thats an understatement! I can hardly bear to visit this thread. I’ve never seen such bollocks!!![ Guys and girls that fly helicopters, or are learning to fly helicopters, will be able to discern the valuable posts from the obvious "b*****ks" or at least ask questions if they require clarification. Accident debates often offend somebody or other, it is the nature of things...but in all matters aviation it is important - nay, vital - that they continue. Hopefully, soberly, respectfully and advisedly. But it's the internet and sometimes that's not always going to be the case. As for journalists stepping by and picking up and printing horse manure...seriously who the heck cares? Surely all educated people know that a large percentage of what is printed these days in newspapers is agenda-led, headline-grabbing codswallop, irrespective of the subject matter. Sure it will influence Joe Public, but that's going to happen regardless of anything that is posted on here. |
Dear all, I am SLF but have been flown by experts in such aircraft and have a bit of experience in crash reconstruction. My I start with condolences to all in this tragedy? I have studied the sad Sun video closely, and I am struck by the appearance of the tail anticollision light as the aircraft rotates. There are two clear images of this. In the first, at almost exactly the 1 minute mark, the image is blurred by the spinning tail rotor.
In the second, about 2 seconds later, the tail anticollision light is small and apparently not blurred. Would a suggestion that this was now due to the rate of rotation of the tail rotor having reduced be reasonable? Regrettably I cannot post my screen captured images as the forum thinks I am trying to post URLs. |
Originally Posted by BFM
(Post 10298277)
...and I am struck by the appearance of the tail anticollision light as the aircraft rotates..
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Originally Posted by The Old Fat One
(Post 10298247)
..As for journalists stepping by and picking up and printing horse manure...seriously who the heck cares? Surely all educated people know that a large percentage of what is printed these days in newspapers is agenda-led, headline-grabbing codswallop, irrespective of the subject matter. Sure it will influence Joe Public, but that's going to happen regardless of anything that is posted on here.
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For those interested in survivability in a similar accident, I refer to this report into a photo flight where and EC130 from a hover, spun from 220 feet and crashed into sand dunes. Even with the EC crash absorbing seats 3 passengers and pilot perished. There was no fire. The report goes into detail regarding vertical G forces.
https://www.onderzoeksraad.nl/en/ond...725A7A690814F2 The crash was recorded on video from a distance so the rate of descent is accurate. Note that pictures of the wreck show the cabin forward of the seats missing, it appears this was done to remove one of the passengers whose limb was trapped rather than being sliced by rotor impact. Mjb |
Originally Posted by Torquetalk
(Post 10298233)
Post 387 above addresses this |
The result of a failed engine would not be as per that seen in the videos. A poor igniter can result in fuel vapour being emitted from the exhaust during the start sequence of many turbine engines - obviously there is more than one igniter.
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Having viewed all the videos, photos and links on this thread, I am unable to see any obvious external faults with the aircraft or its handling until the turn is initiated while in an effective hover at the top of the ascent. Given that the engines would have been operating at or close to maximum power in sustaining the hover, is it possible that the effectiveness of the tail rotor was critically reduced just as something distracted the pilot just for a second while the rotation rate increased? Is there a preferred turn direction? Would the aircraft have survived if the turn had been made in the opposite direction? Is the tail rotor authority sufficient to arrest a spin in either direction while in a high hover? It seems to me that with no forward velocity, once the aircraft started spinning, there was simply no way to go other than straight down. |
White “smoke” on start: I’m surprised by the comments on here. White “smoke” on start is fairly normal and is fuel sprayed out before the igniters have lit it. Seen it often. |
Originally Posted by gulliBell
(Post 10298365)
I remain to be convinced by that explanation....I've never seen a PWC engine do that before, and I've seen many many starts over many years (but not on this particular model engine). During the start cycle of this engine do the igniters energize as soon as the starter is engaged? I suspect so, so if that was fuel being blown out the engine I'd expect it to be like a flame thrower and not smoke like. To me that looks like oil smoke, from oil that has leaked past a seal that shouldn't. And leaking seals can turn into bad bearings. And bad bearings can turn into failed engines.
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One thing that puzzles me here (and has done in the past)... WHY are the throttles placed in the ceiling, essentially unreachable if you're already in the middle of sorting out an emergency that needs hands on the collective and cyclic? It would make me horribly uncomfortable if I couldn't control the engines at the same time as everything else. The "motorcycle" throttle on the collective just seems such an obviously good idea. I can see a practical problem for a twin (like, needing two throttles) but I'm sure that's not beyond the imagination of man.
