AeroElectric-List Digest Archive

Wed 09/13/06


Total Messages Posted: 24



Today's Message Index:
----------------------
 
     1. 05:18 AM - Re: Glowing Warning Lights (MikeEasley@aol.com)
     2. 05:52 AM - Re: Fuel Pump Switch(es) (Gary Casey)
     3. 06:17 AM - Re: Fuel Pump Switch(es) (gordon or marge)
     4. 06:17 AM - Re: Fuel Pump Switch(es) (Bill Denton)
     5. 06:47 AM - Re: Fuel Pump Switch(es) (Dave N6030X)
     6. 07:09 AM - Re: Fuel Pump Switch(es) (OldBob Siegfried)
     7. 07:31 AM - Re: Fuel Pump Switch(es) (Hinde, Frank George (Corvallis))
     8. 09:39 AM - Re: What I learned today (RV Builder (Michael Sausen))
     9. 10:11 AM - Re: What I learned today (Chuck Jensen)
    10. 10:21 AM - Radio shields (Dennis Jones)
    11. 01:00 PM - Re: What I learned today (Doug Windhorn)
    12. 01:47 PM - Re: What I learned today (Dj Merrill)
    13. 02:16 PM - Re: Radio shields (Brian Lloyd)
    14. 04:09 PM - Re: Glowing Warning Lights (Robert L. Nuckolls, III)
    15. 04:21 PM - Re: What I learned today (Robert L. Nuckolls, III)
    16. 04:22 PM - Re: Radio shields (Robert L. Nuckolls, III)
    17. 05:02 PM - Re: Fuel Pump Switch(es) (Kevin Horton)
    18. 06:11 PM - Transponders (Dennis Jones)
    19. 06:35 PM -  (Dennis Jones)
    20. 07:10 PM - Replacement led lights  (B Tomm)
    21. 07:20 PM - Re: Transponders (William Gill)
    22. 07:21 PM - Re: Re: John Deere PM alternator regulator (Ken)
    23. 07:21 PM - Re: alternator vs. second battery (Tony Gibson)
    24. 07:44 PM - Re: Transponders (Dennis Jones)
 
 
 


Message 1


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    Time: 05:18:53 AM PST US
    From: MikeEasley@aol.com
    Subject: Re: Glowing Warning Lights
    After studying the schematic (I'm a little slow with this stuff), it appears that the resistors can be installed at the regulator, one across terminals 3 and 5, and the other in series from the wire running from terminal 5 to the LED. I'm assuming some heat will be generated by the resistors and installing them at the regular would work better for me with cooling. One other question, why not use a relay? I understand the added complexity issue, but that would give you a dark LED without sacrificing any brightness when it's illuminated. Right? Any part number recommendations would be appreciated. Mike Easley Colorado Springs Lancair ES


    Message 2


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    Time: 05:52:12 AM PST US
    From: Gary Casey <glcasey@adelphia.net>
    Subject: Re: Fuel Pump Switch(es)
    Yes, there are still a number of failure modes that could create a problem, even with two independent fuel valves. In the case mentioned below, the low tank valve breaks and won't shut off. In that case the (presumably fuller) tank could be turned on, feeding fuel from both tanks and the plane landed at the earliest convenience. The fuller tank would probably back-feed into the lower tank, extending the range compared to just feeding off the lowest tank, depending on the level of fuel in the fuller tank. In any event one has to assume there is only the fuel left in the lowest tank. If the valve for the "new" tank failed to open (broke in the closed position) the response is simple - land before the low tank goes empty. Not a perfect condition, but there are still options available that might not be available with a single valve. If a single valve broke in the "low" tank position fuel in the fuller tank is completely unavailable. If it sticks and breaks between tanks (what I think is a more likely failure) neither tank is available and the engine quits right away. The normal operating procedure with two valves is to open the valve for the new tank, confirming that it actually moved, and then shutting off the valve from the old tank. Never shut the old one off before turning the new one on. Also, I know that there have been some postings advocating, or at least acknowledging, running a tank dry as a routine operating mode. I suppose if there were more than two tanks this isn't so bad, but with only two tanks doing that gives up one of the redundancies in the system - two independent sources of fuel. I personally don't like the idea of running a tank dry. My own standard is to never run either tank lower than what is required to get to the nearest airport. FWIW. Gary Casey Lancair ES On Sep 12, 2006, at 11:55 PM, AeroElectric-List Digest Server wrote: > > You are worried about fuel valve handles breaking. With your design, > what happens if you have run one tank down low, want to switch to the > other tank, and the valve handle on the tank that is feeding breaks > so you can't close that valve? Won't the engine quit once that tank > is empty and the engine starts sucking air? How is this better than > a valve handle failure with the normal design? > > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada


