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#51
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HondaJet: Not A Steam Gage In Sight
On Thu, 26 Oct 2006 20:21:49 GMT, "Neil Gould"
wrote in : He probably wouldn't have been able to fix the problem en route. As the fix was to burn fuel from the wing tanks before switching to the aux tank, it seems possible to have done it en route. |
#52
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HondaJet: Not A Steam Gage In Sight
Mxsmanic wrote: cjcampbell writes: Most people know that the TV set turns off when the power goes out. You would have to be incredibly stupid to not know that the panels will go off in a power failure. I'm talking about a reboot, not a power failure. The emergency procedures address that. IIRC you shut the thing off, wait something like 30 seconds, then restart. What happens after that depends on the aircraft and the installation. It is possible that the rebooting can be stopped by simply pulling the circuit breaker of the offending unit, leaving the rest of the system operational. One of the advantages of the G1000 over earlier, similar systems like Avidyne is that you can shut it off and then restart it while still in the air. This is a vast improvement over the earlier systems which, once you shut them off, had no way of restarting themselves while the aircraft was moving. |
#53
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HondaJet: Not A Steam Gage In Sight
Mxsmanic wrote: cjcampbell writes: People who fly real airplanes know that anything can break. It is part of the training. I don't have the pilots in mind. I'm thinking of the vendor. If he had the time and knowledge to create an emergency procedure, he had the time and knowledge to fix the bug that can cause a reboot in the first place, which would be far more responsible than simply documenting it and forgetting about it. You are a child, yet. Things don't work that way. The vendor comes up with emergency procedures for every conceivable scenario. The manufacturer knows that almost anything is possible, even though it never shows up in development and testing, and tries to cover all possible bases. Garmin certainly did not intentionally release defective units. |
#54
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HondaJet: Not A Steam Gage In Sight
Recently, Larry Dighera posted:
On Thu, 26 Oct 2006 20:21:49 GMT, "Neil Gould" wrote in : He probably wouldn't have been able to fix the problem en route. As the fix was to burn fuel from the wing tanks before switching to the aux tank, it seems possible to have done it en route. IIRC, that procedure was opposite the instructions for the use of the aux tank. As he wasn't able to get out and take a look at what was happening en route, that would not have been a viable option because if the instructions were correct (which he found out after the fact that they weren't), it would have killed him. Neil |
#55
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HondaJet: Not A Steam Gage In Sight
On Fri, 27 Oct 2006 10:19:40 GMT, "Neil Gould"
wrote in : Recently, Larry Dighera posted: On Thu, 26 Oct 2006 20:21:49 GMT, "Neil Gould" wrote in : He probably wouldn't have been able to fix the problem en route. As the fix was to burn fuel from the wing tanks before switching to the aux tank, it seems possible to have done it en route. IIRC, that procedure was opposite the instructions for the use of the aux tank. As he wasn't able to get out and take a look at what was happening en route, that would not have been a viable option because if the instructions were correct (which he found out after the fact that they weren't), it would have killed him. My point it, that if the fuel gages were operational, and the pilot observed anomalous fuel venting from the wing tanks while crossing the Atlantic Ocean, he may have reasoned, that drawing fuel from the wing tanks might have been preferable to jettisoning it overboard despite the erroneous aux-tank operating instructions. |
#56
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HondaJet: Not A Steam Gage In Sight
Recently, Larry Dighera posted:
On Fri, 27 Oct 2006 10:19:40 GMT, "Neil Gould" wrote in : Recently, Larry Dighera posted: On Thu, 26 Oct 2006 20:21:49 GMT, "Neil Gould" wrote in : He probably wouldn't have been able to fix the problem en route. As the fix was to burn fuel from the wing tanks before switching to the aux tank, it seems possible to have done it en route. IIRC, that procedure was opposite the instructions for the use of the aux tank. As he wasn't able to get out and take a look at what was happening en route, that would not have been a viable option because if the instructions were correct (which he found out after the fact that they weren't), it would have killed him. My point it, that if the fuel gages were operational, and the pilot observed anomalous fuel venting from the wing tanks while crossing the Atlantic Ocean, he may have reasoned, that drawing fuel from the wing tanks might have been preferable to jettisoning it overboard despite the erroneous aux-tank operating instructions. I understand your point, but that's a pretty big "if", IMO. First, the pilot would have to "observe anomalous fuel venting". Is this possible? Next, the pilot would have to reason why the fuel was venting, and I don't see how that would have been possible. It would seem as likely that the conclusion would be that there was some problem with the main tanks, and thus more reliance on the aux tank, aggravating the problem, etc. After all, why would it be reasonable to suspect that fuel would be venting from tanks that were shut off, supposedly taking them out of the system, and that the "fix" would be to disregard the specific instructions on the use of the aux tank? I think Mr. Rhine's analysis of his circumstances and choice of action were right on, as the relevant information was only obtained after-the-fact. Neil |
