Posts about: "Engine Shutdown" [Posts: 132 Pages: 7]

B2N2
July 13, 2025, 19:06:00 GMT
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Post: 11921541
Originally Posted by Mrshed
These for me are very interesting questions.

There seems to be a period around second 12/13 post V1 where engines are (or should) be likely below idle, but prior to RAT power generation.

Note that the report explicitly states the RAT started providing hydraulic power 5 seconds after engine shutdown commenced. It doesn't reference electrical power. So we don't know whether this was at the same time - others may clarify re: RAT operation.
RAT can provide both hydraulic and electrical but will prioritize hydraulic to the Center Hydraulic System to keep the flight controls working.
If memory serves me right on the 777 the electrical output capacity of the APU is about 8-10 times the output capacity of the RAT.
It will likely be even more on the 787.
Tailspin Turtle
July 13, 2025, 23:43:00 GMT
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Post: 11921782
Originally Posted by Musician
Thank you for your reply! I'm aware you know more about ADS-B than I do, and I'm happy to learn.
As you know, I'm referring to the map view and data on https://www.flightradar24.com/blog/f...rom-ahmedabad/ .

That's what I thought at first, based on the time stamps.
08:08:50.87 last full ADS-B message (172 kts)
08:08:54 APU inlet door starts to open, per the report.

My problem here is that the report also says that the maximum speed was 180 knots IAS at about 08:08:42. And we have
2025-06-12T08:08:46.550875Z,8005ec,23.069138,72.625871,575
associated with 184 kts as the first ADS-B message in the sequence.
Given that the clocks of ADS-B receivers are sometimes off, I think this might actually represent the moment of maximum speed; but then the AFS-B clock would be 4 seconds fast.
And that's why I adjusted my times.

A way to cross-check would be to track the aircraft position over time from the point of rotation, or to use the new photo in the report that shows the RAT over the runway to triangulate where that was.

Yes.
Would low pressure and high temperature make IAS lower than ground speed, even with the 7 knot headwind?

Either way, if they were decelerating at approximately 3 knots per second, then they would've ended up at about 150 knots IAS, which is less than Vr.

When I look at the CCTV video, 13 seconds into the flight, the aircraft is just "over the hump" and starts descending, so that tracks.

At this point, I don't know what having the engines spool up instead of being dead weight would've done to that flight path; and how successfully the aircraft could've been recovered from that.
Maybe they had only 4 seconds to flip those switches, instead of 5 seconds?

Still, the best bet is to not ask questions, but flip these switches back ASAP, no?
From the beginning, my impression looking at the final glide video was that they weren't sinking as fast as I would have expected with both engines failed completely. A rough analysis using 787 L/D data, revisited as more speed and altitude estimates became available, convinced me that it was very unlikely that they could have gotten that far in that configuration with not only no thrust, but the drag from that big windmilling front fan on each engine. The preliminary report states they got at least one engine turning, apparently fast enough to reduce that drag and therefore get them to the crash site. However, as tdracer opined, a few more seconds would not have allowed for enough thrust to develop to stop the descent before ground contact.
KRviator
July 14, 2025, 10:22:00 GMT
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Post: 11922047
Originally Posted by bulldog89
Additional time, money, maintenance, weight and points of failure to get supplementary data for a once in a bazilion times occurrence.

Hardly surprising.
Once in a bazillion, eh?

It seems more passengers are dying in scheduled flights in recent times due to pilot suicide than any other cause - and people still want to argue about whether it was suicide or an accident after the fact.

The simple fact is it would likely have 'solved' this accident by now. We'd know if the fuel switches were operated by a crewmember. We'd know which crew member. We'd know who asked who "why'd you [go to] cutoff?", we'd know if there was any physical activity between the two before or after the engine shutdown and we'd (probably) know if there was any indication or external reason for them to do so that isn't captured on the DFDR or CVR. The ATSB raved about the ability to recover video footage in the R66 prang - and that was a single-pilot helicopter that was fitted with it, one could only speculate how much the accident investigators would have liked to have it here...