    Message 3


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    Time: 06:17:26 AM PST US
    From: "gordon or marge" <gcomfo@tc3net.com>
    Subject: Fuel Pump Switch(es)
    -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Gary Casey Sent: Tuesday, September 12, 2006 9:16 AM Subject: Re: AeroElectric-List: Fuel Pump Switch(es) I might have missed some of the discussion, but the comment below seems to be directed at the tank valving method - specifically whether to use two separate fuel valves or one, with the recommendation to run all the fuel through one valve. I chose to put two valves on mine for the following reasons: 1. A single valve is a single point of failure - what if the handle breaks off or the valve sticks? The most likely time for that to happen is when one port is being closed off before the other opens (apparently most or all fuel selectors go to "off" between right and left positions). If it jams in this position all fuel is shut off. My on-off valves are completely independent and controlled from their own lever and cable. If one jams either open or shut the other is unaffected. 2. The fuel can be shut off at the tank, not in the middle of the cockpit. When both valves are shut off no fuel can enter the cockpit, which would be reassuring in case of an off-airport landing. 3. It reduces the number of fuel fittings and therefore the number of potential leak paths, especially in the cockpit. 4. It allows the backup electric pump to be placed at the lowest point in the fuel system which should provide the best protection against vapor lock. 5. When switching tanks the new tank can be turned on before the old tank is shut off, guaranteeing a continuous flow of fuel. 6. A trivial one: If the plane is landed with an unbalanced fuel load, both valves can be left on, equalizing the fuel load before the next flight. The disadvantage is that both valves could be inadvertently turned on, which on a low-wing plane means that if one tank is run dry in that condition the engine could draw air. In that case one fuel gage would read empty and changing the fuel valve positions (shutting off the empty tank) would correct the condition. Interestingly, my DAR was skeptical about the arrangement, but was satisfied by the placement of a placard "continuous operation on both tanks prohibited." Conversely, my test pilot like the arrangement, saying that for at least the first half tank the engine could be operated on both, keeping the fuel load balanced (well, anyone that has had a Cardinal would not be convinced that would happen). Why do high-wing planes often have a "both" position? Probably because the fuel is joined together at the bottom of the plane, several feet below the tanks. One tank would have to run dry with the other pulling enough vacuum to overcome maybe 4 feet of head pressure - very unlikely. A low wing plane has nowhere to connect the tanks together except essentially even with the bottom of the tanks. When one runs dry air would immediately enter the engine. Just my nickel's worth (inflation, you know) Gary Casey Gary: With regard to your point 1); Anything is posssible but a Cessna valve (large single engine) uses a cam to lift check balls from their seats. Unlikely to seize. Point 2); good. Point 3); I count the same number of fittings. Point 4); Not sure. My -4 pump is not at the low point and there has been no trouble. My -8 will have a Weldon pump which has good suction capabilities. Point 5); The plane would have to be level and such an act would obscure your knowledge of fuel used from each tank. I prefer to know that if, for example, if I've used an hour of fuel from a tank that it stays that way. As to operating on both for the initial part of the flight, my experience with the -4 is that when operating in a "both" position one tank will deliver fuel to the other and if it becomes full the surplus goes overboard. At this point we reallly don't know our fuel state. The only airplane I've flown with 2 shutoff valves is a Fairchild 24 and we did not fly with both valves open although I never experimented with both on so don't really know what implications there might be. These are good discussions about non trivial matters. A look at the early Venture fuel system is enough to give you the willies. Gordon Comfort N363GC


    Message 4


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    Time: 06:17:26 AM PST US
    From: "Bill Denton" <bdenton@bdenton.com>
    Subject: Fuel Pump Switch(es)
    Just an observation... While you're sitting there with your head down troubleshooting valves and breaking the handles off and flipping switches until they fall out of the panel, you may well end up sticking your airplane in the ground. I know that it is sometimes necessary to have multiple tanks, valves, and pumps to manage complex fuel systems. But some of what I've been reading on this thread sounds like it's coming from graduates of the Rube Goldberg School of Engineering... -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com]On Behalf Of Gary Casey Sent: Wednesday, September 13, 2006 7:51 AM Subject: Re: AeroElectric-List: Fuel Pump Switch(es) Yes, there are still a number of failure modes that could create a problem, even with two independent fuel valves. In the case mentioned below, the low tank valve breaks and won't shut off. In that case the (presumably fuller) tank could be turned on, feeding fuel from both tanks and the plane landed at the earliest convenience. The fuller tank would probably back-feed into the lower tank, extending the range compared to just feeding off the lowest tank, depending on the level of fuel in the fuller tank. In any event one has to assume there is only the fuel left in the lowest tank. If the valve for the "new" tank failed to open (broke in the closed position) the response is simple - land before the low tank goes empty. Not a perfect condition, but there are still options available that might not be available with a single valve. If a single valve broke in the "low" tank position fuel in the fuller tank is completely unavailable. If it sticks and breaks between tanks (what I think is a more likely failure) neither tank is available and the engine quits right away. The normal operating procedure with two valves is to open the valve for the new tank, confirming that it actually moved, and then shutting off the valve from the old tank. Never shut the old one off before turning the new one on. Also, I know that there have been some postings advocating, or at least acknowledging, running a tank dry as a routine operating mode. I suppose if there were more than two tanks this isn't so bad, but with only two tanks doing that gives up one of the redundancies in the system - two independent sources of fuel. I personally don't like the idea of running a tank dry. My own standard is to never run either tank lower than what is required to get to the nearest airport. FWIW. Gary Casey Lancair ES On Sep 12, 2006, at 11:55 PM, AeroElectric-List Digest Server wrote: You are worried about fuel valve handles breaking. With your design, what happens if you have run one tank down low, want to switch to the other tank, and the valve handle on the tank that is feeding breaks so you can't close that valve? Won't the engine quit once that tank is empty and the engine starts sucking air? How is this better than a valve handle failure with the normal design? Kevin Horton RV-8 (finishing kit) Ottawa, Canada