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Originally Posted by n5296s
(Post 10298387)
One thing that puzzles me here (and has done in the past)... WHY are the throttles placed in the ceiling, essentially unreachable if you're already in the middle of sorting out an emergency that needs hands on the collective and cyclic? It would make me horribly uncomfortable if I couldn't control the engines at the same time as everything else. The "motorcycle" throttle on the collective just seems such an obviously good idea. I can see a practical problem for a twin (like, needing two throttles) but I'm sure that's not beyond the imagination of man.
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Originally Posted by n5296s
(Post 10298387)
...WHY are the throttles placed in the ceiling...
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Originally Posted by 212man
(Post 10298129)
thats an understatement! I can hardly bear to visit this thread. I’ve never seen such bollocks!!!
I don't know that many professionals in the industry, but I do know that anyone with an opinion worth listening too wouldn't post anything on here. |
My thoughts keep reluctantly focussing on sabotage. Swift removal of TRGB drain plug? all billionaires cultivate serious enemies. |
Could the aircraft have responded in the manner seen on the video as a result of pilot incapacitation?
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Originally Posted by Arkroyal
(Post 10298680)
My thoughts keep reluctantly focussing on sabotage. Swift removal of TRGB drain plug? all billionaires cultivate serious enemies. I hope the police know everyone's name who had access to the aircraft after it arrived at the stadium. I hope the investigators would recognise the signs of noxious products in the cabin. |
Originally Posted by flyems
(Post 10298732)
Could the aircraft have responded in the manner seen on the video as a result of pilot incapacitation?
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Originally Posted by flyems
(Post 10298732)
Could the aircraft have responded in the manner seen on the video as a result of pilot incapacitation?
Originally Posted by Arkroyal
(Post 10298680)
My thoughts keep reluctantly focussing on sabotage. Swift removal of TRGB drain plug?
all billionaires cultivate serious enemies. Unlikely that incapacitation could cause a reaction like that. and the coroner in the Bournmouth crash seemed to be dreamimg. The ATC tapes that recorded the pilot talking to himself, trying to talk himself out of the loss of control made things fairly clear as to what happened. In fact I belive the ATCO dealing with the flight didn't work for some time due to word she heard. SND |
Originally Posted by gulliBell
(Post 10298365)
I remain to be convinced by that explanation....I've never seen a PWC engine do that before, and I've seen many many starts over many years (but not on this particular model engine). During the start cycle of this engine do the igniters energize as soon as the starter is engaged? I suspect so, so if that was fuel being blown out the engine I'd expect it to be like a flame thrower and not smoke like. To me that looks like oil smoke, from oil that has leaked past a seal that shouldn't. And leaking seals can turn into bad bearings. And bad bearings can turn into failed engines.
What we can deduce is that an engine failure would not normally result in a fully developed torque induced spin as in this case; however I am far more experienced as an engineer than I am as a pilot, so if someone with more flying experience wants to point out why an engine failure would result in a spin, please do so and educate me. A day without learning is a day wasted after all!! |
Originally Posted by Arkroyal
(Post 10298680)
My thoughts keep reluctantly focussing on sabotage. Swift removal of TRGB drain plug? all billionaires cultivate serious enemies. I have recently flown frequently as a helicopter passenger on numerous occasions in both Switzerland and Australia and the pilots would not land if they could not get a good run for take off without high obstruction in front. |
Originally Posted by anchorhold
(Post 10298742)
Flyems states.........Could the aircraft have responded in the manner seen on the video as a result of pilot incapacitation?
I think that has to be a possibility when faced with an aircraft with less than 300 hrs flight time and a single crew pilot aged 53. This is why the medical requires more frequent ECGs with age. Having said that, an ECG pass, doesn't mean you are not going to be incapacitated by a stroke or heart attack at anytime. That is why it is always better to have two qualified and type rated pilots, which is the case with the queens flight. It is far from my place to suggest this type of scenario could be linked to the accident, and in no way would I speculate as to the cause as simply put, I do not have the knowledge required to comment. What I am saying however is that certain conditions can cause an almost instantaneous loss of consciousness, irrespective of how fit or healthy the individual, and no amount of medical testing can rule out such possibilities. What I can also do is describe the sensation when this loss of consciousness occurs, with tunnel vision being the first stage, followed very briefly by intense dizziness and confusion - during such a time, you have very little capacity to action any rational movements or thoughts, particularly the first time, as it is pure confusion. I do hope that the above wasn't the case, but whatever was the cause, it is a tragic and saddening accident. |
Originally Posted by tbtstt
(Post 10298623)
It's long been like that on pprune. These crash threads are useful for finding links to external sites, but the conjecture ranges from laughable to infuriating and, in most cases, just demonstrates a spectacular lack of knowledge.