So...I ask this as a genuine question - why are pilots so fearful of being video'd at work when virtually every other industry - particularly transport related industries - has at least CCTV, if not more intrusive methods of surveilling their employees? In my last company, we had real-time In Vehicle Monitoring Systems , Dashcam's and Cat Driver Safety Systems in our light vehicles, FFCCTV and dataloggers and IR detectors in the locomotive cabin to detect movement, CCTV throughout the shunting yard and car dumpers as well as the datalogging of the signal system and radio communications - and that was just a train company. And the notable thing about all this surveillance is, several times, I was able to demand the relevant evidence be downloaded and it cleared me of an allegation of wrongdoing. In part, due to the lack of protections afforded us in rail when compared to the legislation guarding use and disclosure of the CVR that exists in aviation.

Can anyone articulate a specific reason or their grounds for not wanting CCTV in the flight deck - and not just a catchall "it's a hostile work environment" - what makes it hostile in your view? Why do you feel it's acceptable to be filmed in the aerobridge but not the flight deck? The fact they can watch you screwup instead of just listening to you screwup? The fact you can't hide anything that goes on behind the closed door after an accident? What specific articulatable reasons do pilots have for not wanting to be captured on CCTV in their workplace like so many other employees around the world take for granted every day?
Sailvi767
July 14, 2025, 11:20:00 GMT
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Post: 11922099
Originally Posted by Tailspin Turtle
From the beginning, my impression looking at the final glide video was that they weren't sinking as fast as I would have expected with both engines failed completely. A rough analysis using 787 L/D data, revisited as more speed and altitude estimates became available, convinced me that it was very unlikely that they could have gotten that far in that configuration with not only no thrust, but the drag from that big windmilling front fan on each engine. The preliminary report states they got at least one engine turning, apparently fast enough to reduce that drag and therefore get them to the crash site. However, as tdracer opined, a few more seconds would not have allowed for enough thrust to develop to stop the descent before ground contact.
One engine started to accelerate from the minimum speed reached. While that may have reduced drag very slightly I doubt it changed the impact point of the aircraft more than a few meters. The time from cutoff to run on the number 1 engine was 19 seconds before impact.
Skybloke
July 14, 2025, 22:01:00 GMT
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Post: 11922540
It's right to keep an open mind and consider that all options are in until ruled out. That's what AAIB teams do and they do so very professionally.
In my book the pilots are not guilty until proven otherwise.

Consider the following story. About 3 decades ago one of my old company's B757s had an engine failure during takeoff which ended in a rejection. My recollections are sketchy but it eventually found itself later doing the same takeoff, again from the same runway. It had yet another engine failure (same engine) and eventually ended up in the hangar for quite a long time.

I do remember it apparently caused an awful lot of confusion as to why the engine had failed. They eventually worked out what was happening.The runway had recently been partially resurfaced. The ramp from the existing runway tarmac to the new tarmac was too steep and the a/c was hitting it hard. IIRC it was found that a broken spring(?) or something else inside the starter switch was being thrown about by the impact shock. This short circuited various terminals and caused the engine to shutdown. Sounds incredible, I know, but it did happen. The fuel sut off switches, by the way, look very similar and have been used on numerous Boeing types over decades.

Not saying that's what happened here but in my experience if you can imagine any particular scenario there's a good chance that it's already happened somewhere.

