00 GMT
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Post: 11924692
Originally Posted by sabenaboy
It really baffles me how the French prosecutor was able to come out just two days after the Germanwings 9525 crash and lay out the likely cause in remarkable detail \x97 even identifying it as an apparent suicide by the co‑pilot. Yet here we are with the Air India 171 crash: it took the AAIB an entire month to release a so‑called \x93preliminary\x94 report, and even then it\x92s vague, incomplete and raises more questions than it answers.

To me, this is unacceptable. If the French could piece things together and be honest about it in 48 hours, the AAIB should have been able to do better than this.
First off, as has already been pointed out, the French prosecutor was not working to ICAO standards for an accident.
Ok, so they put in the preliminary report that the captain intentionally turned both fuel switches to CUTOFF, causing the crash. The Captain and his family is vilified, criminal investigations are launched. Vengeful relatives of those killed in the crash attack - perhaps even kill - members of the captain's family.
Then it turns out that it's NOT what happened... The captain's reputation and his family have already been destroyed - irreparable damage has been done, and no amount of retractions and apologies for the mistake are going to correct that.

Is it really too much to ask that we allow the investigation team to verify and validate their information before we throw someone to the wolves?
GroundedSpanner
July 17, 2025, 23:02:00 GMT
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Post: 11924737
Originally Posted by jimtx
Why "There has been no defect reported pertaining to the fuel control switch since 2023 on VT-ANB." instead of: The mishap switches have been checked and have no defects. Their locking feature is operational.

They have the switches.
Because the preliminary report can only contain verified factual information.
"There has been no defect reported pertaining to the fuel control switch since 2023 on VT-ANB." - This will have been verified by the investigation team fairly rapidly. Verified reportable fact, included in the preliminary report.

Originally Posted by jimtx
"The mishap switches have been checked and have no defects. Their locking feature is operational.".
This could not have been done by the team in the time available. Bear in mind that the EAFR was not read until almost 2 weeks after the crash. Before that point there would have been little focus on the fuel switches, which were recovered in the run position (verifiable and reported). Once attention was directed to the switches, a small team will form just to forensically examine those switches. They will likely take WEEKS to even begin the detailed examination of the switches. Those switches have been through a crash and a fire. They dare not move them until every possible non-destructive examination technique has been used. What do you test first? just pulling the sleeve will move something. Moving the lever will move the contacts. Did fingerprints survive the fire?. You would want to x-ray them, measure wear on the locking, look at contact position. Electrically test the terminals. Does it need to be opened? They would get examples from the manufacturer and destructively test them.

Yes in the final report they would be in a position to make a statement like that. But in the preliminary - No.
jimtx
July 17, 2025, 23:53:00 GMT
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Post: 11924765
Originally Posted by GroundedSpanner
Because the preliminary report can only contain verified factual information.
"There has been no defect reported pertaining to the fuel control switch since 2023 on VT-ANB." - This will have been verified by the investigation team fairly rapidly. Verified reportable fact, included in the preliminary report.


This could not have been done by the team in the time available. Bear in mind that the EAFR was not read until almost 2 weeks after the crash. Before that point there would have been little focus on the fuel switches, which were recovered in the run position (verifiable and reported). Once attention was directed to the switches, a small team will form just to forensically examine those switches. They will likely take WEEKS to even begin the detailed examination of the switches. Those switches have been through a crash and a fire. They dare not move them until every possible non-destructive examination technique has been used. What do you test first? just pulling the sleeve will move something. Moving the lever will move the contacts. Did fingerprints survive the fire?. You would want to x-ray them, measure wear on the locking, look at contact position. Electrically test the terminals. Does it need to be opened? They would get examples from the manufacturer and destructively test them.
Yes in the final report they would be in a position to make a statement like that. But in the preliminary - No.
A visual inspection would verify if the body had a dog and the barrel lined up with it and was behind the dog. Report had nice big pics of exemplar switches and low resolution small pics of mishap switches.
appruser
July 18, 2025, 00:25:00 GMT
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Post: 11924773
Originally Posted by Mrshed
So I've looked again and I think that basically the ADS-B data is 5 seconds out.

So in the diagram (can't modify right now but I will), the blue bar starts at 5 and ends at 13, max altitude marker at 8.

That would tie in with loss of power.

It would put, interestingly, engine cutoffs right at the earliest opportunity within the window available with sampling etc.

(Incidentally an apology to Musician who I incorrectly told earlier that such a movement would be inconsistent with max altitude record, I can see clearly now this isn't the case!).
Apologies for the delay in responding to your posts. I see that you and others have stepped in, thanks.