    Message 5


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    Time: 06:47:53 AM PST US
    From: Dave N6030X <N6030X@DaveMorris.com>
    Subject: Re: Fuel Pump Switch(es)
    --> AeroElectric-List message posted by: Dave N6030X <N6030X@DaveMorris.com> I have a little different point of view that I'd like to just throw out there. In my experimental Dragonfly, I was gripped for a long time by a NASA-like desire to have multiple redundant systems everywhere. I'm a software guy, so I love complicated, microprocessor-controlled everythingies. But when I started working through the cockpit workload part of dealing with multiple independent pumps and switches and bypasses for everything and backup this and that, I realized that there was a single point of failure that was getting more and more overloaded with every new complexity: the pilot (me). Look at the NTSB reports, and you'll see there are many more failures of the human to throw the switch than of the switch breaking. Fuel Starvation due to forgetting how much fuel is in the tank, not knowing how much fuel is in the tank, forgetting to switch tanks, taking off without adequate fuel, etc. etc. I don't remember seeing too many "the fuel selector handle broke off between tanks". The oldest airplanes still flying anywhere (the survivors of all our human failures) have the simplest systems. Take a look at how they did things. My advice, which could be worth exactly as much as you're paying for it is this: build it light, build it high quality, and build it simple enough that you can intuitively grasp it without schematic diagrams and lengthy troubleshooting charts while handling an inflight emergency. If you have requirements such as "don't ever turn off this tank before turning on that tank", I think you're starting to set yourself up for failure. Think Gravity Feed from a header tank wherever possible. Instead of buying two redundant valves and plumbing, buy one high quality valve and replace it every 2 years just for the helluvit. What's that gonna cost you? A hundred bucks? How much weight will you save, and how much cockpit workload? When you're doing your failure mode analysis, include a list of all of the things the pilot has an opportunity to do wrong. We try to do this in software development, and it's a useful exercise before you get carried away anticipating equipment failures that are just never going to occur. When designing software, we no longer worry about whether there will be a bit error on the memory board, or whether the disk drive will crash a track. But we spend a lot of time worrying about whether the user will forget to enter a value or will enter the wrong value. If the user (pilot) CAN do anything wrong, he WILL. Try applying that to your aircraft design and see if you come up with some interesting scenarios you had not thought of before. Dave Morris 1960 Mooney M20A Manual gear retract 3 fuel tanks - single valve No fuel system failures in 46 years (knock on wood wing) At 07:51 AM 9/13/2006, you wrote: >Yes, there are still a number of failure modes that could create a >problem, even with two independent fuel valves. In the case >mentioned below, the low tank valve breaks and won't shut off. In >that case the (presumably fuller) tank could be turned on, feeding >fuel from both tanks and the plane landed at the earliest >convenience. The fuller tank would probably back-feed into the >lower tank, extending the range compared to just feeding off the >lowest tank, depending on the level of fuel in the fuller tank. In >any event one has to assume there is only the fuel left in the >lowest tank. If the valve for the "new" tank failed to open (broke >in the closed position) the response is simple - land before the low >tank goes empty. Not a perfect condition, but there are still >options available that might not be available with a single >valve. If a single valve broke in the "low" tank position fuel in >the fuller tank is completely unavailable. If it sticks and breaks >between tanks (what I think is a more likely failure) neither tank >is available and the engine quits right away. The normal operating >procedure with two valves is to open the valve for the new tank, >confirming that it actually moved, and then shutting off the valve >from the old tank. Never shut the old one off before turning the >new one on. Also, I know that there have been some postings >advocating, or at least acknowledging, running a tank dry as a >routine operating mode. I suppose if there were more than two tanks >this isn't so bad, but with only two tanks doing that gives up one >of the redundancies in the system - two independent sources of >fuel. I personally don't like the idea of running a tank dry. My >own standard is to never run either tank lower than what is required >to get to the nearest airport. FWIW. > >Gary Casey >Lancair ES >On Sep 12, 2006, at 11:55 PM, AeroElectric-List Digest Server wrote: > > >> >>You are worried about fuel valve handles breaking. With your design, >> >>what happens if you have run one tank down low, want to switch to the >> >>other tank, and the valve handle on the tank that is feeding breaks >> >>so you can't close that valve? Won't the engine quit once that tank >> >>is empty and the engine starts sucking air? How is this better than >> >>a valve handle failure with the normal design? >> >> >>Kevin Horton RV-8 (finishing kit) >> >>Ottawa, Canada > >