I don't know that many professionals in the industry, but I do know that anyone with an opinion worth listening too wouldn't post anything on here. TBTSST, I do not know what you do, but many on this thread carry out these VTOL departures each time we fly, EMS, HEMS., Police and the Corporate sector. The reason why we have a lot of interest here, is that this failure, in this phase of flight, is theoretically ignored by certification. As such there is very little guidance in Flight Manuals on how to deal with it. There is a reason for that.....if you think about the outcome of this event! In the end, its up to you if you choose to take part in the discussion or not. However, posing sanctimonious passive aggressive statements, like yours above, means to me you have no value to add at all. So why bother yourself to even visit the thread. |
Originally Posted by DOUBLE BOGEY
(Post 10298786)
That would make you wrong. In our industry we have very little opportunity, as professionals and PPLs alike, to learn from each other. PPRUNE provides that forum. Yes some people can sometimes seems spectacularly stupid (me some of the time) and some of us love a good argument. That's "A" Type extroverts for you...
Originally Posted by DOUBLE BOGEY
(Post 10298786)
...But taken as a whole PPRUNE offers an opportunity to learn from each other especially when an accident like this happens.
Conversation on incidents such as this between knowledgeable individuals is excellent and absolutely worthwhile, but some of the conclusions reached by supposed professionals in threads like this - while in possession of just a handful of facts - are astonishingly reckless. Based on the available evidence I have my own theory as to what has happened but, until the full story is told, I wouldn't consider making any definite conclusions and I absolutely wouldn't start point fingers at any particular party (and, even with a cursory glance, I can see that has already occurred numerous times throughout this thread). It certainly wasn't my intention to appear sanctimonious but it is no secret that the media clearly view this forum and threads like this just fuel the nonsense that we see reported on these incidents in the press. |
Originally Posted by Mike78
(Post 10298784)
I do hope that the above wasn't the case, but whatever was the cause, it is a tragic and saddening accident. That said, I doubt very much if incapacitation will be found to be causal or implicated in this accident. Not only because it is highly unlikely in itself, but also because the pilot was sat next to another person, who although given as a passenger, would almost certainly have been able intervene given their experience and stop matters getting out of hand. |
The problem is this:
Originally Posted by tbtstt
(Post 10298623)
I don't know that many professionals in the industry, but I do know that anyone with an opinion worth listening too wouldn't post anything on here.
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I know that the weather at the time would appear to contradict the formation of a vortex ring, but could the explanation be as simple as that? High power vertical slightly reversed climb followed by a turn and drift into a vortex of descending air? |
There are quite a few very highly experienced and imminently qualified folks who attend these pages and make very good contributions.
On the other hand there are some who think themselves all of that....but who indict that assumption with nearly every post they make. The key, as in all things in life, is to be able to pick the good from the bad. Most folks are able to do that but that ability seems to elude those who just do not get it and continue to post their lame views, ideas, concepts, and boasts of experience. That at least makes it easy to begin the sorting of the good from the bad. I may not always agree with the what is being posted by the genuinely qualified but then we all have our own views of matters as this flying thing we share is not an exact science that can be firmly framed in simple text. Those differences tend to be based upon our individual life experiences flying helicopters, a notion that makes very good sense when considered. As this is a Forum that includes people from all over the World, most using their second language to communicate, there will sometimes be difficulties in communicating what is intended as compared to what was understood. Every conversation via Text suffers from such issues and Rotorheads is no different in that regard. If you post here.....be prepared to corroborate what you say as very often you shall be challenged to do so. If you object to that....please do not post for you do, at some point your feelings shall certainly be hurt. |
Ruling Out Pilot Incapacitation
Both Eric & Izabela (the pilots), followed a plant based diet and regularly exercised. They were healthier than most pilots, so I rule incapacitation out of the equation. Sabotage, something (a bird or drone) hitting the tail rotor or mechanical malfunction is the cause. We will find out soon.
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It has been a few years since I flew heavy helicopters but fundamentally the loss of TR control 200-500 feet above the stadium was not survivable.
