![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#1
|
|||
|
|||
![]()
It seems that if there are two possible causes for a helicopter accident,
the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. Further lets assume that the helicopter had had a prior series of hard landings or other beyond normal stress loadings. Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? What should their action be? Recall and supply exchange parts for no charge? Recall and supply exchange parts for their cost? Change the machining process and ignore the other parts out there? How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? |
#2
|
|||
|
|||
![]()
On Feb 8, 6:16*pm, "Stu Fields" wrote:
It seems that if there are two possible causes for a helicopter accident, the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. * However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. *Further lets assume that the helicopter had had a *prior series of hard landings or other beyond normal stress loadings. *Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? What should their action be? *Recall and supply exchange parts for no charge? *Recall and supply exchange parts for their cost? *Change the machining process and ignore the other parts out there? How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? Anybody know why this guy has such a hard-on? |
#3
|
|||
|
|||
![]() "oldrotor" wrote in message ... On Feb 8, 6:16 pm, "Stu Fields" wrote: It seems that if there are two possible causes for a helicopter accident, the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. Further lets assume that the helicopter had had a prior series of hard landings or other beyond normal stress loadings. Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? What should their action be? Recall and supply exchange parts for no charge? Recall and supply exchange parts for their cost? Change the machining process and ignore the other parts out there? How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? Anybody know why this guy has such a hard-on? I'll answer your question if you answer mine.. |
#4
|
|||
|
|||
![]()
"Stu Fields" wrote in message
... It seems that if there are two possible causes for a helicopter accident, the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. Further lets assume that the helicopter had had a prior series of hard landings or other beyond normal stress loadings. Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? What should their action be? Recall and supply exchange parts for no charge? Recall and supply exchange parts for their cost? Change the machining process and ignore the other parts out there? How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? Hi Stu, You mention a lot of variables here. My thoughts are this - first, why did the bird have a series of hard landings or other "beyond normal stress loadings?" Those, to me, sound like a piloting issue and not necessarily the kit manufacturers problem. Second, if the kit manufacturer discovers that they're selling parts that do have some kind of defect in design or machining, I think they should be obligated to making that right, either by an outright recall or by offering proper replacements to kit owners at cost. At the very least, they should issue a service advisory statement on the problem to be certain that the kit owners are aware it. Having said that, we are talking about "experimental" aircraft here. If I understand all that correctly, that means the owner/builder "is" the manufacturer of the aircraft and is ultimately the one responsible for the safe operation and maintenance of said aircraft. Still, if the kit manufacturer has any integrity, they'll be doing all they can to assist their customers with parts and materials that are discovered to be less than ideal for the job it's asked to do. I'm reminded of something Air Command did many years ago when they finally came around to the benefits of an in-line thrust design for pusher style gyroplanes. If I'm remembering correctly, they issued a statement advising anyone owning the older/original design bird to stop flying them and offered a new frame upgrade with a center line thrust design to "any" owner, "at cost," regardless of whether those owners bought the bird directly from Air Command or from an individual. I think it took a lot of guts for them to do that and speaks volumes for the integrity of the company. Does that answer your question? At least it might help spark the conversation! :-) Fly Safe, Steve R. |
#5
|
|||
|
|||
![]() "Steve R." wrote in message ... "Stu Fields" wrote in message ... It seems that if there are two possible causes for a helicopter accident, the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. Further lets assume that the helicopter had had a prior series of hard landings or other beyond normal stress loadings. Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? What should their action be? Recall and supply exchange parts for no charge? Recall and supply exchange parts for their cost? Change the machining process and ignore the other parts out there? How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? Hi Stu, You mention a lot of variables here. My thoughts are this - first, why did the bird have a series of hard landings or other "beyond normal stress loadings?" Those, to me, sound like a piloting issue and not necessarily the kit manufacturers problem. Second, if the kit manufacturer discovers that they're selling parts that do have some kind of defect in design or machining, I think they should be obligated to making that right, either by an outright recall or by offering proper replacements to kit owners at cost. At the very least, they should issue a service advisory statement on the problem to be