    Message 6


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    Time: 07:09:49 AM PST US
    From: OldBob Siegfried <oldbob@BeechOwners.com>
    Subject: Re: Fuel Pump Switch(es)
    --> AeroElectric-List message posted by: OldBob Siegfried <oldbob@beechowners.com> Good Morning Dave, I recognize that this message is really a "Me Too" message and that such messages are discouraged by the list administrator, but I can't help myself! You have mashed that nail very squarely. I am convinced that any system failure is much likely to be one induced by "yours truly" rather than by any failure of the mechanism of my flying machine. KISS Do Not Archive. Happy Skies, Old Bob AKA Bob Siegfried Stearman N3977A Downers Grove Illinois LL22 --- Dave N6030X <N6030X@DaveMorris.com> wrote: > --> AeroElectric-List message posted by: Dave N6030X > <N6030X@DaveMorris.com> > > I have a little different point of view that I'd > like to just throw out there. > > In my experimental Dragonfly, I was gripped for a > long time by a > NASA-like desire to have multiple redundant systems > everywhere. I'm > a software guy, so I love complicated, > microprocessor-controlled > everythingies. But when I started working through > the cockpit > workload part of dealing with multiple independent > pumps and switches > and bypasses for everything and backup this and > that, I realized that > there was a single point of failure that was getting > more and more > overloaded with every new complexity: the pilot > (me). > > Look at the NTSB reports, and you'll see there are > many more failures > of the human to throw the switch than of the switch > breaking. Fuel > Starvation due to forgetting how much fuel is in the > tank, not > knowing how much fuel is in the tank, forgetting to > switch tanks, > taking off without adequate fuel, etc. etc. I don't > remember seeing > too many "the fuel selector handle broke off between > tanks". The > oldest airplanes still flying anywhere (the > survivors of all our > human failures) have the simplest systems. Take a > look at how they did things. > > My advice, which could be worth exactly as much as > you're paying for > it is this: build it light, build it high quality, > and build it > simple enough that you can intuitively grasp it > without schematic > diagrams and lengthy troubleshooting charts while > handling an > inflight emergency. If you have requirements such > as "don't ever > turn off this tank before turning on that tank", I > think you're > starting to set yourself up for failure. Think > Gravity Feed from a > header tank wherever possible. Instead of buying > two redundant > valves and plumbing, buy one high quality valve and > replace it every > 2 years just for the helluvit. What's that gonna > cost you? A > hundred bucks? How much weight will you save, and > how much cockpit workload? > > When you're doing your failure mode analysis, > include a list of all > of the things the pilot has an opportunity to do > wrong. We try to do > this in software development, and it's a useful > exercise before you > get carried away anticipating equipment failures > that are just never > going to occur. When designing software, we no > longer worry about > whether there will be a bit error on the memory > board, or whether the > disk drive will crash a track. But we spend a lot > of time worrying > about whether the user will forget to enter a value > or will enter the > wrong value. If the user (pilot) CAN do anything > wrong, he > WILL. Try applying that to your aircraft design and > see if you come > up with some interesting scenarios you had not > thought of before. > > Dave Morris > 1960 Mooney M20A > Manual gear retract > 3 fuel tanks - single valve > No fuel system failures in 46 years (knock on wood > wing) > > > At 07:51 AM 9/13/2006, you wrote: > >Yes, there are still a number of failure modes that > could create a > >problem, even with two independent fuel valves. In > the case > >mentioned below, the low tank valve breaks and > won't shut off. In > >that case the (presumably fuller) tank could be > turned on, feeding > >fuel from both tanks and the plane landed at the > earliest > >convenience. The fuller tank would probably > back-feed into the > >lower tank, extending the range compared to just > feeding off the > >lowest tank, depending on the level of fuel in the > fuller tank. In > >any event one has to assume there is only the fuel > left in the > >lowest tank. If the valve for the "new" tank > failed to open (broke > >in the closed position) the response is simple - > land before the low > >tank goes empty. Not a perfect condition, but > there are still > >options available that might not be available with > a single > >valve. If a single valve broke in the "low" tank > position fuel in > >the fuller tank is completely unavailable. If it > sticks and breaks > >between tanks (what I think is a more likely > failure) neither tank > >is available and the engine quits right away. The > normal operating > >procedure with two valves is to open the valve for > the new tank, > >confirming that it actually moved, and then > shutting off the valve > >from the old tank. Never shut the old one off > before turning the > >new one on. Also, I know that there have been some > postings > >advocating, or at least acknowledging, running a > tank dry as a > >routine operating mode. I suppose if there were > more than two tanks > >this isn't so bad, but with only two tanks doing > that gives up one > >of the redundancies in the system - two independent > sources of > >fuel. I personally don't like the idea of running > a tank dry. My > >own standard is to never run either tank lower than > what is required > >to get to the nearest airport. FWIW. > > > >Gary Casey > >Lancair ES > >On Sep 12, 2006, at 11:55 PM, AeroElectric-List > Digest Server wrote: > > > > > >> > >>You are worried about fuel valve handles breaking. > With your design, > >> > >>what happens if you have run one tank down low, > want to switch to the > >> > >>other tank, and the valve handle on the tank that > is feeding breaks > >> > >>so you can't close that valve? Won't the engine > quit once that tank > >> > >>is empty and the engine starts sucking air? How > is this better than > >> > >>a valve handle failure with the normal design? > >> > >> > >>Kevin Horton RV-8 (finishing kit) > >> > >>Ottawa, Canada > > > > > > > > > > browse > Subscriptions page, > FAQ, > http://www.matronics.com/Navigator?AeroElectric-List > > Web Forums! > === message truncated ==


    Message 7


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    Time: 07:31:22 AM PST US
    Subject: Fuel Pump Switch(es)
    From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com>
    --> AeroElectric-List message posted by: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> Exactly! And now back to the one pump in each wingroot solution....left tank ...switch left pump on...Right tank switch right pump on... Both tanks (TO and landing).. Both switches on. Pretty simple I think. The other advantages are... No selector valves to switch. Highly resistant to Vapour lock...Biggest driver to use auto fuel SIMPLE No single point of failure anywhere...OK the fuel line, servo and battery is (assuming you don't have an isolated twin battery setup) Plug a fuel filter...Who cares? Downsides Uses more electrical power. Have to design the "what happens if the alternator craps out" failure mode...I have dual alternaors...8 amp back up is just big enough for a radio, tansponder and one fuel pump Extra 3 feet of pressurised fuel line in the cockpit. Frank RV7a 4 hours -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Dave N6030X Sent: Wednesday, September 13, 2006 6:45 AM Subject: Re: AeroElectric-List: Fuel Pump Switch(es) --> AeroElectric-List message posted by: Dave N6030X --> <N6030X@DaveMorris.com> I have a little different point of view that I'd like to just throw out there. In my experimental Dragonfly, I was gripped for a long time by a NASA-like desire to have multiple redundant systems everywhere. I'm a software guy, so I love complicated, microprocessor-controlled everythingies. But when I started working through the cockpit workload part of dealing with multiple independent pumps and switches and bypasses for everything and backup this and that, I realized that there was a single point of failure that was getting more and more overloaded with every new complexity: the pilot (me). Look at the NTSB reports, and you'll see there are many more failures of the human to throw the switch than of the switch breaking. Fuel Starvation due to forgetting how much fuel is in the tank, not knowing how much fuel is in the tank,


