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and at the maintenance shop they installed the wrong plug and the cables were switched too I think.
1 twisted pair colours "opposite" to the rest of the connector an a batch of aircraft that the drawing update never got to on the production line..........:*:* They changed a whole connector insert for a bent pin on large multi pin rack connector, most leckys I know would have quizzed that one straight away due to the amount of disturbance even one for one...:* |
Engine3firehandle....
As long ago as 1992 it was SOP on the Airbus family to carry out full/free control movement and visually check that the control surfaces were moving in the correct sense on the FCTRL system page. Additionally on reaching each extreme of movement you waited 2 seconds for an ECAM warning of control malfunction. This was (and still is) carried out by both pilots in turn. As the handling pilot's sidestick was cross wired no ECAM warning would have sounded because data to the SDAC indicated that control movement was as commanded. The non-handling pilot in the Lufthansa incident could not possibly have monitored the control check properly as otherwise he would have seen the ailerons move in the incorrect sense. OK we are all human.... but increasingly now we are the last line of defence. If we get it wrong then we all die. |
Additionally on reaching each extreme of movement you waited 2 seconds for an ECAM warning of control malfunction I do not believe the 2s is required any more - we certainly don't emphaise it although I do it - change in software or something... NoD |
There was indeed a flight warning computer software change that sped up the system's ability to sense a control malfunction during the control check.
And before anyone lays it on the LH F/O, who was indeed the last line of defense in a system where many errors led up to the incident, you might want to ask yourself if you have ever looked at something and saw you expected to see, only to later realize that what you saw and what was really there were two different things. It's called "expectation bias", and it's been cited as a factor in several incidents and accidents. Prior to the LH incident, none of us who flew Airbus FBW aircraft were aware that any such problem was possible, but our senses were certainly piqued once we learned what had happened that day. |
BEA press release
Bienvenue sur le site du Bureau d'Enquêtes et d'Analyses
summary " data from CVR and FDR have been recovered at Honeywell in Seattle in presence of BEA and NTSB people. BEA is now going to exploit these data" Hope we will soon have news now. |
Originally Posted by NoD
I believe this came in after the Excalibur A320 incident @ LGW.
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BEA indicates this day, that the FDR datas have been retrieved by honeywell, and will now be analyzed. We should have some sort of answer very soon, and be able to stop all this speculation.
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So Belgique wasn't far out when he said at this link:
Looking good for undetected/unrecognized flap asymmetry upon extension for the approach? . How does the A320's systems cope with that (or for that matter, with asymm spoiler extension - upon spoilers being armed?) |
From RTFM link on "A320 handling difficulties following flap replacement"
At first the FO attributed the undemanded roll to crosswind and applied left sidestick but the aircraft continued to roll to the right and he had to apply full left sidestick to contain the undemanded roll. Meanwhile the commander uttered words to the effect that the FO should take action to correct the situation |
Brace yourselves for a FACTUAL post:
"In agreement with the Perpignan State Prosecutor, the BEA is releasing the following information on the accident that occurred on 27 November 2008 to the Airbus A320 registered D-AXLA. After the recovery of the flight recorders, it appeared that the data that could have been recorded could be downloaded only by using the facilities available at Honeywell, the manufacturer of these recorders, in Seattle (United States). The work undertaken in the recorder manufacturer's laboratories, with the participation of specialized investigators from the BEA and the NTSB, did in fact make it possible to recover the data from memory cards of the two recorders, the Cockpit Voice Recorder (CVR) and the Flight Data Recorder (FDR). All the work was undertaken in the presence of a senior French Police officer, in the context of an International Judicial Commission. The BEA will now begin analyzing this data, in parallel with the operations undertaken within the framework of the judicial inquiry." "In agreement with the Perpignan State Prosecutor, the BEA is releasing the following information on the accident that occurred on 27 November 2008 to the Airbus A320 registered D-AXLA. After the recovery of the flight recorders, it appeared that the data that could have been recorded could be downloaded only by using the facilities available at Honeywell, the manufacturer of these recorders, in Seattle (United States). The work undertaken in the recorder manufacturer's laboratories, with the participation of specialized investigators from the BEA and the NTSB, did in fact make it possible to recover the data from memory cards of the two recorders, the Cockpit Voice Recorder (CVR) and the Flight Data Recorder (FDR). All the work was undertaken in the presence of a senior French Police officer, in the context of an International Judicial Commission. The BEA will now begin analyzing this data, in parallel with the operations undertaken within the framework of the judicial inquiry." |
Werner,
I have PM`d you with a much fuller explaination of my position. The ECAM warning you talk about came from the Excalibar post maintenance spoiler incident where the spoilers on one wing were de-activated full up. Again, I say that a conscientious comfirmation of the actual displayed flight control surface deflection related to the sidestick movement will always correctly detect any faults. (indeed I once taxyied back in on a B747 when an outboard aileron failed to unlock - as displayed by the SPI) The faulty CM1 sidestick could only have displayed a) fully correct deflection b) full/partial incorrect deflection or c) no deflection. In other words a two in three chance of detecting the fault. These check must be done slowly and methodically to avoid `seeing what we expect to see`!! However you try to `spin` it - the essential control check was not satisfactorily carried out. |
After the recovery of the flight recorders, it appeared that the data that could have been recorded could be downloaded only by using the facilities available at Honeywell, the manufacturer of these recorders, in Seattle (United States) Physical damage ? Data corruption ? Really mysterious... |
Originally Posted by atakacs
Interesting info but doesn't tell why the admittedly well equipped BEA could not read those recorders from a fairly modern Airbus...