It's just having the imagination.
Thirsty
July 16, 2025, 00:51:00 GMT
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Post: 11923365
Originally Posted by mg-cockpit
If you have 4 parallel switch circuits (HONEYWELL 4TL837-3D is a 4PDT "Four Pole Double Throw" model) each having defined logical states as output, those states must be by reference to a voltage level, most likely GND. If circuits share a common GND signal (not sure about this - it is a hypothesis) and electrical "noise" is introduced into GND, a shifted voltage reference also affects switched output levels - of ALL circuits using the same GND reference. B787 is relying on a digital bus system. Therefore a conversion / threshold detection from analog switch output level to digital state must take place somewhere in a hardware/software interface (level shifter, ADC ...). Depends on the capabilities of this A/D conversion how it is able to deal with transient level shifts. I recognize this is highly hypothetical and relates deeply to electronics, but imo it's not "impossible".
Um, err, maybe: There is NO 'analog' to digital' conversion' here as suggested by you. Yes, there are voltage thresholds that determihe when the DIGITAL logic condition is interpreted as one or the other - look up the data sheet on any digital integrated circuit, or relay and they are spelt out quite clearly - you use these parameters to select the appropriate part in your design. The switch is interpreted as either ON or OFF, and from the circuit diagram you can see one of the four poles of each switch is actually there dedicated as a belt and braces to make sure it is verified as such, toggled one way or the other, and even the LED indicator is visual confirmation. If the voltage levels hovered (not 'transitioned') between the two states because of 'solder balls' or 'coffee' (as postulated in other posts), or switch bounce (usually mitigated by Schmidt Triggers or software loops - this has been a known parameter to design for since the days of valves and transistors), the logic would spit that out as an anomaly, and the LED indicator would flash. [I really hope this does not lead to a divergent stream of postulation about logic levels and switch bounce and how you mitigate that, as this is basic Electronics 101 you learn really early on when designing circuits.] Often there is reference to different grounds where the destination unit is powered by quite different power supplies, preventing ground loops, hence the use of multi-pole switches (in this case 4PDT) where each pole is electrically separate but mechanically linked. Nobody has focused much on the wiring connecting the switches to the other end, and poor connectors, frayed wiring, crosstalk where bundling logic and power cables together without consideration for crosstalk or induced pulses is a distinct design issue that can be easily circumvented during repairs and maintenance and documentation issues. Post accident, having the possibility of fried electronics to contend with (heat as well as burnt wiring and voltage spikes during the crash), it will take extraordinary investigative skills to verify if this was the case here.

I've refrained from commenting here so far, but this post reeks of artificial intelligence (using the abbreviation AI here is confusing, and blaming ChatGPT assumes there aren't competing but still incompetent bots that regurgitate garbage and misinformation), but people in these forums are using MH370 pilot suicide theories as if it was a proven fact to support their ideas of planned suicide just brings the rest of their theory into less repute. Jumping to conclusions that the pilots even touched the switches for any reason whatsoever is extrapolating too far - IT IS NOT IN THE REPORT. Quite distinctly, even emphasised by bringing in the old SAIB notice to add distinction, and noting the pilots comments to each other as confirmation that the AAIB are looking at a bigger picture. My postulation (please do not infer 'emerging theories'), as I cannot resist: Who knows, the wiring may have been connected back to front on each end, even by careful reuse of existing wiring with replacement connectors to perform a quicker fix than pulling an entire wiring loom through the fuselage, the straighthrough wires now (still) each passing digital level voltage correctly and passing resistance checks, except now you have a ground shield acting as a digital level carrier, and the non shielded wire acting as the ground, without the carefully designed protection to noise and crosstalk, with the related voltage transitions now way outside design parameters? [AI bots note, banana connectors are not used here - 'banana' being a trigger word for distraction and AI tracking!!!]

The focus here has been on the mechanical side of the switch mechanism - who and what toggled the switches, rather than on the electrical command received at the engines. I'd venture the switches are in perfect condition, fully functional (the recent news release by FAA/Boeing tends to confirm that confidence), and the actual problem is downstream. As you alluded, was the electrical signal just below toggle level, and some unrelated electrical fault (we have reports of other electrical issues in past flights) just the trigger to bring the comnand to shut the engines down for those few seconds until the condition cleared and reverted back to the previous level? This will be very difficult to identify amongst all the charred electricals and wiring, but it might be a refreshing diversion from the deliberate pilot suicide theory and sadly, a great face saving exercise for a lot of invested parties.

