Paphitis,
Thank you once again for your expert opinion on Flight AF 447.
It could well have happened as you have written above and we will not now the facts until all the information needed to make that determination if and when the Flight Recorder (FDR) and the Cockpit Voice Recorder (CVR) are found.
You are quite correct. However, there is a lot of industry speculation which you won't read about in the media.
From all the very early news reports on this crash, the weather was the main suspect, but in what they wrote, it was not very credible for me to accept it as facts, since their explanation was very elementary to say the least. Take a look at these reports.
The severe weather conditions encountered by AF447 was a major contributor for this accident. There is some speculation of
structural failure of Yaw Dampers, and the Hydraulic Actuators of the
Horizontal Stabiliser and
Rudder, because the aircraft encountered severe turbulence and exceeded its wing loading limit of 1.5g. These are made from
carbon-fibre composite materials.
The cause of the crash will not be known until the black boxes are recovered — which could take days or weeks. But weather and aviation experts are focusing on the possibility of a collision with a brutal storm that sent winds of 100 mph (160 km/h) straight into the airliner's path.
"The airplane was flying at 500 mph (800 km/h) northeast and the air is coming at them at 100 mph," said AccuWeather.com senior meteorologist Henry Margusity. "That probably started the process that ended up in some catastrophic failure of the airplane."
http://news.yahoo.com/s/ap/20090603/ap_ ... l_plane_78 [/quote]
The above news article is the most ridiculous thing I have read.
Winds are not a factor at all. At altitudes greater than 25,000 feet, aircraft encounter Jet streams or strong winds, up to 150kts. I have seen jet streams as strong as 180 knots. These winds cause absolutely no stress on the airframe, and quite often, we will climb into these jet streams, if it gives us a good tailwind. This saves flight time and fuel. If we are encountering a Jet stream head on, we will descend to a lower level, where winds are not so high, so that we don't get the full brunt of the headwind. So Jet stream winds are really good if it translates to a Tailwind, but are bad if they translate to a Headwind.
This is what I thought of at the time I read the above;
"Reading the above section from a news article on Air France Flt 447 that crashed into the Atlantic last Sunday, more and more I'm beginning to get the feeling that the media and Air France is giving us a "snow job" in trying to keep us in the dark as to what may have happened, because the only scenario they are focusing on more than anything else, is the weather, which so far for me, it's the least cause of the loss of Flt 447."
The media is focusing on the weather because so far this is the only
verifiable element as to the cause of this accident.
Do not concern yourself with Air France too much. There is speculation that the Airbus A330/A340/A380 have some
critical design faults which Airbus are desperately trying to cover up and issue an Air Directive to operators about some urgent maintenance and modifications.
The Airbus A330/A340/A380 are constructed from cast aluminium and carbon fibre composites (plastic). The Horizontal Stabiliser, Yaw Dampers, Rudder, Ailerons, and hydraulic Actuator Pins are carbon-fibre plastic. This material, after many cycles is known to become very brittle and can endure much less stress than the aluminium designs.
The speculation within the industry is that AF447 suffered catastrophic structural failure when encountering severe turbulence and wing loading g-force. In other words, the Horizontal Stabiliser just broke away. The aircraft then had absolutely no pitch control and would have plunged into the ocean.
So Airbus Industries would be a little concerned about this right now. Because if an aviation expert is brave enough to tell the media that AF in all likelihood went down due to a design fault in the Actuator Pins of the Horizontal Stabiliser and that these Pins failed because they are made from carbon-fibre which becomes brittle and shatters under fatigue, then Airbus will go bust and not only. The whole Airbus A330/A340/A380 fleet will be grounded. Airlines that have all Airbus fleets like Cyprus Airways will also go under overnight. All airlines that have ordered the A330/A340/A380 will sue Airbus. It will be the end of all carbon-fibre aircraft. The Airbus A350 won't even get of the ground and neither will the B787 Dream-liner. Airbus could very well be destroyed.