Physical damage ? Data corruption ? Really mysterious... Trust me, there's nothing mysterious about it. Once you have to go into the innards, you really go on tiptoe. The BEA press release said they had to read the memory boards. Sounds already as if they were lucky and did not have to try and read each chip.... Now, one) reading a memory board from a specific manufacturer needs a fair amount of hardware and software,which BEA would not necessarily have in place, and two) the bits and bytes from the memories are meaningless, until you have the full decoding software to translate them to the actual parameters being recorded, which can also vary from manufacturer to manufacturer. CJ |
ChristiaanJ
Can you really believe that the BEA doesn't have the necessary equipment to read the recorders of an A320, whoever being the hardware manufacturer (and Honeywell is certainly not the most exotic supplier of such devices...) ?! If it's really the case they can very well close shop and subcontract all their investigations to the NTSB.... Something fairly unusual happened here. I guess it will be reported eventually but in the meantime I'm still bemused. |
Does anyone have an idea about how much the necessary hardware and software to read every possible manufacturer´s black boxes would cost? Why would the French board invest in something which will most likely be needed once in, say, 20 years when they know the manufacturer has the equipment in place and also people who have been trained to use it? Furthermore, depending on the extent of damage to the boxes, it may be safer to send them to the manufacturer anyway?
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atakacs,
Are you an avionics/electronics engineer? If you are, I can't see your point. It's not the BEAs job to keep a huge store of breakout boxes, schematic diagrams, test specifications, ATE software, etc. etc. for every single board used in every single FDR in every single aircraft flying in French airspace.... If you are not, Finn47 already has answered most of your question. CJ |
Does anyone have an idea about how much the necessary hardware and software to read every possible manufacturer´s black boxes would cost? So how many manufacturers are actually supplying Airbus for the A320 FDR ? I might be wrong (I am an electronic engineer but not in that field) but I would be very surprised that there would be more than half a dozen. Would it be a Tupolev or some exotic airframe the story would be obviously different, but the A320 ?! Why would the French board invest in something which will most likely be needed once in, say, 20 years when they know the manufacturer has the equipment in place and also people who have been trained to use it? Anyway we should hear more factual information shortly. |
This device reads all Honeywell solid state recorders. I would bet other manufacturers offer similar data access devices for airlines to use.
Recorder Test and Ground Support Equipment (GSE) - Honeywell Aerospace |
Come on guys... there's a lot of difference between reading a FDR / CVR in "normal circs", and one (as here) apparently damaged / not readable.
The manufacturer will no doubt have tools to dismantle / read the memory chips way beyond the average "reader" which seems, in this case, not to have worked. Unless of course, for post maint / non public transport / whatever reasons they were not functioning at all on this flight :{ NoD |
Nigel,
It would seem it was working, since they now have downloaded the basic contents at Honeywell's. But otherwise you're right. Once you're dealing with an FDR that has been through a water impact and picked up from 40m under water, it's somewhat rare to be able to just plug it in and read it out.... The BEA is highly competent.... but they're not feckin' magicians. CJ |
Originally Posted by md80fanatic
This device reads all Honeywell solid state recorders. I would bet other manufacturers offer similar data access devices for airlines to use.