#57
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HondaJet: Not A Steam Gage In Sight
On Fri, 27 Oct 2006 14:10:18 GMT, "Neil Gould"
wrote in : Recently, Larry Dighera posted: On Fri, 27 Oct 2006 10:19:40 GMT, "Neil Gould" wrote in : Recently, Larry Dighera posted: On Thu, 26 Oct 2006 20:21:49 GMT, "Neil Gould" wrote in : He probably wouldn't have been able to fix the problem en route. As the fix was to burn fuel from the wing tanks before switching to the aux tank, it seems possible to have done it en route. IIRC, that procedure was opposite the instructions for the use of the aux tank. As he wasn't able to get out and take a look at what was happening en route, that would not have been a viable option because if the instructions were correct (which he found out after the fact that they weren't), it would have killed him. My point it, that if the fuel gages were operational, and the pilot observed anomalous fuel venting from the wing tanks while crossing the Atlantic Ocean, he may have reasoned, that drawing fuel from the wing tanks might have been preferable to jettisoning it overboard despite the erroneous aux-tank operating instructions. I understand your point, but that's a pretty big "if", IMO. First, the pilot would have to "observe anomalous fuel venting". Is this possible? Apparently it's not only possible, it actually occurred. You need to read Mr. Rhine's narrative: http://www.alexisparkinn.com/nwpilot's_tranatlantic_flight.htm Upon reaching FL095 I was on top and looked to my left -- and really got scared!!! The aircraft vent was venting a large amount of fuel out into space! Thank you, Cessna for the under-wing courtesy lights! Next, the pilot would have to reason why the fuel was venting, and I don't see how that would have been possible. Really? Surely your powers of deduction are capable of reasoning, that fuel is exiting the vent because the tank is full. It would seem as likely that the conclusion would be that there was some problem with the main tanks, That conclusion would be partially correct; they were over full. and thus more reliance on the aux tank, aggravating the problem, etc. Alternatively, an insightful pilot might have reasoned, that burning fuel from over full tanks might alleviate the over full condition. After all, why would it be reasonable to suspect that fuel would be venting from tanks that were shut off, supposedly taking them out of the system, If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, prior to departure, he would know, that the wing tanks remain in the system regardless of the position of the fuel selector and fuel shutoff valves. and that the "fix" would be to disregard the specific instructions on the use of the aux tank? If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, he would have a good chance of figuring out what was occurring, IMO. I know I would have thoroughly scrutinized the POH, and mentally analyzed the function of the fuel system and its modifications, before departing. I think Mr. Rhine's analysis of his circumstances and choice of action were right on, as the relevant information was only obtained after-the-fact. I'm not questioning Mr. Rhine's action when he realized he had a problem. There is little question, even if the cause had been reasoned out, that it would be prudent to get back on the ground pronto. But I believe, that a pilot who had analyzed the fuel system's operation before departure, would have had a good chance of, not only diagnosing the cause of the fuel venting in flight, but questioning the functionality of the fuel system modification before departure. |
#58
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HondaJet: Not A Steam Gage In Sight
Recently, Larry Dighera posted:
On Fri, 27 Oct 2006 14:10:18 GMT, "Neil Gould" wrote in After all, why would it be reasonable to suspect that fuel would be venting from tanks that were shut off, supposedly taking them out of the system, If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, prior to departure, he would know, that the wing tanks remain in the system regardless of the position of the fuel selector and fuel shutoff valves. and that the "fix" would be to disregard the specific instructions on the use of the aux tank? If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, he would have a good chance of figuring out what was occurring, IMO. I know I would have thoroughly scrutinized the POH, and mentally analyzed the function of the fuel system and its modifications, before departing. So, in essence, you are saying that Mr. Rhine's main problem was that he didn't reverse-engineer the installations of the aux tank and electronics, because had he done that, he would have known that the instructions for the use of the aux tank were eroneous and that there were problems with the electronics. Frankly, I think that would be beyond many (if not most) pilots' capabilities. Given your own predisposition towards thinking that the G1000's failure was in a problem of its design (e.g. calling Mr. Rhine's failure experience a "mode") rather than a side-effect of a botched installation of unrelated panel components, I think it may be unreasonable to think that the average pilot could analyze such a situation any better than Mr. Rhine did. The most recent C172 that I've flown was our club's C172SP. I would not call its construction as being conducive to such an analysis by anyone other than an A&P. Since the instructions included by the installer of the aux tanks were clearly wrong, the only way to understand the actual installation of the aux tank and its impact on the C172's fuel system would be to take the plane apart. I did not have the impression that this was one of Mr. Rhine's options. Neil |