The AAIB will want to quickly establish the '4 corners' of the accident to confirm that all the components of the aircraft are present at the crash scene. One video shot seems to suggest that a component flew away from the aircraft with high energy immediately before control was lost, the only components posessing such energy would have been a MR pocket (or two) or a TR blade. The fact that the aircraft immediately lost yaw control indicates it may have been a TR blade.... Crash site pictures indicate 2 TR blades present but one is half missing, you could argue it had been consumed in the post crash fire but the edges appear jagged as if it had been torn apart rather than burnt. The AW 169 has an impeccable safety record with no history of TR blade mishaps or other TR drive or contol problems. So why in this case? TR blades are stressed in construction so as to survive a minor impact from a birdstrike and still perform their role. In this day and age modern helicopters do not crash because birds fly through the tail rotors. In-service failure due to substandard manufacturing is a possibility but frankly unlikely. It is much more likely that a foreign object struck the tailrotor causing sufficient damage to cause blade failure and separation.... But caused by what? The surrounding area several hundred yards in every direction will be thoroughly searched for debris.... who knows what else might be found? Might we be looking at the first fatal aviation accident due to an aircraft colliding with a drone? |
What does a "Plant based Diet" have to do with the question of "Sudden Incapacitation"?
I also question the suggestion the "Second Pilot" could have handled the situation if it had occurred......just how do we know that? |
Originally Posted by Magplug
(Post 10298880)
It has been a few years since I flew heavy helicopters but fundamentally the loss of TR control 200-500 feet above the stadium was not survivable.
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In general....I would agree with MagPlug about the differences between small and large Helicopters when we talk of Tail Rotor failures.
The forces generated by the Rotor systems on large aircraft create a real design problem for the Engineers designing the aircraft. How much Tail Fin area does it take to facilitate adequate weather vane effect for those large helicopters? My trusty old Huey did pretty well.....the Huey Cobra derived from the Huey.....did not. I would bet my other trusty steed, the Sikorsky S-58T, was far better than the Sikorsky S-61 or CH-53. As in some other things in life....Size does matter along with technique. |
Originally Posted by SASless
(Post 10298885)
What does a "Plant based Diet" have to do with the question of "Sudden Incapacitation"?
I also question the suggestion the "Second Pilot" could have handled the situation if it had occurred......just how do we know that? |
Originally Posted by SASless
(Post 10298885)
What does a "Plant based Diet" have to do with the question of "Sudden Incapacitation"?
I also question the suggestion the "Second Pilot" could have handled the situation if it had occurred......just how do we know that? |
Originally Posted by Torquetalk
(Post 10298937)
We don’t. But were “passive” incapacitation or annnounced incapacitation involved, I think it’s reasonable to assume that a pilot of her experience would be able to apply control inputs to maintain a safe flight condition. |
So speculation as ever but given what has been observed so far it seems most likely that:
a) The aircraft was high enough at the apparent point of failure to avoid hitting the TR on any part of the stadium or other fixed object b) Therefore the failure was likely caused either by something else airborne hitting it - or some sort of separate mechanical failure Assuming the mechanical failure option, (in the absence of any clear evidence of another airborne object) one thing that still puzzles me is why the pilot chose to lift to such an apparently unnecessary height before attempting to transition into forward flight. Could it be that he was aware of some sort of anomaly on the lift out that made him want to gain extra altitude to have the option of an autorotation away from the confined space of the take-off site? If there was a problem near the ground he would presumably have just put it straight back down - so whatever it was presumably occurred somewhere between the height at which he would normally have transitioned (200ft?) and the height he eventually reached (1000ft?). To give this theory any validity, there would have to be some sort of anomaly warning (sound/vibration/warning system?) that would encourage the pilot to believe that continuing to gain height enough to attempt a safe autorotation was his best (or only) option. What might this have been? |
At this point....without an official determination of what hellcopter flying skills experience, training, or knowledge the "Passenger Pilot" had at the time of the Accident....and without any information of "incapacitation" being an issue at all..... I would suggest we have not reached any level of being able to make an "assumption" and must limit the qualification of any such suggestion as being purely baseless pontification.
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Originally Posted by SASless
(Post 10298975)
At this point....without an official determination of what hellcopter flying skills experience, training, or knowledge the "Passenger Pilot" had at the time of the Accident....and without any information of "incapacitation" being an issue at all..... I would suggest we have not reached any level of being able to make an "assumption" and must limit the qualification of any such suggestion as being purely baseless pontification.
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Originally Posted by asdf1234
(Post 10298970)
It's my understanding that the passenger pilot had a fixed wing licence and not a rotary wing licence .if that is the case, and please correct me if I'm wrong, how would her fixed wing experience help her in a rotary wing environment?
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