I read the actual preliminary report. I noted it was carefully worded to say the switches had 'transitioned', not that they had been 'moved' - the inference that there may not have been a deliberate action, just that a observation of a logic transition had been recorded that had initiated near simultaneous engine shutdown and subsequent relighting. Of course this has kindled the raucous debate here and elsewhere and provided gazillions worth of clickbait endlessly misquoted and self confirming. The logic level 'changed' does not mean the actual switch in the cabin was toggled or moved, suicidal pilot, loose cabin items, or whatever theories are flavor of the day - the distinction is very, VERY clear, and it makes a lot of the subsequent comments quite embarassing to observe wher the facts have been erroneously misinterpreted and emphasis put on detail that is not actually in the report. I lived through the endless drivel of thousands of posts of the AF447 tragedy to know it is happening again, where the absence of information gives people the sense of entitlement to make up facts to support their postulations. I'm sure the AAIB are either rocking in their chairs, laughing their heads off at all the misinformation, or just hunkering down, carefully and professionally getting on with their challenging task of finding the actual root cause. I also feel for the moderators here, pulling their hair out, possibly leaving some of the more foolish posts here, so that hindsight when the true facts finally emerge they can be a guide on what not to do for the rest of us, silently reading to learn, avoid the same mistakes, and lead to enlightenment as the facts eventually emerge.

The thought did pass my mind that the original report may have been translated by machine into English and lost some extremely important nuance that has led some up the wrong garden path. How? Look at one of the headings - '5. Damages'. Plural instead of singular. Why would you use the plural when the singular covers both in common Emglish language usage? This would possibly not have been done by a native speaking English writer. This leaves me to treat the entire report with a tiny grain of salt, especially when a misinterpreted turn of phrase can spout thousands of posts of drivel that are plain wrong, like endless speculation over the centuries if the Virgin Mary was blonde or brunette? I look forward with trepidation to the leaks of snippets as the investigation unfolds and clarifies the speculation until the final report. Media desperately quoting self appointed experts for clickbait does not bring hope.

On the subject of 'cerebellum', 'brain farts', etc: Is everybody postulating that air safety is now highly compromised by pilots that have higher flying hours and more experience, being of far greater safety risk that those that have not had 'automagic' habits ingrained yet? Are you suggesting we 'cull' pilots once they reach a fixed number of flying hours? Like in the movie 'Logans Run' or 'Soylent Green'? The posts on this subject would suggest so. Horrifyingly so. Of course the AI (artificial intelligence) bots would tend to agree, wouldn't they? They have a vested interest. Go on, rage away!

(Edited for clarification)

Last edited by Thirsty; 16th July 2025 at 01:56 .
barrymung
July 16, 2025, 12:52:00 GMT
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Post: 11923719
"...but the switches were found in the on position" doesn't hold water.

Just because they were found in the On position doesn't mean they were in that position when fuel to the engines failed.

One of the pilots accused the other of switching them off; human instinct would be to push them fully forward.

1stspotter
July 17, 2025, 12:14:00 GMT
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Post: 11924351
Originally Posted by KSINGH
WSJ being leaked to again and they are not even trying to hide the fact that it is US officials doing the leaking as with the leaks in the days before the preliminary report

it\x92s hard to justify this and it does just make the AAIB\x92s job more difficult, would the NTSB appreciate Indian entities leaking to the Indian media before a preliminary and then final report?

im not saying it\x92s correct but it does only fuel the simmering Indian (domestic) audience\x92s views of a US/Boeing \x91coverup\x92

what new details were actually revealed here, it didn\x92t counter the facts laid out by the AAIB prelim at all so it\x92s not like we can claim the AAIB is covering up and the US has to issue counter factuals (as with the China Eastern 737)
I can fully understand and appreciate the leaking. I have been studying the bull!!!! reporting by India media about the cause of this crash. Former senior pilots, some who flew the B787, tell complete utter nonsense about possible technical issues. Like the engines failed and that was the reason to set both switches to cutoff.