    Message 8


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    Time: 09:39:12 AM PST US
    Subject: What I learned today
    From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net>
    --> AeroElectric-List message posted by: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net> You want this to be a list of the people, so to speak, so here is my question. Out of curiosity what is the actual percentage of requests to ban George over the entire list membership? Is this another case of the vocal minority winning out over the silent majority? I for one think George, Paul, and others add value even if it is veiled in a load of rhetoric and even BS sometimes. Some of the most brilliant people in history had social issues. When I smell something funny in a post I always have the option of exercising the delete key. Honestly I spend more time deleting posts of complaints about other people than I do of the actual people. Talk about circular arguments. One of the problems with email has always been the way a person interprets emotions in the writing. Most of the time people are wrong in their assumptions so it is better to take emotion out and look for the actual substance of a post. Less bruised egos and useless replies that only escalate a situation that probably didn't exist in the first place. My $0.02 Michael Sausen -10 #352 Fuselage Oh yes, and unlike most of the other posts on this subject.... Do Not Archive -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, September 06, 2006 8:11 AM Subject: AeroElectric-List: What I learned today --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" --> <nuckollsr@cox.net> Listers, Folks have been bugging me about George for some time. Over a year perhaps. They keep citing this venue as being my list and suggested that I have full authority to manage it in whatever way I want. I never wanted to view this as "my list". It's always been my fondest wish that the AeroElectric List be a joint venture, a quest for the best-we-know-how-to-do. On the other hand, I cannot tolerate circular arguments that perpetually hat-dance around the simple-ideas while confusing or misleading those who come here for practical advice. I guess I could treat this more like a university job. It's not my building but it is my classroom. A good teacher must be open to consider every idea but with absolute control over classroom decorum and a bulwark against bad science and individuals who disrupt what should be a calm, considered sifting of the simple-ideas. I might liken this effort to that of accident investigator. The real work begins after the fire trucks, ambulances and distraught individuals have left. I've had several occasions where folks who witnessed or were involved in an accident came over to see what I was doing and conversationally relive the events from their perspective. This was always distracting and never yielded useful information. I never asked any of those folks to leave . . . after all, the space we shared wasn't my personal property. In retrospect I'm coming to understand that "space" comes in many forms and just because someone has a fundamental right to co exist with us in a physical space doesn't give them a right to invade (and stir up trouble) in folk's intellectual space. I promise not to allow such situations to carry on so long again. We all have better ways to invest our most precious commodity, time. Thank you all for your understanding and support of the AeroElectric List mission. I learn from the List every day and I believe it to be a powerful tool for advancing the state of our art and science in crafting the best airplanes to have ever flown. Bob . . . --------------------------------------------------------- < What is so wonderful about scientific truth...is that > < the authority which determines whether there can be > < debate or not does not reside in some fraternity of > < scientists; nor is it divine. The authority rests > < with experiment. > < --Lawrence M. Krauss > ---------------------------------------------------------


    Message 9


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    Time: 10:11:07 AM PST US
    Subject: What I learned today
    From: "Chuck Jensen" <cjensen@dts9000.com>
    --> AeroElectric-List message posted by: "Chuck Jensen" <cjensen@dts9000.com> Good point, Michael. I rarely ever use the delete key. Even when Georges posts one of his long tirades that is obviously a pile of horse s..t, I always dig through it thinking there might be a pony in there somewhere. Chuck Jensen Do Not Archive > -----Original Message----- > From: owner-aeroelectric-list-server@matronics.com > [mailto:owner-aeroelectric-list-server@matronics.com] On > Behalf Of RV Builder (Michael Sausen) > Sent: Wednesday, September 13, 2006 12:37 PM > To: aeroelectric-list@matronics.com > Subject: RE: AeroElectric-List: What I learned today > > > --> AeroElectric-List message posted by: "RV Builder (Michael > Sausen)" > --> <rvbuilder@sausen.net> > > You want this to be a list of the people, so to speak, so > here is my question. Out of curiosity what is the actual > percentage of requests to ban George over the entire list > membership? Is this another case of the vocal minority > winning out over the silent majority? > > I for one think George, Paul, and others add value even if > it is veiled in a load of rhetoric and even BS sometimes. > Some of the most brilliant people in history had social > issues. When I smell something funny in a post I always have > the option of exercising the delete key. Honestly I spend > more time deleting posts of complaints about other people > than I do of the actual people. Talk about circular arguments. > > One of the problems with email has always been the way a > person interprets emotions in the writing. Most of the time > people are wrong in their assumptions so it is better to take > emotion out and look for the actual substance of a post. > Less bruised egos and useless replies that only escalate a > situation that probably didn't exist in the first place. > > My $0.02 > > Michael Sausen > -10 #352 Fuselage > > Oh yes, and unlike most of the other posts on this > subject.... Do Not Archive > > -----Original Message----- > From: owner-aeroelectric-list-server@matronics.com > [mailto:owner-aeroelectric-list-server@matronics.com] On > Behalf Of Robert L. Nuckolls, III > Sent: Wednesday, September 06, 2006 8:11 AM > To: aeroelectric-list@matronics.com > Subject: AeroElectric-List: What I learned today > > --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" > --> <nuckollsr@cox.net> > > Listers, > > Folks have been bugging me about George for some time. > Over a year perhaps. They keep citing this venue as being my > list and suggested that I have full authority to manage it in > whatever way I want. > > I never wanted to view this as "my list". It's always been my > fondest wish that the AeroElectric List be a joint venture, a > quest for the best-we-know-how-to-do. On the other hand, I > cannot tolerate circular arguments that perpetually hat-dance > around the simple-ideas while confusing or misleading those > who come here for practical advice. > > I guess I could treat this more like a university job. > It's not my building but it is my classroom. A good teacher > must be open to consider every idea but with absolute control > over classroom decorum and a bulwark against bad science and > individuals who disrupt what should be a calm, considered > sifting of the simple-ideas. > > I might liken this effort to that of accident investigator. > The real work begins after the fire trucks, ambulances and > distraught individuals have left. I've had several occasions > where folks who witnessed or were involved in an accident > came over to see what I was doing and conversationally relive > the events from their perspective. This was always > distracting and never yielded useful information. I never > asked any of those folks to leave . . . after all, the space > we shared wasn't my personal property. > > In retrospect I'm coming to understand that "space" > comes in many forms and just because someone has a > fundamental right to co exist with us in a physical space > doesn't give them a right to invade (and stir up > trouble) in folk's intellectual space. I promise not to allow > such situations to carry on so long again. We all have better > ways to invest our most precious commodity, time. > > Thank you all for your understanding and support of the > AeroElectric List mission. I learn from the List every day > and I believe it to be a powerful tool for advancing the > state of our art and science in crafting the best airplanes > to have ever flown. > > > Bob . . . > > > --------------------------------------------------------- > < What is so wonderful about scientific truth...is that > > < the authority which determines whether there can be > > < debate or not does not reside in some fraternity of > > < scientists; nor is it divine. The authority rests > > < with experiment. > > < --Lawrence M. Krauss > > --------------------------------------------------------- > > > > > > > > > > >


