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#41
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In article ,
"Morgans" wrote: "Jay Honeck" wrote The wing clearly departed the airframe before the crash. I wonder if these old birds are simply fatigued? I wonder about catastrophic unconfined engine failure, severing the spar. There was an account of the sound and sight of an explosion before the wing departed, wasn't there? Snapping structures sound a lot like explosions -- especially to nonexpert witnesses. -- Remve "_" from email to reply to me personally. |
#42
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The PT6 is mounted above and forward of the wing leading
edge, if the turbine had a failure, the bits and pieces are not likely to impact the wing. But, if that happened there will be positive evidence. The PT6 is a pretty small turbine, they don't have many problems internal to the engine. -- James H. Macklin ATP,CFI,A&P -- Merry Christmas Have a Safe and Happy New Year Live Long and Prosper Jim Macklin "Big John" wrote in message ... | Jay | | A monday morning WAG. | | Turbine (disk) blew up and destroyed enough of the wing structure that | it failed. | | Fuel tank(s) in wing then dumped fuel on hot parts of turbine and | caught fire. | | Wingless (one wing) fuselage impacted water and broken off wing | floated down burning until it hit the water. | | Lets see if my years of experience with accidents guessed right on | this bad accident. | | Big John | `````````````````````````````````````````````````` ````````````` | | On Tue, 20 Dec 2005 14:08:24 GMT, "Jay Honeck" | wrote: | | My guess is that they had a loose or broken fuel line, | caught fire and the fuel vapor exploded and the fire melted | the spar enough for it to fail. | | Boy, I sure hope that's "all" it was. (Who'd ever think we'd be saying that | kind of stuff?) | | With everyone describing an "explosion" (which the video tends to | support) -- and Chalk's not having to do much in the way of security | screening, as a small carrier -- this could easily have been some kind of a | nut-job with a shoe bomb and a "cause". | | And *then* we'd start seeing all sorts of stupid proposals for "enhanced | security" that we don't want or need. | | Sad to say, a mechanical problem is the best-case scenario. | |
#43
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"Jack" wrote in message
. net... [...] Just how elastic do you think the connections between the airframe and the engine are? When it comes to acceleration, they better form pretty much one piece, don't you think? For the sake of this discussion, it doesn't really matter. The difference in forces may be negligible, but *inasmuch as they might not be*, a lighter engine doesn't help, it hurts. Still, your comment about elasticity is irrelevant. Gross weight is what we accelerate, not components. The components are connected by structure designed for specific forces. For example, I can add a one ounce weight to the back of my airplane with some scotch tape, and it won't fall off, no matter how fast I accelerate. But if I tried to pull the entire airplane by pulling on that one ounce weight, the tape will fail, even at extremely low acceleration. Pete |
#44
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This news article
(http://www.breitbart.com/news/2005/12/20/D8EKBRTG0.html) says that the wing was recovered from the water today, and the engine and prop are still attached. There's even a photo showing it. Looks like the wing separated pretty well inboard of the engine. At this point, speculation seems that either a fuel leak/fire melting the spar... or perhaps just simple plain structural failure of the spar with the fire happening afterwards could both possibly explain the wing separation. Jim Macklin wrote: More likely that a fuel line was not properly safetied or otherwise failed. Turbine engines have fuel pressures as high a 1,000 PSI, so the fuel system in the engine is highly stressed. The fuel supply pumps are high capacity and 50 to 100 PSI, so again, the fuel connections and lines are stressed. If there was a fuel leak into the nacelle, wing root area, any source of ignition could cause an explosion and the resulting fire would soften the aluminum spar quickly. The emergency procedure for a fire is to shut off the fuel valves, but if the failure was between the tank and fuel tank or the valve was damaged, it might not be possible to shut the fuel off. The NTSB is very good at investigating this type of failure, the will track melted and bent metal, see the pattern of soot and follow the fractures in the metal. |
#45
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The Chalk Island web site says that their airplanes were in