I think for various reasons the ADSB data's absolute values are offset by some amount, for possibly all of the parameters. But there should be consistency in the deltas for the timestamp (by receiving station), the raw baro altitude, the Flightradar24 AGL values, and the airspeed. Flightradar24 themselves note that for altitude " ... the data is not above ground level, but it is consistent to itself."

08:08:46.55 ... 575ft ... 21ft ... 184kt
08:08:48.14 ... 600ft ... 46ft ... 179kt
08:08:48.61 ... 600ft ... 46ft ... 177kt
08:08:49.01 ... 600ft ... 46ft ... 177kt
08:08:49.46 ... 625ft ... 71ft ... 177kt
08:08:49.92 ... 625ft ... 71ft ... 174kt
08:08:50.39 ... 625ft ... 71ft ... 174kt
08:08:50.87 ... 625ft ... 71ft ... 172kt

From the Preliminary Report's airport cctv picture, the RAT was seen deployed at, by my estimate here , 150ft baro altitude, between 4-7 seconds after rotation. So the ADSB readings have to be prior to that.

What's interesting is that the ADSB data covers:
- 4-5 seconds of time (let's approximate 4 seconds from 46.55 to 50.55, ignoring the 0.32s for the moment)
- 50ft of altitude gain
- Declining airspeed from the 1st reading to the last in this final segment from the runway.

Big questions in my mind:
1. If the loss of ADSB corresponds to the E1/E2Fuel Cutoff switches being moved from RUN -> CUTOFF, why is the airspeed declining for the prior 4 seconds?
2. In 4 seconds, why is there only 50ft of altitude gain? that seems odd.
3. To account for only 50ft of alt gain, if we assume the 1st reading is on the runway just before rotation, the intermediate +25ft alt gain is at rotation (Nose up but MLG still on the runway), and the last 4 readings are in the air (nose up an additional 25ft), that means that 1 second or less after lift-off, ADSB was lost - this is before E1/E2 FCO RUN-> CUTOFF.

It's just weird .

Last edited by appruser; 18th July 2025 at 00:41 . Reason: added a comma for clarity
Sailvi767
July 18, 2025, 01:32:00 GMT
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Post: 11924794
Originally Posted by appruser
Apologies for the delay in responding to your posts. I see that you and others have stepped in, thanks.

I think for various reasons the ADSB data's absolute values are offset by some amount, for possibly all of the parameters. But there should be consistency in the deltas for the timestamp (by receiving station), the raw baro altitude, the Flightradar24 AGL values, and the airspeed. Flightradar24 themselves note that for altitude " ... the data is not above ground level, but it is consistent to itself."

08:08:46.55 ... 575ft ... 21ft ... 184kt
08:08:48.14 ... 600ft ... 46ft ... 179kt
08:08:48.61 ... 600ft ... 46ft ... 177kt
08:08:49.01 ... 600ft ... 46ft ... 177kt
08:08:49.46 ... 625ft ... 71ft ... 177kt
08:08:49.92 ... 625ft ... 71ft ... 174kt
08:08:50.39 ... 625ft ... 71ft ... 174kt
08:08:50.87 ... 625ft ... 71ft ... 172kt

From the Preliminary Report's airport cctv picture, the RAT was seen deployed at, by my estimate here , 150ft baro altitude, between 4-7 seconds after rotation. So the ADSB readings have to be prior to that.

What's interesting is that the ADSB data covers:
- 4-5 seconds of time (let's approximate 4 seconds from 46.55 to 50.55, ignoring the 0.32s for the moment)
- 50ft of altitude gain
- Declining airspeed from the 1st reading to the last in this final segment from the runway.

Big questions in my mind:
1. If the loss of ADSB corresponds to the E1/E2Fuel Cutoff switches being moved from RUN -> CUTOFF, why is the airspeed declining for the prior 4 seconds?
2. In 4 seconds, why is there only 50ft of altitude gain? that seems odd.
3. To account for only 50ft of alt gain, if we assume the 1st reading is on the runway just before rotation, the intermediate +25ft alt gain is at rotation (Nose up but MLG still on the runway), and the last 4 readings are in the air (nose up an additional 25ft), that means that 1 second or less after lift-off, ADSB was lost - this is before E1/E2 FCO RUN-> CUTOFF.

It's just weird .
I am not sure why 50 feet in 4 seconds seems odd right after liftoff in a heavy aircraft. That corresponds to 750 FPM. Seems entirely normal to me. The rate would have been increasing as the timeline advanced. I would also point out that RAT deployment verses the rat coming online fully are two different times. When that RAT is singled to deploy it bangs out nearly instantly. It begins producing its rated electrical and hydraulic power sometime after deployment.
The widely watched video shows a very normal initial rotation and climb.
jimtx
July 18, 2025, 03:23:00 GMT
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Post: 11924808
Originally Posted by tdracer
Yea DAR, it's time for another break. It's been days since anything really new has been posted - just hamster wheel arguments of the same theories, and even stuff that I thought had been thoroughly discredited, dead, and buried has come back to life (e.g. TCMA and the fuel condition switches both unilaterally changing state).