    Message 10


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    Time: 10:21:21 AM PST US
    From: "Dennis Jones" <djones@northboone.net>
    Subject: Radio shields
    I'm wiring the harness for a Terra TX-760D radio. My question is the interconnect diagram shows the shield for the mic. audio, mic. key and the headphone attach to the ground. I plan on using the daisy chain system shown by Bob, however I'm confused about the shields connecting into the ground wire itself or do they connect to the shield of the ground wire? Dennis


    Message 11


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    Time: 01:00:23 PM PST US
    From: "Doug Windhorn" <N1DeltaWhiskey@comcast.net>
    Subject: Re: What I learned today
    --> AeroElectric-List message posted by: "Doug Windhorn" <N1DeltaWhiskey@comcast.net> Michael, I agree with your last paragraph. Of course, one way to handle the situation is to not post messages when on has an emotional response. Both of these gentlemen seem to have a difficult time doing that. We should also recognize that Bob sometimes contributes to these ongoing threads by taking up the challenges posed by these two individuals (I recognize he feels a need to do so to keep misinformation or poor quality from getting a hold). It takes two to have an argument. IMHO, all could benefit from some marshal arts training to learn how to brush off challenging posts. For laughs, I checked messages that I have saved that I thought might be useful down the road sometime. I have counted 3 from George and a dozen or so from Paul off this list that I thought might fit that category; that is from more than 400 saves. So for all of their postings, and certainly by word count, I think almost anyone on this list has a higher percentage of worthwhile content than do either George or Paul. Also, given the fact that their postings are often lengthy it takes a lot of time to get through them - not good value. Not sure that I will miss what might have been future postings, but not sure they should be banned (wrong word - they have been told to lay off) either. My $0.01 worth. Doug Windhorn P.S. Now, my pet peeve. My browser opens a message at the top. If one has important something to say, post it at the top of the message, not the bottom (I probably have already read the prior messages, that the meaty content is the resolution of a thread - why should I have to wade through all the other stuff to get to the conclusion?) Exception: when responding to several subjects with embedded comments, that is OK, but say you are doing that at the top. ----- Original Message ----- From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net> Sent: Wednesday, 13 September, 2006 9:36 Subject: RE: AeroElectric-List: What I learned today > --> AeroElectric-List message posted by: "RV Builder (Michael Sausen)" > <rvbuilder@sausen.net> > > You want this to be a list of the people, so to speak, so here is my > question. Out of curiosity what is the actual percentage of requests to > ban George over the entire list membership? Is this another case of the > vocal minority winning out over the silent majority? > > I for one think George, Paul, and others add value even if it is > veiled in a load of rhetoric and even BS sometimes. Some of the most > brilliant people in history had social issues. When I smell something > funny in a post I always have the option of exercising the delete key. > Honestly I spend more time deleting posts of complaints about other > people than I do of the actual people. Talk about circular arguments. > > One of the problems with email has always been the way a person > interprets emotions in the writing. Most of the time people are wrong > in their assumptions so it is better to take emotion out and look for > the actual substance of a post. Less bruised egos and useless replies > that only escalate a situation that probably didn't exist in the first > place. > > My $0.02 > > Michael Sausen > -10 #352 Fuselage > > Oh yes, and unlike most of the other posts on this subject.... Do Not > Archive > > -----Original Message----- > From: owner-aeroelectric-list-server@matronics.com > [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of > Robert L. Nuckolls, III > Sent: Wednesday, September 06, 2006 8:11 AM > To: aeroelectric-list@matronics.com > Subject: AeroElectric-List: What I learned today > > --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" > --> <nuckollsr@cox.net> > > Listers, > > Folks have been bugging me about George for some time. > Over a year perhaps. They keep citing this venue as being my list and > suggested that I have full authority to manage it in whatever way I > want. > > I never wanted to view this as "my list". It's always been my fondest > wish that the AeroElectric List be a joint venture, a quest for the > best-we-know-how-to-do. On the other hand, I cannot tolerate circular > arguments that perpetually hat-dance around the simple-ideas while > confusing or misleading those who come here for practical advice. > > I guess I could treat this more like a university job. > It's not my building but it is my classroom. A good teacher must be open > to consider every idea but with absolute control over classroom decorum > and a bulwark against bad science and individuals who disrupt what > should be a calm, considered sifting of the simple-ideas. > > I might liken this effort to that of accident investigator. > The real work begins after the fire trucks, ambulances and distraught > individuals have left. I've had several occasions where folks who > witnessed or were involved in an accident came over to see what I was > doing and conversationally relive the events from their perspective. > This was always distracting and never yielded useful information. I > never asked any of those folks to leave . . . > after all, the space we shared wasn't my personal property. > > In retrospect I'm coming to understand that "space" > comes in many forms and just because someone has a fundamental right to > co exist with us in a physical space doesn't give them a right to invade > (and stir up > trouble) in folk's intellectual space. I promise not to allow such > situations to carry on so long again. > We all have better ways to invest our most precious commodity, time. > > Thank you all for your understanding and support of the AeroElectric > List mission. I learn from the List every day and I believe it to be a > powerful tool for advancing the state of our art and science in crafting > the best airplanes to have ever flown. > > > Bob . . . > > > --------------------------------------------------------- > < What is so wonderful about scientific truth...is that > > < the authority which determines whether there can be > > < debate or not does not reside in some fraternity of > > < scientists; nor is it divine. The authority rests > > < with experiment. > > < --Lawrence M. Krauss > > --------------------------------------------------------- > > >