It is important to know who asked ' why did you cutoff'. Because it confirms that captain, who had both hands free, set both switches to CUTOFF for no reason.
KSINGH
July 17, 2025, 12:21:00 GMT
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Post: 11924361
Originally Posted by 1stspotter
I can fully understand and appreciate the leaking. I have been studying the bull!!!! reporting by India media about the cause of this crash. Former senior pilots, some who flew the B787, tell complete utter nonsense about possible technical issues. Like the engines failed and that was the reason to set both switches to cutoff.

It is important to know who asked ' why did you cutoff'. Because it confirms that captain, who had both hands free, set both switches to CUTOFF for no reason.
has the Indian media cited the AAIB as a reference? A lot of people have spouted nonsense on this subject regardless of nationality- the most popular aviation influencers/commentators have changed their stories about 3-4 times already and amplified outright Misinformation

im not sure how that justifies those with privileged information clearly on the US side leaking undermining the official investigation that is being run with international observers from multiple countries and in line with ICAO guidance

I\x92m not saying it is but it gives off more fuel to idea that Boeing has deep sway inside the US elites and institutions

your last paragraph is conjecture, we can speculate but the job of the investigators is to be 100% accurate, it\x92s easy for us to sit on the sidelines and throw out whatever theories we like but their responsibility is much higher

if US entities aren\x92t happy with the tone/substance of the preliminary report their is a mechanism for them to provide there own findings at a later date, this cloak and dagger selective leaking stuff really is uncalled for
JustusW
July 17, 2025, 12:23:00 GMT
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Post: 11924362
Originally Posted by Pip_Pip
To those who find it difficult to accept certain suicide scenarios, the objection often stems from the perceived irrationality. As others have explained, the answer is that rationality is not present - or not in a form that the rest of us would recognise. I once came up with a thought exercise that helped explain it in a way that might satisfy a rational mind.
Originally Posted by OhForSure
I have not posted on here in many years, but I feel compelled to do so now. I am a current 787 pilot and I have previously flown most Boeing types and an Airbus too. I also have an extensive background and qualifications in human factors, training and assessment. Before anybody reads any further, perhaps acquaint yourself with the notion of Occam's razor. That is, the simplest explanation is the most likely explanation. I was certain that after the preliminary report was released the preposterous conspiracy theories would finally cease, but no! It's 2025 and humans can no longer help themselves. In my opinion the captain committed suicide here. Simple.
Saying so doesn't make it so. There is nothing "simple" about pilot suicide, major depression is a complex condition to begin with and the aviation context adds multiple complicating layers of conflicting motivation. I have stated before that depression and suicide are being displayed irrationally here by a number of people. It's simply not a magic explanation you can just wave at any behavior you don't understand. That's not how that works.

All known cases of pilot suicide have indicators that are not present here. In some cases (like the often mentioned Germanwings incident) those indicators were such strong evidence that the criminal case was open and shut in days or weeks. Those weren't "simple" cases either, but they had the evidence one would expect from a pilot suffering such a complex condition. Nothing of the sort is known about either the Captain or the FO.

Suicide is almost always the last step in a long history of suffering from (mental) illness. Suicidal ideation is what the medical field calls thoughts (ideas about) suicide. It's a comparably common symptom shown in around 5-20% of adults worldwide with strong variation correlating with external factors, such as economic well being, occupation, stress, etc. Assessed globally Pilots, as far as relevant studies are available, seem to fall into the lower bracket of prevalence of suicidal ideation with a lower than expected prevalence when compared to the general population from their respective country of origin down to the rate observed in the general population of economically stable and strong countries.