If something new comes up - then either reopen or someone can start a new one.
Yes, even the switch thing can go nowhere without "interim reports".
Spoiler
 


Last edited by T28B; 18th July 2025 at 13:32 . Reason: rant placed in the spoiler
appruser
July 18, 2025, 03:43:00 GMT
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Post: 11924815
Originally Posted by Sailvi767
I am not sure why 50 feet in 4 seconds seems odd right after liftoff in a heavy aircraft. That corresponds to 750 FPM. Seems entirely normal to me. The rate would have been increasing as the timeline advanced. I would also point out that RAT deployment verses the rat coming online fully are two different times. When that RAT is singled to deploy it bangs out nearly instantly. It begins producing its rated electrical and hydraulic power sometime after deployment.
The widely watched video shows a very normal initial rotation and climb.
It's a good point. If we're talking including the first 25ft or so after rotation the MLG is still on the ground; but when the lift-off occurs wouldn't it be nearer 1000fpm and accelerating upwards; after lift-off it would cover that height in 2 seconds or less.

Since the preliminary report states E2 cutoff after 3-4 seconds after lift-off, if that cutoff corresponds to ADSB interruption and which itself was only transmitting for 4 seconds, then 50ft after liftoff is a bit anemic?

But if we include the first 25ft after rotation but before lift-off, then, because the ADSB duration is only 4 seconds, it means that ADSB was interrupted before the E2 FCO operation. I don't know if there is a sliding window - part after rotation, part after lift-off that might meet all of these constraints.

That still leaves unexplained the declining airspeed seen in the ADSB data... did prior discussions on the ADSB data cover this? is there a good explanation?

Last edited by appruser; 18th July 2025 at 04:03 . Reason: fixed heights
Speedbard
July 18, 2025, 03:55:00 GMT
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Post: 11924822
I posted a week or so ago, on the forums generally, suggesting that the moderation of the Air India threads had gotten excessive, and at that particular point, it might even be an opinion I stand by. But reading through the last 100+ posts, other than the above few comments, it's just garbage. I'm sorry, to those who think they're saying something meaningful, but it's just hot garbage.

For the legal types - stop quoting what is, and isn't, the burden of proof. This is a forum on the Internet. The topic being discussed is an international investigation into a plane crash. For both of those things, there is no possible relevance to the burden of proof in legal cases in <whatever your country is>.

For the psychologists (both actual ones and those pilots who are moonlighting as one) - stop quoting psychological theory. Many of us know it, others don't, but we all have such an incredible lack of information about the pilots concerned that it's pointless mentioning it, except in passing. No one has time for pages of guesswork or instructions to the investigators on what they should be looking at.

For the tech guys who are still talking about the possibility of malfunctioning switches, please, stop. The pilot saying "why did you do x" is not consistent with a switch failure, you don't say that just because of an unexpected run-down, you say something more generic, like "holy smokeballs, dual engine failure". The specificity of the comment implies clearly observed action, specific to the switches, which aligns with the data record.

For everyone - just because something isn't absolutely mathematically impossible does not mean you can or should bring it out and eat up pages doing so. Investigations do not have to cover every single possible "what if", because in an unlimited universe no investigation would ever conclude. What they have to do is come up with the most likely scientifically derived assessed outcome for an already fairly unlikely event. I can accept people saying "We don't know for sure that the switches were operated deliberately" even though that's probably more likely than not. I can't accept the kind of argument which isn't dissimilar to: "Maybe there was a flaw with the switch detent, and a book fell off the console, and the previous crew had spilled water on it, making it slippery, and before that when the console was installed it was 1.5 degrees more inclined than it should be, and that caused the rollback. I accept that we're already in "unlikely event" scenario, but once the impossible has been eliminated, refusing to accept that there's probably 2-3 likely scenarios left, and instead inserting incredibly unlikely theoretical stuff... well that's just bad faith.