    Message 12


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    Time: 01:47:36 PM PST US
    Subject: Re: What I learned today
    From: Dj Merrill <deej@deej.net>
    --> AeroElectric-List message posted by: Dj Merrill <deej@deej.net> Doug Windhorn wrote: > > > P.S. Now, my pet peeve. My browser opens a message at the top. If > one has important something to say, post it at the top of the message, > not the bottom (I probably have already read the prior messages, that > the meaty content is the resolution of a thread - why should I have to > wade through all the other stuff to get to the conclusion?) > Exception: when responding to several subjects with embedded comments, > that is OK, but say you are doing that at the top. Hi Doug, As a counter, my pet peeve is when people post things at the top... *grin* My brain processes things easier when it is laid out in order, from top to bottom, and I like to have the context of the previous messages listed out before the replies, which makes things MUCH easier to understand when going back to reference that saved e-mail, or when reading through the archives. Reading from bottom to top tends to get very confusing... So, there are two sides to every coin, I guess. :-) -Dj do not archive -- Dj Merrill - N1JOV Glastar Sportsman 2+2 Builder #7118 http://econ.duke.edu/~deej/sportsman/ "Many things that are unexplainable happen during the construction of an airplane." --Dave Prizio, 30 Aug 2005


    Message 13


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    Time: 02:16:47 PM PST US
    Subject: Re: Radio shields
    From: Brian Lloyd <brian-av@lloyd.com>
    --> AeroElectric-List message posted by: Brian Lloyd <brian-av@lloyd.com> rOn Wed, 2006-09-13 at 10:12, Dennis Jones wrote: > I?m wiring the harness for a Terra TX-760D radio. My question is the > interconnect diagram shows the shield for the mic. audio, mic. key and > the headphone attach to the ground. I plan on using the daisy chain > system shown by Bob, however I?m confused about the shields connecting > into the ground wire itself or do they connect to the shield of the > ground wire? If the radio itself has separate sheild and ground connections (most don't) then you would connect the shield and ground to their respective connections. Most radios just have a ground connection so both the shield and the ground wire (if they are separate) should connect to the ground pin(s) at the radio. Normally I would run separate wire for mic/ptt and headphone. Speaking specifically of the mic/ptt wiring, you can use the shield of the mic cable as your mic and ptt ground wiring if you wish. If your mic wiring has three conductors plus shield, I would probably use one conductor for ground and then not attach anything to the shield (except at the radio). If you are using an intercom you will probably have separate mic/ptt wiring for each mic jack. (Most intercoms provide mic isolation when you hit the PTT for one mic, the other mics are muted to keep noise from getting into the transmit audio.) If you are not using an intercom then you may daisy-chain your mic and PTT connections. Just continue ground, shield, PTT, and mic hot. Whatever you choose to do be sure you insulate the mic jacks from the airframe. Headphone wiring does not need to be shielded. I would use twisted pair. You can get away with using airframe ground for the ground side of your headphone but you are more likely to get some noise pick-up. This may become objectionable if you are trying to have high-fidelity audio. Best to insulate the headphone jacks as well. Brian Lloyd


    Message 14


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    Time: 04:09:31 PM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Glowing Warning Lights
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 08:16 AM 9/13/2006 -0400, you wrote: >After studying the schematic (I'm a little slow with this stuff), it >appears that the resistors can be installed at the regulator, one across >terminals 3 and 5, and the other in series from the wire running from >terminal 5 to the LED. Look at it again. The two resistors would go in series between 3 and 5 and the LED fed from the protected end of the fuse and the TAP BETWEEN the two resistors. > I'm assuming some heat will be generated by the resistors and > installing them at the regular would work better for me with cooling. The RECOMMENDED resistors are at least 1/2 watt and 1 watt is preferred. Like the selection of 1N540X series diodes over 1N400X series is their mechanical robustness. The actual power dissipated in the 220 watt series resistor is about 11(squared)/220 = 550 milliwatts which is divided in two again due to the approx 50% duty cycle of the flashing lamp. So heating is an insignificant concern. > >One other question, why not use a relay? I understand the added >complexity issue, but that would give you a dark LED without sacrificing >any brightness when it's illuminated. Right? Any part number >recommendations would be appreciated. LED's are current operated devices, the resistors don't sacrifice brightness, they prevent darkness by keeping the LED from being destroyed by using it to directly replace an incandescent lamp sans resistors. A relay would suffer from the same kinds of issues as a barefoot LED. Relays can be held closed by a tiny fraction of the current that it takes to energize it. Further, you would still need at least one of the two resistors to set the LED's operating current. Finally, relays are rated amongst the least reliable of components. It behoves us to limit their use where ever practical. Bob . . .