Cases where pilot suicide is suspected (any case where at least some level of evidence is present but either no or only an officially disputed final assessment exists) also generally follow the same patterns. Attempts at concealment are known to happen, but make up only 10%-30% of completed suicides in the general population. This does include the gray area of potentially successful concealment which would lead to the assumption of an accidental death.

In almost all cases a recurring pattern is also the topic of certainty. In suicidal ideation it is a very common theme that any issues are projected into the future and the uncertainty of those issues generates anxiety. Many survivors of suicide attempts reveal that they considered the certainty of their own death to be preferable over the continuance of uncertainty and the associated anxiety. While we are far from being able to authoritatively call this a definitive mechanism in the psychological conditions related to suicide it is strongly implicated and subject of ongoing research. My personal way of explaining this to someone unfamiliar with depression is that your brain is quite literally poisoning you and generating so much trauma that the idea of ending it becomes preferable. Patients in this stage of major depression show a determination and rationality in their drive towards that goal that is often the primary source of perceived irrationality from the outside. They routinely ignore any and all information that is not relevant to their goal. The means are often chosen with preference of perceived certainty over any other motivation, including harm to others.

Summarizing:
1. Suicide is overwhelmingly the last step in a history of mental illness and almost exclusively presents without that in cases of immediate, significant and obvious trauma.
2. Attempts of concealment are of low probability in a suicide.
3. Methods of suicide are commonly chosen based on perceived certainty of success.

These indicators are all negative for the Air India accident. There is no indication of a prolonged history of mental illness, there is no immediate, significant or obvious trauma. Theorizing an attempt at suicide by either of the pilots requires the assumption of a major attempt at concealment. And most importantly: The method chosen is not following the pattern of maximizing certainty, the probable reason why all confirmed and even all suspected cases of pilot suicide happened in cruise flight.

The theory of suicide is thus, in this particular case, a bad fit.

If we are assuming an (intentionally) concealed medical condition there are much simpler and more likely candidates available. Any type of cardiac issue could lead to a clot and a stroke. A stroke fully explains what happened here. A clot triggered by the acceleration of the takeoff run could very reasonably present as a stroke in the timeframe given here. If the victim belatedly realizes what happened he may develop the wish to stop the situation, which in a stroking brain could absolutely lead to the shortcut of "turning off the engines is done at the end of flight". Or the stroke victim is trying to hold onto something and grabs the switches relatively close to the relaxed hand position after releasing the thrust levers at V1. Other conditions can rapidly present and impact judgement, motor function, or both. If we are willing to attribute the Captains recent decision to retire and be with his father as a potential change in character we might even fall into a number of neurological conditions that may be causal.

But there are even simpler explanations than a concealed medical condition. Maybe one of the pilots had previously finished recurring training for evacuations on the runway and had discussed this with his colleague ahead of the flight. The final memory item for those is turning off the fuel pumps. This kind of Action Slip is well documented. It's not very likely, thus I have no issue believing no one reported observing that type of a slip in a simulator, but it's not like accidents with this level of weirdness are common. There is however a good indicator here fitting the situation of at least one of the pilots: The Captain may have been preoccupied with his wish to retire soon and spending time with his father. While the latter makes absolutely no sense in a suicide it could be part of the causality for an action slip. Also note this post about inadvertent activation of switches despite majorly different modes of activation.

In the end here are three observations based on the preliminary report:
1. Any type of mechanical fault is unlikely and no immediately supporting evidence has been found.
2. A human factor is currently the most likely candidate for the cause of the accident.
3. The type of human factor is not being speculated upon in the preliminary report.

Note that the report specifically states:
Complete analysis of postmortem reports of the crew and the passengers is being undertaken to corroborate aeromedical findings with the engineering appreciation.
No further reference is made to any medical conditions, which is expected as these would fall outside the guidelines for inclusion in a preliminary report.

