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#1
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posted to rec.boats
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Oh no. Here we go again. This is definitely not cool.
http://www.nbcnews.com/news/world/ai...e-says-n275696 |
#2
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posted to rec.boats
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On 12/27/14 11:29 PM, Tim wrote:
Oh no. Here we go again. This is definitely not cool. http://www.nbcnews.com/news/world/ai...e-says-n275696 Another air travel tragedy. ![]() |
#3
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posted to rec.boats
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They're not sure but the searchers are finding oily stuff floating. The news is saying it's probably on the bottom of the ocean...
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#4
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posted to rec.boats
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Late last evening and just this morning, I've begun hearing discussions about the flight control systems in Airbus and pilot's misinterpretations being a possible factor. Another topic touched upon briefly was "jet upset", an event that can happen because of the fact that jets operating at such high altitudes where the air is very thin can be very close to the stalling speed even at the proper cruising speed. Any sudden movement of the controls or rapid change in relative wind because of weather (especially in a thunderstorm) can cause a high speed stall from which it is very difficult if at all possible to recover.
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#5
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posted to rec.boats
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On Mon, 29 Dec 2014 11:31:38 -0500, wrote:
On Mon, 29 Dec 2014 06:30:56 -0800 (PST), Tim wrote: They're not sure but the searchers are finding oily stuff floating. The news is saying it's probably on the bottom of the ocean... AvWeb had this interesting tidbit from the FAA about the AirBus 320 (the plane that floats better than it flies) http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/210629d32e131bc986257daa007ccddb/$FILE/2014-25-51_Emergency.pdf http://tinyurl.com/qjmagsd === Automation run amok, scary stuff when there are lives at stake. |
#6
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posted to rec.boats
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Tim wrote:
They're not sure but the searchers are finding oily stuff floating. The news is saying it's probably on the bottom of the ocean... The air bus is mostly plastic, so should be a lot of floating debris. |
#7
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posted to rec.boats
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#8
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posted to rec.boats
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Another thing to consider is the plane was already at 38000 ft and the craft is rooted for a safety cowling of 39. And the pilot requested to climb? Maybe it was like the USS Thrasher only reverse
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#9
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posted to rec.boats
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On 12/29/2014 4:30 PM, Tim wrote:
Another thing to consider is the plane was already at 38000 ft and the craft is rooted for a safety cowling of 39. And the pilot requested to climb? Maybe it was like the USS Thrasher only reverse Thresher. What I am hearing is it was flying at 32,000 ft and the pilot requested 38,000. That request was denied due to other aircraft in the area. It raises the question of why the pilot tried to climb anyway (assuming he did). What actually happened will eventually come out if they recover the black boxes. My pure guess right now is faulty input data in the flight management system causing the pilot to react in a manner that was inappropriate, further complicated by the thunderstorms and attempts to avoid them. I think the altitude rating is conservative and is for normal flight conditions. It can actually go higher but it's not normal procedure. |
#10
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posted to rec.boats
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On Mon, 29 Dec 2014 15:58:50 -0500, "Mr. Luddite"
wrote: On 12/29/2014 3:20 PM, wrote: On Mon, 29 Dec 2014 13:40:19 -0600, Califbill wrote: Tim wrote: They're not sure but the searchers are finding oily stuff floating. The news is saying it's probably on the bottom of the ocean... The air bus is mostly plastic, so should be a lot of floating debris. I am sure they will turn up a debris field pretty soon and this is relatively shallow water so getting the boxes will be easier to do as soon as we get decent assets in the area. The more we hear, the more this sounds like a departure stall and an unrecoverable dive into the sea. If these 3d world bozos maintained their boxes, they should have the real answer pretty soon. Politics and the legal issues may determine when it is actually announced to the public. Not technically a "departure" stall, but similar if the pilot was trying to climb at too steep of an angle of attack for speed. Departure stalls are practiced all the time in flight school and simulate a take-off with too steep of an angle of attack. Basically you are trying to stand the airplane on it's tail at full throttle while balancing it with the rudder. Eventually it stops flying and drops, usually to one side which, if not corrected, can result in a spin. === If you closely read the Airworthiness Directive that Greg found, you will notice that it is not an actual stall condition they are warning about. Instead it is an instrumentation error that triggers the flight automation system into an erroneous stall recovery mode. The stall recovery automation does the text book solution by putting the plane into a nose down dive to build airspeed and get the plane flying again. The problem is that the plane was never in a stall to begin with, and there is a special sequence that the pilots have to follow to disable the automation and get the plane out of the dive. Scary stuff if it takes the pilots by surprise and they are not carefully trained. http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/210629d32e131bc986257daa007ccddb/$FILE/2014-25-51_Emergency.pdf I quote: ----------------------------------------- An occurrence was reported where an Airbus A321 aeroplane encountered a blockage of two Angle of Attack (A of A) probes during climb, leading to activation of the Alpha Protection (Alpha Prot) while the Mach number increased. The flightcrew managed to regain full control and the flight landed uneventfully. When Alpha Prot is activated due to blocked A of A probes, the flight control laws order a continuous nose down pitch rate that, in a worst case scenario, cannot be stopped with backward sidestick inputs, even in the full backward position. If the Mach number increases during a nose down order, the A of A value of the Alpha Prot will continue to decrease. As a result, the flight control laws will continue to order a nose down pitch rate, even if the speed is above minimum selectable speed, known as VLS. This condition, if not corrected, could result in loss of control of the aeroplane. --------------------------------------------------------- |
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