Unfortunately, not many people would be willing to speak up about this right now, because there is no proof or solid evidence to back this up. Airbus would move very quickly and deny any reports that do come out and probably sue anyone who makes any defaming statements as to the integrity of carbon-fibre parts and how they might have contributed to this accident. This still does not prevent all the industry gossip, speculation and rumours from pilots, and engineers.
The only way we will ever find out is if the Cockpit Voice and Data Recorders are salvaged.
http://www.newscientist.com/article/mg2 ... uture.html
I was of course referring to lightning strikes on the aircraft and not on severe Turbulence that may have occurred as a result from bad weather. We have since the above report been getting more attention on the PITOT Tube as being the problem, which once again, leaves me with few more questions unanswered. Here are few puzzling questions that is bothering me.
The Pitot Tubes iced over resulting in ADR discrepancy. Please note that ADR discrepancy is listed as one of the faults on the AF447 ACARS transmission attached above. This also resulted in Traffic and Terrain Collision Avoidance System (TCAS) failure, as TCAS relies on speed data from the 3 ADRs. The aircraft's central nervous system also shut down. As you can see from the ACARS report, all the systems referred to in the above link just shut down including the auto pilot and auto throttle.
http://aviationtroubleshooting.blogspot ... arthe.html Once again here is a short list from the above attached ACARS readout.
34-22-25 - INDICATOR - ISIS (INTEGRATED STANDBY INSTRUMENT SYSTEM)
34-43-00 - TRAFFIC AND TERRAIN COLLISION AVOIDANCE SYSTEM
34-12-00 - AIR DATA/INERTIAL REFERENCE SYSTEM (ADIRS) ((ADIRU & CDU))
34-10-00 - AIR DATA/INERTIAL REFERENCE SYSTEM (ADIRS)
27-90-00 - ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)
22-83-34 - FMGEC (FLIGHT MANAGEMENT, GUIDANCE AND ENVELOPE COMPUTER)
22-62-00 - FLIGHT ENVELOPE COMPUTATION
22-30-00 – AUTOTHRUST
27-23-00 - RUDDER AND PEDAL TRAVEL LIMITING ACTUATION
27-93-00 - FLIGHT CONTROL PRIMARY COMPUTER (FCPC)
34-11-15 - PROBE – PITOT
27-93-34 - FCPC (FLIGHT CONTROL PRIMARY COMPUTER)
21-31-00 - PRESSURE CONTROL AND MONITORING
27-91-00 - OPERATIONAL CONFIGURATION (F/Ctl Altn law)
Three hours before Flt 447 took to the skies, another Air France took off from the same airport Paris bound and landed safely. Granted 3 hours is a long time and the weather could have changed in the meantime, but how about all the other aircraft using the airspace around where Flt 447 disappeared. Why have we not heard of any problems with these flights if the weather was so bad. I'm sure the South Atlantic route from South America to Europe is not as busy as the case is with the North American route to Europe, but surely there had to have been other pilots who had to had some involvement with the weather in this area, and yet, I have not heard anything. So the conclusion is, everyone made it OK through the proclaimed bad weather, except for Flt 447. This is very hard for me to accept if no other pilots had encountered such bad weather in this area. But as you have very clearly stated, the onboard weather radar would have been used to fly around the storm if it was that bad, so did they or did they not do this, and if so, what happened. Perhaps if they did turn back towards Brazil, now that path had also closed in, but we do not have that information on a 180° degree turn yet.
There was a
SIGMET Weather Report along AF447's route. I have this SIGMET report at home and I will post it for you next week. This SIGMET report, in all likelihood was reported by another preceding aircraft.
What this SIGMET report indicated was severe CB formations to the left and to the right of AF447's track. So the pilots probably decided to continue to Paris thinking that they would be able to negotiate these severe storms just like other aircraft did beforehand. A very reasonable decision under the circumstances. However, tropical CB cells have 3 stages. The Developing Stage, Mature Stage and the Dissipating Stage. The most dangerous is the Mature stage.
http://en.wikipedia.org/wiki/Thunderstorm The life cycle of a tropical storm is very small. There life cycle can be as short as 1-4 hours before they start dissipating but are extremely fierce in the Mature stage.