certain that the kit owners are aware it. Having said that, we are talking about "experimental" aircraft here. If I understand all that correctly, that means the owner/builder "is" the manufacturer of the aircraft and is ultimately the one responsible for the safe operation and maintenance of said aircraft. Still, if the kit manufacturer has any integrity, they'll be doing all they can to assist their customers with parts and materials that are discovered to be less than ideal for the job it's asked to do. I'm reminded of something Air Command did many years ago when they finally came around to the benefits of an in-line thrust design for pusher style gyroplanes. If I'm remembering correctly, they issued a statement advising anyone owning the older/original design bird to stop flying them and offered a new frame upgrade with a center line thrust design to "any" owner, "at cost," regardless of whether those owners bought the bird directly from Air Command or from an individual. I think it took a lot of guts for them to do that and speaks volumes for the integrity of the company. Does that answer your question? At least it might help spark the conversation! :-) Fly Safe, Steve R. Surprising enough a series of hard landings were experienced by high time helicopter pilot. Ship didn't have anywhere near 400hrs when a shaft in the transmission experienced a fatigue failure. The focus was on the hard landings as the cause and the stress risers of the shaft were ignored. Another accident occurred where the builder did something not right which caused some strong vibrations. He corrected the problem but didn't replace a part that had a near zero radius fillet and that is exactly where the fatigue failure occurred. This resulted in a fatal accident. Another fatal accident occurred where another fatigue failure occurred at a place where the fillet radius was reported as sharp. Again other historical occurences were logged and the failure occurred at the sharp fillet radius. Again the focus was placed on the historical occurrences and not on the poorly machined fillet. There are a number of kits out there that have been supplied similar elements. The machinist for these parts had drawings which did not call out a fillet radius. (That has been changed now.) Another instance was called to the kit manufacturers attention where a rubber seal was scarring (0.020 deep jagged groove) in a main rotor shaft. The response was that they had seen this before and it didn't constitute a dangerous condition. To date the kit manufacturer has not sent out any warnings. They merely, on their website, offer to inspect and replace the parts if you are concerned about them. It sounds like they don't see a problem, but if you the builder-flyer does, they will try to make you happy. All of these parts are enclosed inside elements that come from the kit manufacturer complete and closed up and evern cotter keyed. Unless the kit builder tears these elements down and has enough of a technical background to do a good inspection, he will not be aware of the risk that he is taking. Yeah the Air Command story speaks highly of someone's integrity. (We probably know the guy). The "Center Line Thrust" was an arguable issue. Cdr. Ken Wallis had his opinions about this and he had more than a few hours in non "Center Line Thrust" ships. On the other hand the Stress concentrations seen in this other kit is a well known issue to avoid. Yeah I wish this kit manufacturer of issue would adopt the Air Command philosphy. Stu |
#6
|
|||
|
|||
![]()
"Stu Fields" wrote in message
... Surprising enough a series of hard landings were experienced by high time helicopter pilot. Ship didn't have anywhere near 400hrs when a shaft in the transmission experienced a fatigue failure. The focus was on the hard landings as the cause and the stress risers of the shaft were ignored. Another accident occurred where the builder did something not right which caused some strong vibrations. He corrected the problem but didn't replace a part that had a near zero radius fillet and that is exactly where the fatigue failure occurred. This resulted in a fatal accident. Another fatal accident occurred where another fatigue failure occurred at a place where the fillet radius was reported as sharp. Again other historical occurences were logged and the failure occurred at the sharp fillet radius. Again the focus was placed on the historical occurrences and not on the poorly machined fillet. There are a number of kits out there that have been supplied similar elements. The machinist for these parts had drawings which did not call out a fillet radius. (That has been changed now.) Another instance was called to the kit manufacturers attention where a rubber seal was scarring (0.020 deep jagged groove) in a main rotor shaft. The response was that they had seen this before and it didn't constitute a dangerous condition. To date the kit manufacturer has not sent out any warnings. They merely, on their website, offer to inspect and replace the parts if you are concerned about them. It sounds like they don't see a problem, but if you the builder-flyer does, they will try to make you happy. All of these parts are enclosed inside elements that come from the kit manufacturer complete and closed up and evern cotter keyed. Unless the kit builder tears these elements down and has enough of a technical background to do a good inspection, he will not be aware of the risk that he is taking. Yeah the Air Command story speaks highly of someone's integrity. (We probably know the guy). The "Center Line Thrust" was an arguable issue. Cdr. Ken Wallis had his opinions about this and he had more than a few hours in non "Center Line Thrust" ships. On the other hand the Stress concentrations seen