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Air France Jet Crash |
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| Jun3-09, 11:03 PM | #35 |
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Air France Jet Crash[edit] Just read up on TWA 800. That one was apparently, that catastrophic: the plane just abruptly disappeared, electronically. The flight data recorders were intact and simply stopped recording and the transponder stopped tranmitting. For Pan Am 103, I was wrong, though: the wiki says that while the explosion only punched a 20 inch hole in the fuselage, but the secondary effects, structural damage and aerodynamic forces were enough to rapidly tear apart the plane... but not violent enough to kill the passengers. It's a little disturbing to think about, but in most such cases (and in the Shuttle Challenger!), the passengers were almost certainly killed by impact with the ground, not by the explosion/breakup of the aircraft. [edit2] TWA 800 was particularly gruesome. Though the explosion was much bigger than Pan Am 103's, the damage was more localized and complete -and not huge, meaning the damage didn't affect the rest of the plane at all. Ironically, this led to a very similar crash scenario: the nose separated from the fuselage and fell intact and the body with the wings continued intact in a separate piece. Most of the passengers surely survived the explosion and those in the back 3/4 of the plane rode a burning but still flying piece of airplane until it pitched up enough to rip off the wings (probably only a few seconds), then fell, in flames. It must have been horrible. |
| Jun3-09, 11:05 PM | #36 |
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Wings can also take a lot of stress, 787 wing being loaded to 150% of it's maximum design load
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| Jun3-09, 11:51 PM | #37 |
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The last I heard of it on public channels, it was aired on NBC with graphics supplied by the CIA involving the conclusion of a flame front chassing the plane then igniting the center tanks. The early official story evolved from plausible to ad hoc. It stinks of team spirit. |
| Jun4-09, 12:22 AM | #38 |
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Commerical oceanic airliners are required to have instruments in thriplets (two for over-land flights).
For instance, there are 3 ADIRUs (Air Data [and] Inertial Reference Units). There are three flight computers. If the first pair disagree, they are shut down, and the third assumes control. The first indicated failures that, apparently, caused the autopilot program to relenquish control, were from the ADIRUs and the ISISs. These are located in instrument bays somewhere in the main airframe. Probably under the cockpit. Concerning cabin pressure of the last transmission, in the goof lingo used in commercial aviation, I read "Cabin vertical speed" advisory to mean what you all have thought it to be: a drop in cabin pressure. Thanks for the link MGB... But the initial failures reported occured in the ADIRUs and the ISISs. These are equipped with redundant power sources: 120V/400Hz, 28V and 28V battery backup. They are equipped with lightning supression circuits. Can they protect against all overvoltage spikes producted by lightning? I don't see how. |
| Jun4-09, 12:38 AM | #39 |
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| Jun4-09, 12:40 AM | #40 |
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| Jun4-09, 12:53 AM | #41 |
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| Jun4-09, 01:13 AM | #42 |
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Here's an interesting plane crash where a change of CG due to the pilot going to the bathroom (!), combined with wind shear caused the breakup of a small plane:
Relevant fresh news story: http://news.yahoo.com/s/ap/brazil_plane |
| Jun4-09, 01:16 AM | #43 |
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Interesting article about this crash and a "brutal freak turbulence" theory:
From the wiki on that crash: So that example is of exactly the type of thing I was speculating about. But it also is 40 years old. |
| Jun4-09, 01:55 AM | #44 |
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Here's my scenario.
I presume Airbus builds it's nose cones from carbon fiber. Why? because of the compound curvature of the surface and Airbus's dedication to reducing fuel costs from any quarter. If they don't build it from carbon, nevermind, I'm up the wrong tree. Carbon composite has far greater bulk resistivity than aluminum. Electical damage to semiconductors was once identificed as coming from both electrostatic discharge and induced electromagnetic induction (ESD-EMI). Lighning has a great capability for induction. Changing fields on one side of a carbon fiber barrier can transmit to the other side. Simply put, carbon fiber makes a poor Faraday cage. On the other side of the nose cone resides the main avionics systems, as far as I can tell. I surmise that lightning penatrated the nose and took out the main avionics. |
| Jun4-09, 05:31 AM | #45 |
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Anybody knows if navy submarines are used to help localize black box? They are equipped with the state of the art hydrophones, they can be at the site in a blink (well, much faster than surface vessels) and they are not limited by the weather.
Could be it is not as easy - their hydrophons can be optimized for other frequencies and for other directions, but the idea seems plausible to me. |
| Jun4-09, 08:38 AM | #46 |
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They say pilot slowed down - perhaps too much - before flying into the thunderstorm area.
I wonder where this information came from. |
| Jun4-09, 09:07 AM | #47 |
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| Jun4-09, 09:12 AM | #48 |
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The 150% wing test always struck me as a slightly silly figure. It's 150% of the intended operating maximum - of course if you really design the operating maximum to be the worst conditions it could encounter then there is no need for 150%. But if you consider the maximum to be the maximum for normal use then 150% is too small a margin for some of the situations it could get into. |
| Jun4-09, 09:18 AM | #49 |
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The problem is that the sea is 4km deep with a rocky bottom, at that depth sidescan will tell you nothing. |
| Jun4-09, 09:29 AM | #50 |
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The main issue with composite airframes and lightning is electrically bonding panels together, if there is a break in electrical continuity between a panel that is hit and an adjacent one you get arcing which leads to damage. |
| Jun4-09, 09:40 AM | #51 |
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http://en.wikipedia.org/wiki/Underwater_locator_beacon Edit: mgb already answered while I was googling. |
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