So for AF447, it was a case of being in the wrong place at the wrong time. If they arrived in the area as little as 3 hours earlier or later, they might have been OK. Even structural failure might not have occurred if AF447 did not encounter these freak weather conditions.
Lets talk about the Pitot tube problem. Yes there will be problems with the airspeed, altimeter and the vertical air speed indicators if the flow of air into it was restricted due to ice or other foreign objects. Lets just say that the pitot tube was iced up and the auto pilot reacted to it accordingly, increased speed or reduced speed depending on the exact problem. Surely experienced pilots would have noticed drastic change in the planes two engines RPM indicators as being either too high/low than normal RMS's during cruising at 35,000 ft.
The auto throttle had failed due to Air Data Reference (ADR) discrepancy. If anything, the autopilot would have reduced thrust, in order to achieve
Turbulence Penetration Speed. But if the ADR's are giving erratic readings, then the auto throttle doesn't know what to do and shuts itself down. ADR warning flags will appear as well as the Autopilot shutdown (AP OFF). TCAS will also fail as a result.
At this point, there is no method of ascertaining the aircraft's airspeed accurately, resulting in either possible overspeed or stall.
What about the GPS on board.? Not only they would give the pilot the aircrafts location, but also the ground speed of the aircraft. All the years I've flown on commercial airliners which had GPS screens for the passengers, which I keep on most of the time during the flight by the way, the most head/tail winds I've seen has been around 120-130 mph, therefore, if the GPS is showing 800 mph, I would be very surprised if the pilots accepted that being that they had an 300 mph tailwind, or GPS showing 200 mph, meaning that they had a headwind at 300 mph, since from experience and the speed they had before the crash, that they were flying at 500 mph as "true speed". I'm using the above numbers, because as reported lately, that if the pitot tube was faulty, then it would have caused the auto-pilot to increase/decrease speed depending what the problem was. I just can't accept, that experienced pilots did not see and did not compute in what the airspeed indicator was reading, what the engines rpm indicators were reading, and what the GPS indicators was reading, and yet, no action was taken by the pilots. I find this hard to believe.
You are also assuming that the GPS was functioning. GPS has an external antenna mounted on the fuselage, and if AF447 was struck by lighting, then it would have been fried just like all other VHF/UHF and HF comms.
Furthermore, all aircraft have a Turbulence Penetration Speed when encountering turbulence. This is to limit any undue stress on the fuselage and control surfaces. I do not know what the Turbulence Penetration Speed for the A330 is, but it could be as low as 350knots True Air Speed (TAS). In thunderstorms, it is feasible to expect wind gusts up to 180 knots, severe wind shear and microburst.
The GPS, if operational, will only give Ground Speed (GS) or the speed travelled over the ground. As you know this is different to the TAS as the tailwind component is added or the headwind component is subtracted. If the winds were as high as 180 knots, then the GS could either be very high or very low, dependant on whether it is a tailwind or headwind.
In this scenario, it is impossible for the pilots to even guess their TAS.
However, I do know that AF447's final reported speed was 447 knots. This reading may also be unreliable due to ADR discrepancy.
No radio transmission by the pilots for any emergency calls. Why not.? Surely they would have had time to transmit something, even to warn other pilots in the area. At least send a out a call giving the conditions if it's really that bad with the weather. There were 3 pilots aboard, but it is possible, one may have been out of the cockpit taking a short sleep in one of the crew berths, perhaps the captain.? No explanation which gives me concerns.
All pilots would have transmitted their position, and the weather conditions encountered when ops normal. If ops are not normal, all pilots will give a
MAYDAY call on emergency frequency 121.50 Mhz and Area Control probably on HF as the area is very remote and far away from control centres.
The fact that AF447 made no calls whatsoever, suggests that the aircraft was struck by lightning and lost ALL comms.