Finally, it's personal taste, but I remain a bit disappointed with the deliberate blindness being applied to inconvenient truths by some on here. The two currently most likely rational explanations are simple - deliberate pilot action, accidental pilot action. Either way, it's pilot action . As frustrating as some of the wild theories are, the obfuscation being pushed out by the "circle the wagons" brigade is just as bad. Any pilot knows that their life - and those of their passengers - relies on clear sightedness and not avoiding uncomfortable data points. So let's trust our instruments. There should be no absurd rush to judgement but also, please, let's not hide behind the "they were professionals, treat them with respect" stuff, endlessly. Someone selected fuel on both engines to cut-off, mere moments after they left the ground. It won't be an engine restart procedure (too low, too early), it won't be some bizarre technical problem that hasn't happened in millions of flight hours on other 787s worldwide. The CVR says "why did you do X" and the data recorder says "X happened". The two line up. What we don't know for absolute certain is why, so the only sensible things now being examined are:

1) Deliberate pilot action (can only assume harmful intent at Vr + 3 sec)
2) Accidental pilot action (due to severe cognitive disconnect, or "wallet in freezer" stuff)

I'm one of many being frustrated by the lack of CVR recording being released, because that will almost certainly identify whether it was 1 or 2. But it would be abnormal for that to happen, and I respect that until they're sure, if the CVR points to something, they will want it confirmed before releasing it, because whether it's 1 or 2, it's bad news for the families of that particular pilot.

Oh, and to whoever said "Ask yourself if we are ready to hear it?".... come on. Hundreds of people died. Ignoring a piece of evidence related to that because it might be uncomfortable hearing it is unacceptable, and a bit childish. It might be uncomfortable, but professionals follow the evidence, wherever it may lead, however uncomfortable it might be.

Sorry this sounds so angry. The cause is that having stuck my neck out and said "Why are you guys moderating so much" to the mods, a free run of the thread has revealed such nonsense being posted that I'm embarrassed about having said anything. Lock away, I say!
PuraVidaTransport
July 18, 2025, 04:13:00 GMT
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Post: 11924826
This reminds me of EgyptAir 990. Fuel cutoff switches thrown, other pilot asks why. Then a fight for engine restart. Captain El-Habashi fought so hard it cased a split elevator. I see this investigation taking many years as the reason for the crash is investigated, analyzed and debated. I can also see one party refusing to acknowledge the facts of the crash.

Let us remember the long history of pilots fighting to save their passengers. One or perhaps both (one in a billion, I know) of these men fought with everything they had to bring everyone home alive. The eight pilots on 9/11 all fought with everything they had. The captain of Germanwings who tried to get back into the cockpit. The Ethiopian Airlines captain and FedEx crew who fought and lived to tell about it. If there are evil intentions on an aircraft, I know without doubt the crew will do anything and everything to make sure I walk off the aircraft. So let's focus on that as we wait on the final report.
Mrshed
July 18, 2025, 05:07:00 GMT
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Post: 11924844
Originally Posted by appruser
Apologies for the delay in responding to your posts. I see that you and others have stepped in, thanks.

I think for various reasons the ADSB data's absolute values are offset by some amount, for possibly all of the parameters. But there should be consistency in the deltas for the timestamp (by receiving station), the raw baro altitude, the Flightradar24 AGL values, and the airspeed. Flightradar24 themselves note that for altitude " ... the data is not above ground level, but it is consistent to itself."

08:08:46.55 ... 575ft ... 21ft ... 184kt
08:08:48.14 ... 600ft ... 46ft ... 179kt
08:08:48.61 ... 600ft ... 46ft ... 177kt
08:08:49.01 ... 600ft ... 46ft ... 177kt
08:08:49.46 ... 625ft ... 71ft ... 177kt
08:08:49.92 ... 625ft ... 71ft ... 174kt
08:08:50.39 ... 625ft ... 71ft ... 174kt
08:08:50.87 ... 625ft ... 71ft ... 172kt

From the Preliminary Report's airport cctv picture, the RAT was seen deployed at, by my estimate here , 150ft baro altitude, between 4-7 seconds after rotation. So the ADSB readings have to be prior to that.

What's interesting is that the ADSB data covers:
- 4-5 seconds of time (let's approximate 4 seconds from 46.55 to 50.55, ignoring the 0.32s for the moment)
- 50ft of altitude gain
- Declining airspeed from the 1st reading to the last in this final segment from the runway.

Big questions in my mind:
1. If the loss of ADSB corresponds to the E1/E2Fuel Cutoff switches being moved from RUN -> CUTOFF, why is the airspeed declining for the prior 4 seconds?
2. In 4 seconds, why is there only 50ft of altitude gain? that seems odd.
3. To account for only 50ft of alt gain, if we assume the 1st reading is on the runway just before rotation, the intermediate +25ft alt gain is at rotation (Nose up but MLG still on the runway), and the last 4 readings are in the air (nose up an additional 25ft), that means that 1 second or less after lift-off, ADSB was lost - this is before E1/E2 FCO RUN-> CUTOFF.

It's just weird .
I don't believe those figures on ADS-B are airspeed, rather groundspeed. Which would make sense during a climb out that they would decrease (given a constant airspeed).