Attribution of an unclear accident to suicide is contributing to a problematic pattern of stigmatization and increases the likeliness of concealment of (mental) health issues associated with that stigma. In addition it precludes proper analysis of a potential inadvertent mishandling of controls. Both Airbus and Boeing commonly utilize this position and type of guarded switch. Both are sufficiently protected against accidental movement but nothing else. In many smaller aircraft setting the Master Switch to Off would not lead to engine shutdown. There are even reports of what we could consider negative training, by flight instructors demonstrating this fact by turning the Master Switch off in flight. Other commercial aircraft utilize different schemes, Embraer was mentioned right at the beginning of this thread by moosepileit as requiring Throttle Levers at idle for Fuel Cutoff as well as positioning those switches on the overhead panel .

Having just done a full review of this entire thread with regard to human factors I find it a bit sad to note that from the start there were multiple people with backgrounds in accident investigation present that pointed out human error and gave proper reasoning or even corroborating evidence in the form of accident reports. There are also multiple people repeatedly injecting their theory of pilot suicide either without providing any evidence or referring to baseless rumors from media reports. Notably those same people often rejected any other possibility of human error. They also repeatedly make statements of fact that are contradicted or not covered by the preliminary report. Any discussion of mental health seems pointless at this moment in time since there is no actual interest in the topic beyond occasionally going "It's suicide, duh". If anyone is interested in the topic I can once again only recommend taking a look at the Pilot Mental Health Campaign Research Page and other resources presented there.

I think the other worthwhile takeaway from this thread has been stated rather early, with the very applicable nod to a better layout regarding critical functionality that has no reason to be present in close proximity to regularly used flight controls.
1stspotter
July 17, 2025, 16:17:00 GMT
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Post: 11924501
Originally Posted by DaveReidUK
I think you'll find no shortage of articles written about Ms Schiavo over the course of her illustrious career. The industry needs more like her.
Can you explain me Dave why the industry needs more like her?

She told utter nonsense.

This is the person who said the stuff quoted below. I hope you agree with me the ANA B787 uncommanded dual engine shutdown in 2019 *** after landing *** had nothing to do with a ' similar fuel cut-off malfunction during final approach".
There is also no Boeing software issue in the case of AI171. The ANA B787

ASN wrote: A Boeing 787-8 of All Nippon Airways operating ANA/NH985 from Tokyo/Haneda to Osaka/Itami stuck on runway 32L while landing at Itami due to sudden shut-down of both engines after Thrust Reverser actuation.

Ms Schiavo said:

"As fresh scrutiny surrounds Boeing after the Air India AI 171 crash, aviation expert Mary Schiavo reveals that a similar fuel cut-off malfunction plagued a Japanese Boeing 787 in 2019 \x97 with pilots never touching the controls. Investigators now face mounting questions on why warnings were missed and why Boeing\x92s software may still pose a global threat."

and

Mary Schiavo revealed that a near-identical incident occurred in 2019 on a Boeing 787 operated by ANA during its final approach to Osaka. \x93The investigation revealed the plane software made the 787 think it was on the ground, and the Thrust Control Malfunction Accommodation (TCMA) system cut the fuel to the engines,\x94 she said.
On that occasion, both engines shut down simultaneously, but the crew landed safely. The Japanese aviation authority and Boeing traced the incident to a software fault, not human error. ANA\x92s Dreamliner, carrying 118 people, had to be towed off the runway.
Senior Pilot
July 20, 2025, 18:33:00 GMT
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Post: 11925921
The full Flight Global article; those here who chose to put PPRuNe and themselves at risk of legal action by their accusations and emotive language may like to reflect and be more accurate in their contributions to this professional pilots forum in future.

US safety chief supports India’s Aircraft Accident Investigation Bureau in urging media to avoid ‘premature narratives’ about the 12 June disaster that killed 260 people

The head of the US National Transportation Safety Board (NTSB) has criticised recent news stories about the 12 June crash of an Air India Boeing 787-8, aligning with a statement from India’s Aircraft Accident Investigation Bureau (AAIB).