The automated transmission that you posted above (ACARS) stated that there was a problem with the electrical power system and loss of cabin pressure. This transmission had to have been sent before the plane hit the water, and yet, there was no transmission of anything by the pilots. Why not.?
Once again suggesting that AF447 had no comms. Lightning strike will do this.
OK, I've asked a lot of questions and it is very difficult to get into the head of the pilots to understand what they were doing/not doing, but the questions on the ACARS transmissions without the pilots transmitting anything leads me to believe that;
a) the aircraft broke up in the air by going too fast because the auto pilot just added full power if the airspeed indicators were giving false results to the auto pilot due to the pitot tube problems
The auto throttle would have been reducing power to achieve turbulence Penetration Speed. It may have tried to increase power only if the airspeed indication was far too low and risking a stall. But with ADR discrepancy it just shut down.
b) that the vertical stabilizer (tail) fell of the aircraft due to heavy turbulence which would have doomed the aircraft immediately. In 2001 American Airlines Flt 587, A300 lost it's vertical stabilizer right after take off causing the plane to crash killing all aboard and few on the ground, because the aircraft previously had some lateral forces applied on it's tail section in bad weather which had weakened the connecting point of the tail to the rest of the fuselage. Same may have happened here.??
The speculation is that the Horizontal Stabiliser might have fallen off.
This is why I was referring to
Structural Failure in my initial post.
There is a lot of talk about carbon-fibre parts and this has the potential to absolutely
destroy Airbus, and the A330/A340/A350/A380. The B787 dreamliner will not be immune to this either. So Airbus might be hoping that the Cockpit Voice and Data Recorders are never found.
If this turns out to be true, then the ramifications will turn the aviation industry inside out.
c) a bomb could have been the reason why everything happened so quickly that the pilots did not have a chance to make any transmission and the loss of electrical power and cabin pressure. It is very convenient that this aircraft went down soon after it left all radar covered areas. A bomb with a timer to go off at certain time would make the aircraft disappear, which would take much longer to find any evidence if there is no radar coverage. This reminds me of the Pan Am Flt 103, B-747 that was bombed over Lockerbie, Scotland, killing all aboard plus some on the ground. The reason why Flt 103 exploded over land and not over the sea as it was planned, was because Flt 103 was delayed for take off by 2 hours at Heathrow, which would have been somewhere between Iceland and Greenland if it had been on time, which all evidence would have been lost at see and the Libyan agents would not have been caught as a result. So bombing of Flt 447 is a very possibility. I would like to know whether the recovered bodies were all naked or they had clothes on them. If they are found to be naked, it would indicate if the plane broke up in the air and people feel to their deaths (they would have been already dead in few seconds if the plane broke up at 35,000 ft ) at high speed causing their clothes to be ripped off them. I would also like to know who were on board, like any important people.
This was ruled out because of all the data received from ACARS indicating several electrical system failures. If there was a bomb, there would be no ACARS transmission as AF447 would have been an instant fireball. Add to this the prevailing severe weather conditions, and the potential for structural failure. Terrorism is extremely
unlikely.
So, here you have it Paphitis, but I have one other thing to state here and that is;
"I want to comment on the "Black Boxes" for a moment. I do not understand, why the general aviation administration has not built a system where all flight and voice recordings are transmitted by radio frequency to a land based computer through all our GPS and communication satellites that are out there in space at the same time such information is also fed into the aircrafts own "black boxes". This way, we do not have to always worry about whether we can find the "black boxes" or not from every time a plane crashes, to get the information to find out what the cause was, because all the information will be available on a computer on land somewhere. I have been questioning this idea in my head for many years now, and yet, it has not happened. Why not.?"
Well, I can tell you that the above is possible. So why has it not happened?
Probably because of the
"Affordable Safety" ideals that have penetrated the industry over the last 20 years. The costs and logistics of setting something like this up would be enormous and airlines would need to fork out for these costs. They will eventually pass on these costs to the flying public and perhaps that is a bit prohibitive.
But I do agree with your idea.
As always, I really enjoy your aviation posts and insight...
Keep posting more whenever possible..