in this other kit is a well known issue to avoid. Yeah I wish this kit manufacturer of issue would adopt the Air Command philosphy. Stu Well, it certainly sounds like the kit manufacturer isn't much interested in making this good without a lot more motivation. Considering they know the tail drive needs updating (and has, in fact, within their organization), I'd think they'd want to let that fact be known. It's a matter of safety and it's disappointing that they're not stepping up on this. I assume you're not in a position to say what company this is? The tail drive issues are one thing. I'm absolutely flabbergasted that they'd say that a groove being machined into the "main rotor mast" by a problem seal "doesn't constitute a dangerous condition!!!" Good, then let "them" fly the thing! I understand that the centerline thrust issues was/is a hotly debated issue. I never understood why that was. I understand that there are relatively high time pilots out there that learned on HTL machines and have successfully flown them for many hours but that doesn't counter the fact that these machines are easily capable of doing the classic bunt over, or power push over. Too many people have died because of it, including others who were also described as "experienced" gyro pilots!! A true CLT pusher style gyro will not do that and is inherently a safer bird because of it. The fact that some well respected and experienced gyro pilots argued hard in favor of the HTL side of things left a very bad taste in my mouth way back when. Good luck with whatever you're trying to establish with the helicopter kit manufacturer! Fly Safe, Steve R. |
#7
|
|||
|
|||
![]() "Steve R." wrote in message ... "Stu Fields" wrote in message ... Surprising enough a series of hard landings were experienced by high time helicopter pilot. Ship didn't have anywhere near 400hrs when a shaft in the transmission experienced a fatigue failure. The focus was on the hard landings as the cause and the stress risers of the shaft were ignored. Another accident occurred where the builder did something not right which caused some strong vibrations. He corrected the problem but didn't replace a part that had a near zero radius fillet and that is exactly where the fatigue failure occurred. This resulted in a fatal accident. Another fatal accident occurred where another fatigue failure occurred at a place where the fillet radius was reported as sharp. Again other historical occurences were logged and the failure occurred at the sharp fillet radius. Again the focus was placed on the historical occurrences and not on the poorly machined fillet. There are a number of kits out there that have been supplied similar elements. The machinist for these parts had drawings which did not call out a fillet radius. (That has been changed now.) Another instance was called to the kit manufacturers attention where a rubber seal was scarring (0.020 deep jagged groove) in a main rotor shaft. The response was that they had seen this before and it didn't constitute a dangerous condition. To date the kit manufacturer has not sent out any warnings. They merely, on their website, offer to inspect and replace the parts if you are concerned about them. It sounds like they don't see a problem, but if you the builder-flyer does, they will try to make you happy. All of these parts are enclosed inside elements that come from the kit manufacturer complete and closed up and evern cotter keyed. Unless the kit builder tears these elements down and has enough of a technical background to do a good inspection, he will not be aware of the risk that he is taking. Yeah the Air Command story speaks highly of someone's integrity. (We probably know the guy). The "Center Line Thrust" was an arguable issue. Cdr. Ken Wallis had his opinions about this and he had more than a few hours in non "Center Line Thrust" ships. On the other hand the Stress concentrations seen in this other kit is a well known issue to avoid. Yeah I wish this kit manufacturer of issue would adopt the Air Command philosphy. Stu Well, it certainly sounds like the kit manufacturer isn't much interested in making this good without a lot more motivation. Considering they know the tail drive needs updating (and has, in fact, within their organization), I'd think they'd want to let that fact be known. It's a matter of safety and it's disappointing that they're not stepping up on this. I assume you're not in a position to say what company this is? The tail drive issues are one thing. I'm absolutely flabbergasted that they'd say that a groove being machined into the "main rotor mast" by a problem seal "doesn't constitute a dangerous condition!!!" Good, then let "them" fly the thing! I understand that the centerline thrust issues was/is a hotly debated issue. I never understood why that was. I understand that there are relatively high time pilots out there that learned on HTL machines and have successfully flown them for many hours but that doesn't counter the fact that these machines are easily capable of doing the classic bunt over, or power push over. Too many people have died because of it, including others who were also described as "experienced" gyro pilots!! A true CLT pusher style gyro will not do that and is inherently a safer bird because of it. The fact that some well respected and experienced gyro pilots argued hard in favor of the HTL side of things left a very bad taste in my mouth way back when. Good luck with whatever you're trying to establish with the helicopter kit manufacturer! Fly Safe, Steve R. Steve: As an old Bensen pilot from the "Self Taught 60's" when dual instruction didn't exist, I taught myself to fly the thing as well a my wife at the time soloed also. However, the advent of the side-by-side ships