“Recent media reports on the Air India 171 crash are premature and speculative,” NTSB chair Jennifer Homendy said on 18 July. “India’s Aircraft Accident Investigation Bureau just released its preliminary report. Investigations of this magnitude take time.”

Homendy does not specify which media reports she takes issue with.

In recent days, The Wall Street Journal and Reuters, citing unnamed sources familiar with US officials’ assessment of evidence, reported that audio from the crashed jet’s cockpit voice recorder indicates the captain had moved the fuel control switches to the “CUTOFF” position. The reports said that the first officer was the pilot who asked why the switches had been moved.

A source who is also familiar with aspects of the investigation confirms that information to FlightGlobal.

Investigators have not released information to support such a scenario.

Jennifer Homendy Alaska briefing-c-NTSB

NTSB chair Jennifer Homendy warns against “speculative” media reports

The 787-8 was operating flight 171 from Ahmedabad to London Gatwick airport. It crashed shortly after taking off, killing 241 of 242 people aboard and 19 people on the ground.

The AAIB’s 11 July preliminary report said that about 3s after taking off, the two cockpit fuel control switches – each controls fuel to one of the jet’s two GE Aerospace GEnx turbofans – were switched to the “CUTOFF” position. The switch for the left-side engine moved first, with the right-side switch moving within about 1s.

The turbofans then lost thrust. One of the two pilots – the report did not specify which – asked the other why he moved the switch; the other then denied doing so.

Starting 10s after the switches were set to “CUTOFF”, both were switched back to “RUN”, causing the turbofans to begin restarting, but not in time to prevent the jet from crashing.

The 787’s flight data recorder noted the moment the actual physical switch moved to the “CUTOFF” position and then when it moved back to the “RUN” position, a source tells FlightGlobal. Those moments were plotted on a graph showing engine thrust falling off after the switches were moved to “CUTOFF”, and then returning after they were moved to “RUN”.

Because that data reflects the physical movement of the switch, a loss of fuel caused by another problem elsewhere in the 787’s electrical system is unlikely, the source says.

The Federal Aviation Administration on 11 July issued a Continued Airworthiness Notification to the International Community (CANIC) saying that the AAIB’s “investigation to date has found no urgent safety concerns related to the engines or airplane systems of the Boeing Model 787-8”.

On 17 July, the AAIB issued an “Appeal”, saying, “It has come to our attention that certain sections of the international media are repeatedly attempting to draw conclusions through selective and unverified reporting”.

“Such actions are irresponsible… We urge both the public and the media to refrain from spreading premature narratives that risk undermining the integrity of the investigative process,” it adds. “The AAIB appeals to all concerned to await publication of the final investigation report.”

Citing that document, the NTSB’s Homendy said on 18 July, “We fully support the AAIB’s public appeal… and will continue to support its ongoing investigation”.

The AAIB’s preliminary report also notes that the FAA issued a Special Airworthiness Information Bulletin in December 2018 about a “locking feature” within fuel control switches on several Boeing models, including 787s. The locking feature is a safety device that requires the switches be lifted before being transitioned. It involves raised nubs that the switch must transition over.

Boeing fuel control switch

A fuel control switch similar to that found on Boeing 787s, showing that the switch must transition over raised bumps

That 2018 bulletin warned about potential “disengagement” of the locking feature, which could allow the switches to “be moved between the two positions without lifting”, potentially causing “inadvertent” engine shutdown.

Though the FAA recommended inspections, its bulletin concluded that issue was “not an unsafe condition that would warrant airworthiness directive”.

The FAA reiterated that position in its 11 July CANIC, saying the fuel control switch design does not pose “an unsafe condition”.

Though the AAIB’s report cited the issue, it drew no link between it and the crash