#59
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HondaJet: Not A Steam Gage In Sight
cjcampbell writes:
You are a child, yet. Things don't work that way. That doesn't mean that they can't. It's possible to build reliable software systems. Unfortunately, people have been conditioned to accept catastrophic errors in software systems as if they were unavoidable realities rather than simply the avoidable result of carelessness. And they are usually unwilling to pay the cost of error-free systems, anyway, even if it misking risking their own lives to save money. But many of them don't realize the actual magnitude of the risks they are accepting. Software bugs are not imposed by Mother Nature or the laws of physics; they are the result of poor design and construction, just like physical engineering defects. There is no excuse for them in safety-of-life applications, and companies should be held liable for their reckless mistakes in building safety-of-life applications that contain dangerous bugs. The vendor comes up with emergency procedures for every conceivable scenario. The catastrophic software failures are often those that the vendor has not bothered to imagine. It is the unhandled exception that causes the catastrophic failure. Garmin certainly did not intentionally release defective units. Probably true, but that doesn't mean that it is blameless for defects. There are still notions of due diligence and fiduciary duty, although for some reason people seem reluctant to apply them to the software industry, even though they might apply them ruthlessly in any other comparable domain. -- Transpose mxsmanic and gmail to reach me by e-mail. |
#60
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HondaJet: Not A Steam Gage In Sight
On Fri, 27 Oct 2006 16:21:49 GMT, "Neil Gould"
wrote in : Recently, Larry Dighera posted: On Fri, 27 Oct 2006 14:10:18 GMT, "Neil Gould" wrote in After all, why would it be reasonable to suspect that fuel would be venting from tanks that were shut off, supposedly taking them out of the system, If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, prior to departure, he would know, that the wing tanks remain in the system regardless of the position of the fuel selector and fuel shutoff valves. and that the "fix" would be to disregard the specific instructions on the use of the aux tank? If the prudent pilot of a transatlantic flight has invested the time required to familiarize himself with the design and operation of the aircraft's fuel system upon which his safety depends for the over water portion of his course, he would have a good chance of figuring out what was occurring, IMO. I know I would have thoroughly scrutinized the POH, and mentally analyzed the function of the fuel system and its modifications, before departing. So, in essence, you are saying that Mr. Rhine's main problem was that he didn't reverse-engineer the installations of the aux tank and electronics, because had he done that, he would have known that the instructions for the use of the aux tank were eroneous and that there were problems with the electronics. I'm not saying anything about Mr. Rhine being wrong. Frankly, I think that would be beyond many (if not most) pilots' capabilities. If a pilot is incapable of understanding his aircraft's fuel system, he should not be certified to fly it. Given your own predisposition towards thinking that the G1000's failure was in a problem of its design (e.g. calling Mr. Rhine's failure experience a "mode") rather than a side-effect of a botched installation of unrelated panel components, I think it may be unreasonable to think that the average pilot could analyze such a situation any better than Mr. Rhine did. I fail to understand how the Garmin G1000's continuous re-boot mode can be seen as anything other than a failure mode. If Garmin had conceived of a modular, fault tolerant design, such a failure mode may not have occurred. The average pilot doesn't fly solo across the Atlantic, so I'm not sure your opinion is relevant. The most recent C172 that I've flown was our club's C172SP. I would not call its construction as being conducive to such an analysis by anyone other than an A&P. Does not the POH contain a fuel system schematic diagram and theory of operation information? It shouldn't be beyond the average pilot's ability to comprehend that information. Since the instructions included by the installer of the aux tanks were clearly wrong, the only way to understand the actual installation of the aux tank and its impact on the C172's fuel system would be to take the plane apart. The ONLY way? Please. Why couldn't one request a similar aux fuel system schematic diagram and theory of operation information as contained in the POH from the aux tank STC holder. I did not have the impression that this was one of Mr. Rhine's options. A pilot always has the option of requesting more information, no? |
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