the shop for the engine changes and complete mechanical refurbishment and new paint/interiors. There should be some preliminary data released by the NTSB before Christmas or New Year, I would expect. -- James H. Macklin ATP,CFI,A&P -- Merry Christmas Have a Safe and Happy New Year Live Long and Prosper Jim Macklin wrote in message ps.com... | This news article | (http://www.breitbart.com/news/2005/12/20/D8EKBRTG0.html) says that the | wing was recovered from the water today, and the engine and prop are | still attached. There's even a photo showing it. Looks like the wing | separated pretty well inboard of the engine. At this point, | speculation seems that either a fuel leak/fire melting the spar... or | perhaps just simple plain structural failure of the spar with the fire | happening afterwards could both possibly explain the wing separation. | | | Jim Macklin wrote: | More likely that a fuel line was not properly safetied or | otherwise failed. Turbine engines have fuel pressures as | high a 1,000 PSI, so the fuel system in the engine is highly | stressed. The fuel supply pumps are high capacity and 50 to | 100 PSI, so again, the fuel connections and lines are | stressed. | | If there was a fuel leak into the nacelle, wing root area, | any source of ignition could cause an explosion and the | resulting fire would soften the aluminum spar quickly. The | emergency procedure for a fire is to shut off the fuel | valves, but if the failure was between the tank and fuel | tank or the valve was damaged, it might not be possible to | shut the fuel off. | | The NTSB is very good at investigating this type of failure, | the will track melted and bent metal, see the pattern of | soot and follow the fractures in the metal. | | |
#46
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#47
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Reports I saws this morning said that the NTSB said they
found a fatigue crack in the main spar, maybe the conversion was not done well or the maintenance was not though enough. I'll bet the fleet is grounded and they require immediate, "before further flight" NDT inspections of the wings, etc. -- James H. Macklin ATP,CFI,A&P -- Merry Christmas Have a Safe and Happy New Year Live Long and Prosper Jim Macklin "Ron Natalie" wrote in message m... | wrote: | I'm wondering if fitting turbine engines on the old airframes | didn't pull something loose in the wing/mount. | | Turbines run a whole lot smoother than the round Pratts that were on | originally. They don't have the power pulses that radial engines have. | | Not that they aren't subject to resonance issues. Remember the Electra? |
#48
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Jim Macklin wrote:
Reports I saws this morning said that the NTSB said they found a fatigue crack in the main spar, maybe the conversion was not done well or the maintenance was not though enough. I'll bet the fleet is grounded and they require immediate, "before further flight" NDT inspections of the wings, etc. Chalk's has voluntarily grounded thier Mallards and is performing an exhaustive test of the spars on one of them now. The NTSB rep voiced the opinion that age alone would not be sufficient to cause this failure; some additional stress would be required. George Patterson Coffee is only a way of stealing time that should by rights belong to your slightly older self. |
#49
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That is probably true. The odds are that inspections will
not find any other similar cracks in the rest of the Chalk fleet, I imagine that every Mallard, worldwide, will be inspected soon. It is even possible that the crack that was found was recent, metallurgical tests will have to be done to know for sure. It is even possible that it was caused by some defect dating back 50 years and was not visible on the surface. I'm sure that it will be fixed, too bad, a wing coming off has only one recovery mode, parachute a la Cirrus. -- James H. Macklin ATP,CFI,A&P "George Patterson" wrote in message news:ixoqf.29956$CL.291@trnddc04... | Jim Macklin wrote: | Reports I saws this morning said that the NTSB said they | found a fatigue crack in the main spar, maybe the conversion | was not done well or the maintenance was not though enough. | I'll bet the fleet is grounded and they require immediate, | "before further flight" NDT inspections of the wings, etc. | | Chalk's has voluntarily grounded thier Mallards and is performing an exhaustive | test of the spars on one of them now. The NTSB rep voiced the opinion that age | alone would not be sufficient to cause this failure; some additional stress | would be required. | | George Patterson | Coffee is only a way of stealing time that should by rights belong to | your slightly older self. |
#50
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George Patterson wrote:
Jim Macklin wrote: Reports I saws this morning said that the NTSB said they found a fatigue crack in the main spar, maybe the conversion was not done well or the maintenance was not though enough. I'll bet the fleet is grounded and they require immediate, "before further flight" NDT inspections of the wings, etc. Chalk's has voluntarily grounded thier Mallards and is performing an exhaustive test of the spars on one of them now. The NTSB rep voiced the opinion that age alone would not be sufficient to cause this failure; some additional stress would be required. A pretty irresponsible statement for an NTSB person. Fatigue can cause a stressed member to fail at a very low load, much less than even flight loads. I seem to remember a picture of a Buff whose wing had failed on the ground. It has been years and I don't remember the details, but it seems like it was due to something fairly innocous such as refueling. I believe fatigue was determined to be the root cause. Matt |
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