presented an aerodynamic "Barn Door" which may have had something to do with the bunt overs, and there were sure a bunch. I flew in winds and turbulence with mine strong enough to hover and fly backwards and never had a problem. In fact our ship never had a ding. It is true that once while doing the "Brock Spirals" I noticed the nose tipping over more and more. Reduction of throttle and easing forward on the cyclic and stopping the rotation was all that was required. Based on my experience, I think that the old Bensens were relatively safe with their "Rock Guard" horizontal and a relatively high thrust line. I also noticed flying the Sparrohawk prototype that the hands off flying thru turbulence had nearly zero pitch disturbance. I guess if I had a side-by-side gyro I would probably look much closer at the CLT. However the helicopters have my attention now. This issue with the scarred main rotor shaft is the fourth separate issue of what is apparently ignorance or disregard of fatigue problems. Even when I reference things like the Standard Handbook of Machine Design, they pretty much ignore me. I don't understand their apparent ignoring what could be a very nasty liability issue. Stu |
#8
|
|||
|
|||
![]() "The OTHER Kevin in San Diego" skiddz "AT" adelphia "DOT" net wrote in message ... On Mon, 8 Feb 2010 16:16:59 -0800, "Stu Fields" wrote: It seems that if there are two possible causes for a helicopter accident, the preferred one for the manufacturer is the one for which they have no fault. That certainly is the best for them. However, lets say that a low hour helicopter suffers a failure directly attibutable to fatigue. Further lets assume that the helicopter had had a prior series of hard landings or other beyond normal stress loadings. Now lets further assume that the fatigue failure occurred at a point in the helicopter drive system where a diameter change was machined into the shaft without any radius or attempt at a proper fillet which yielded a strong stress riser. Lets say that the kit manufacturer is very aware that a number of kits have been sold with the same machining flaw. Should the kit manufacturer issue a service advisory statement advising all owners of those ships of a potential safety issue caused by those parts? You'd hope so. What should their action be? Recall and supply exchange parts for no charge? If it's a machining/design defect, absolutely. Since you mention in a later post the machine shop was given drawings that don't indicate any type of fillet where the diameter of the shaft changes, I'd lean towards a design defect and expect the manufacturer to replace the shaft on their dime. Recall and supply exchange parts for their cost? At a minimum. Change the machining process and ignore the other parts out there? If I'm following what you said, it's not a machining process issue. It's that the designer (or CAD guy) didn't call out that fillet. How about sell the business to someone else and just duck and hope that nothing bad ever comes from the above? Would that "absolve" the previous owners of any liability, especially if they were aware of the issue prior to peddling the biz? Common sense (and the litigous nature of the States these days) says no but we all know how short in supply THAT is. This wouldn't have anything to do with your upcoming project, would it? Hi Kevin. Things have moved on. I have found a jagged groove in the main rotor shaft that is approx 0.020 deep with jagged bottom. I've got a photo from an optical comparator for more detail. This groove occurs just at the top of a roller bearing that is the last point of support of the shaft. There is a rubber seal at this point. Manufacturers instructions were to remove the spring from the inside of this seal to avoid possible gouging of the shaft. Well evidently the rubber seal is capable without the spring of generating this jagged groove. The manufacturer has said that they have seen these before and they do not constitute a hazardous condition!! This is a soft (non-heat treated) TI shaft and all my books say that TI doesn't handle fatigue well if the surface of the shaft is rough with imperfections. I could be wrong, but I don't believe that the manufacturer has done a detailed fatigue analysis of the shaft with this kind of groove. Hell with what I've read about fatigue, it would take a world famous structural engineer with a bunch of fatigue design experience to convince me to fly that shaft. Even then I would want to try to borrow a bunch of money from him before my flight to test his surety. Apparently, based on written statements, the manufacturer doesn't believe that any of the accidents that occured were the fault of the poor fillets. Even in spite of the accident investigating agencies statement that the fatigue failure had occurred where the fillet was a sharp corner. There were reportedly other events of exceptional stresses that possibly could have started a crack in these highly stressed points. The mfr. has issued drawings that specify radiuses at the flillet locations and have offered a "Speedy-Sleeve" to protect the shaft from seal wear. All new ships are supposed to have these mods. The manufacturer has offered to provide these parts to owners of older ships. However, there has been no indication that the owners will receive any cost breaks. Aah the world of experimental aviation!!! I have sure got a new appreciation for the depth of the education available to the people who build, or buy kit aircraft. Upcoming project has had a closer look at the serious points and so far it looks good. That isn't to say that I'm not finding some warts on it, but so far, with the exception of adequate room for a helmet, the warts look easily handleable. |
Thread Tools | |
Display Modes | |
|
|