<<See link in post>>Recorder Test and Ground Support Equipment (GSE) - Honeywell Aerospace FDRs, QARs and CVRs are basically ARINC standard, so as long as they are intact, there are no major problems in connecting to them and doing a read-out. But once the box is smashed up sufficiently for one to have to go inside, "all bets are off". I take it you've never seen what avionics boxes look like after a crash.... I have. CJ |
Now, one) reading a memory board from a specific manufacturer needs a fair amount of hardware and software,which BEA would not necessarily have in place, and two) the bits and bytes from the memories are meaningless, until you have the full decoding software to translate them to the actual parameters being recorded, which can also vary from manufacturer to manufacturer. (my own translation ...) Before reading any data, a phase of observation and risk assessment is carried out. It is necessary to isolate the component by unsoldering it. To limit the risk of data loss, temperature is monitored throughout the process. You can read the raw memory with a drive designed for the needs of the technical investigation. These exams require the use of tools developed specifically for the needs of BEA In case of damaged components, the avionics laboratory is able to extract the data down to the level of the chip |
The Wall Street Journal is reporting 'good news' in recovering information . . .
Air NZ black boxes uncover 'useful info' Two black boxes from the Air New Zealand Airbus which crashed off the French coast in November have given investigators some useful information. The Wall Street Journal reported investigators got some good news this week when the manufacturer of the aircraft's data recorder and cockpit voice recorder, known as the black boxes, retrieved useful data. Until now investigators had been stymied in their search for clues to what made the three-year-old, 150-seat Airbus A320 crash into the sea near Perpignan, off the southern coast of France on November 28. There was no mayday call from the two German pilots doing the assessment flight before the aircraft was returned to Air New Zealand after being leased to the German company XL Airways. Both pilots and five New Zealanders on board were killed. The bodies of six victims had been recovered but one was still missing. Most of the wreckage still lay in about 40 metres of water and New Zealand authorities said earlier this week if enough useful information was retrieved from the black boxes to determine the cause of the crash, French authorities may leave most of the wreckage where it lay. The Wall Street Journal said the crash inquiry was being closely watched by the global aviation community because the twin-engine A320 was a workhorse of airlines around the globe. |
ChristiaanJ, my apologies if I wasn't clear. By posting the link I was not implying that something nefarious is occurring regarding this accident.
Only was trying to dispel the myth that accessing and working with these recorders is a daily occurrence, and not really a black art performed by a small handful of scientists. :) |
Due to extensive damage to the boxes, the only way to gain access to the data on the recorders in this case was to download it from the individual memory chips. That is a process that no investigating body, including the mighty NTSB, can do on their own. That is the one and only reason that the recorders were sent to Honeywell, where they have the necessary tools and expertise.
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Due to extensive damage to the boxes, the only way to gain access to the data on the recorders in this case was to download it from the individual memory chips |
There are generally two reasons for recorders to be damaged; severe inertial/impact forces or post crash fire. I'm pretty sure that we can rule out fire here.
Last atakcs' post reminds me of "enlightened" passengers' question: "If the black boxes are made of crash-proof material, why then the all aeroplane is made of the same material to make the crashes survivable?" This (and number of people killed in road accidents) shows that there are a lot of folks out there unable to grasp folowing concepts: 1) inertia 2) kinetic energy effects (e.g. damage to property and bodily harm) are not proportional to speed but to speed squared. Ever since two days after the crash, there was not one new bit of reliable and useful information about the accident. However, the little that is known makes simple crosswired stick extremely unlikely because 1) it is mandatory to check that ECAM indication of the movement of the flight controls corresponds with sidestick deflection before every normal flight, let alone post-maintenance test flight 2) it is unlikely that handling of the aeroplane would be checked from one side only during test flight 3) even if at 3500 ft there was first handover of the controls, crosswired sidestick doesn't make A320 leave normal law, there would be plenty of altitude to recover, even if pitch/bank limits were reached. New theory, ore even better, new facts, please. |
Last atakcs' post reminds me of "enlightened" passengers' question |
Could the following be of interest? :
FR Doc E8-29182 |
Due to extensive damage to the boxes, the only way to gain access to the data on the recorders in this case was to download it from the individual memory chips. That is a process that no investigating body, including the mighty NTSB, can do on their own. That is the one and only reason that the recorders were sent to Honeywell, where they have the necessary tools and expertise And a black box can take a LOT ! http://i65.servimg.com/u/f65/11/75/17/84/nz_01710.gif http://i65.servimg.com/u/f65/11/75/17/84/nz_01810.gif |
"BEA has all that expertise"
Not according to the BEA, they don't. They're saying that only Honeywell has the means to extract the data: "Après la récupération des enregistreurs de vol, il était apparu que les données susceptibles d'avoir été enregistrées ne pourraient être extraites qu'en utilisant des moyens disponibles uniquement chez Honeywell, constructeur de ces enregistreurs, à Seattle (Etats-Unis)." (BEA statement, 8 January) |
That's what they write on January 8, but then how do we call what's on their website ... publicité mensongère ?
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Originally Posted by CONF iture
That's what they write on January 8, but then how do we call what's on their website ... publicité mensongère ?
They have equipment that can get at the contents of individual chips. (the manufacturer would not have such equipment, since they would have no need for it). Once they actually get the raw bits and bytes, they work very closely with the manufacturer to actually decode and analyse the data. md80fanatic posted a link to the Honeywell "Recorder Test and Ground Support Equipment (GSE)" and said "This device reads all Honeywell solid state recorders. I would bet other manufacturers offer similar data access devices for airlines to use." Sure. It's a big laptop with extra interface boards. It's made to talk to an intact FDR..... I've designed and developed very similar equipment (used for FDR development and acceptance testing), so I know what's in it. CJ |
meanwhile the delayed preliminary is due out today or so, no?
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ChristiaanJ, I take your point.
Nevertheless, it was not a big deal to get those data, Seattle got them in a few days. Now, who is going to believe that Airbus has been patiently waiting for the French criminal investigation to give their OK to have a chance to know what happened ? Do you imagine if tomorrow morning, a NWA 320 crash out of Minneapolis ... ? Things don't add up here, but as seen on other threads, people don't question. |
Originally Posted by CONF iture
ChristiaanJ, I take your point.
Nevertheless, it was not a big deal to get those data, Seattle got them in a few days. From snippets here and there, it would seem the memory boards were still intact. Since it was Honeywell who manufactured them, they would be the people with all the breakouts and test equipment right there on the lab shelves, to test and read out those exact boards. So in my opinion, the BEA made the right decision not to barge in where even engineers fear to tread (to coin a phrase...). Now, who is going to believe that Airbus has been patiently waiting for the French criminal investigation to give their OK to have a chance to know what happened ? But they have enough unforunate experiences with French "criminal investigations" (judicial enquiries) involving flight recorders (with Habsheim and St. Odile at the head of the list), that they'd rather wait a few days until heads had cleared after the Xmas and New Year holidays, instead of trying to apply pressure, which wouldn't have solved anything anyway. "The mills of French judicial enquiries (not necessarily criminal) tend to grind extremely slowly". I don't know if you follow French news, but Sarkozy has just announced he wants to get rid of the "juge d'instruction", and replace her/him by a "juge de l'instruction". You have to know French to get the point, but the essential difference is that the "juge" will no longer be the "omnipotent pacha" during the enquiry ("instruction") but simply one of the representatives of the judicial system. CJ |
The mills of French judicial enquiries (not necessarily criminal) tend to grind extremely slowly". if tomorrow morning, a NWA 320 crash out of Minneapolis ... ? |
Sometimes a CVR has to be taken to the manufacturer to get the data as in this case.
"While attempting to download the information from the CVR, it was found that the recorded data had been erased. The CVR was taken to the manufacturer’s facility in Seattle and the data was successfully recovered. The CVR showed that 31 seconds before the end of the recording the CVR was powered down; the time recorded on the CVR from the aircraft UTC clock was 21:33:39. The CVR was then powered up again at 21:49:36, erased twice and then powered down six seconds after the second erase command was completed." http://www.tsb.gc.ca/eng/rapports-re...8/a04o0188.pdf So for anyone who thinks erasing a CVR might get rid of the evidence, it is still retrievable. |
Sometimes a CVR has to be taken to the manufacturer to get the data as in this case. "While attempting to download the information from the CVR, it was found that the recorded data had been erased. The CVR was taken to the manufacturer’s facility in Seattle and the data was successfully recovered. The CVR showed that 31 seconds before the end of the recording the CVR was powered down; the time recorded on the CVR from the aircraft UTC clock was 21:33:39. The CVR was then powered up again at 21:49:36, erased twice and then powered down six seconds after the second erase command was completed." Erreur 404 / Error 404 So for anyone who thinks erasing a CVR might get rid of the evidence, it is still retrievable. Also I would rather work on recovering an erased CVR than one that has been written over with conversations. |
CJ:
You need to make up your mind. In post # 403, you said, They (the BEA) have equipment that can get at the contents of individual chips. (the manufacturer would not have such equipment, since they would have no need for it). Since it was Honeywell who manufactured them, they would be the people with all the breakouts and test equipment right there on the lab shelves, to test and read out those exact boards. |
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