    Message 15


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    Time: 04:21:04 PM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: What I learned today
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 11:36 AM 9/13/2006 -0500, you wrote: >--> AeroElectric-List message posted by: "RV Builder (Michael Sausen)" ><rvbuilder@sausen.net> > > You want this to be a list of the people, so to speak, so here is my >question. Out of curiosity what is the actual percentage of requests to >ban George over the entire list membership? Is this another case of the >vocal minority winning out over the silent majority? This is not a democracy. The decision to ask George to leave was mine alone and I stand by it . . . his nugget/noise ratio was simply too low to invest any more time on it. Somebody asked for "a vote" but that was after I'd made the decision and no amount of voting one way or another would have altered it. > I for one think George, Paul, and others add value even if it is >veiled in a load of rhetoric and even BS sometimes. Some of the most >brilliant people in history had social issues. When I smell something >funny in a post I always have the option of exercising the delete key. >Honestly I spend more time deleting posts of complaints about other >people than I do of the actual people. Talk about circular arguments. > > One of the problems with email has always been the way a person >interprets emotions in the writing. Most of the time people are wrong >in their assumptions so it is better to take emotion out and look for >the actual substance of a post. Less bruised egos and useless replies >that only escalate a situation that probably didn't exist in the first >place. Words mean things. You may use them to inform, entertain, persuade or hurt. The fact that 5% of someone's words fall into the first two categories does not justify a toleration of 95% falling into the later categories. This is especially true when they hat-dance around the core issues of the discussion, never participate in the exploration and assembly of simple-ideas, and cannot lay foundation for persuasion masquerading as information. I've participated in many classrooms both up front and sitting in the chairs. It's a poor return on investment of time to sift through "noise" looking for "nuggets". I've left the chairs in a classroom where nugget/noise radio was poor. I have assumed responsibility for keeping those numbers high in this classroom. Assuming one has a common ground in the meaning of written words, then interpretation must be based on the words and not upon anyone's feelings about the words. If writers never use words intended to hurt, then a reader's feelings are his/her own problem. There's no duty on the part of a writer to assuage the reader's discomforts other than to clarify information. There is risk some folks are hurt by words others find "entertaining". Common sense is called for . . . it's easy for hurting words to masquerade as entertainment. Red Skelton and George Burns could entertain and hurt nobody. Much of what passes for entertainment today is overtly mean and exacts a toll on liberty of others. I try to start any conversation with a core belief that folks on the other end are looking for clear and useful info. They have every right to expect the best possible foundations be laid for anything I or anyone else has to offer. Anything outside this process is noise and should be minimized. Should the noise become overwhelming or hurtful, then polite termination is called for. Bob . . . DO NOT ARCHIVE


    Message 16


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    Time: 04:22:29 PM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Radio shields
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 12:12 PM 9/13/2006 -0500, you wrote: >I m wiring the harness for a Terra TX-760D radio. My question is the >interconnect diagram shows the shield for the mic. audio, mic. key and the >headphone attach to the ground. I plan on using the daisy chain system >shown by Bob, however I m confused about the shields connecting into the >ground wire itself or do they connect to the shield of the ground wire? Can you scan the wiring from the instruction manual and send it to me? It would be useful to see how they've depicted their suggestions for the installation. Bob . . . --------------------------------------------------------- < What is so wonderful about scientific truth...is that > < the authority which determines whether there can be > < debate or not does not reside in some fraternity of > < scientists; nor is it divine. The authority rests > < with experiment. > < --Lawrence M. Krauss > ---------------------------------------------------------


    Message 17


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    Time: 05:02:57 PM PST US
    From: Kevin Horton <khorton01@rogers.com>
    Subject: Re: Fuel Pump Switch(es)
    Fuel system problems are a major cause of engine stoppage in homebuilt aircraft. Any fuel system that deviates from the norm, in either design or installation details, opens the door to unexpected problems. You have made a bunch of assumptions on how the system will perform following various types of failures. It would be wise to validate those assumptions via actual tests, either on the ground, or in the air over a nice long runway. Kevin Horton On 13 Sep 2006, at 08:51, Gary Casey wrote: > Yes, there are still a number of failure modes that could create a > problem, even with two independent fuel valves. In the case > mentioned below, the low tank valve breaks and won't shut off. In > that case the (presumably fuller) tank could be turned on, feeding > fuel from both tanks and the plane landed at the earliest > convenience. The fuller tank would probably back-feed into the > lower tank, extending the range compared to just feeding off the > lowest tank, depending on the level of fuel in the fuller tank. In > any event one has to assume there is only the fuel left in the > lowest tank. If the valve for the "new" tank failed to open (broke > in the closed position) the response is simple - land before the > low tank goes empty. Not a perfect condition, but there are still > options available that might not be available with a single valve. > If a single valve broke in the "low" tank position fuel in the > fuller tank is completely unavailable. If it sticks and breaks > between tanks (what I think is a more likely failure) neither tank > is available and the engine quits right away. The normal operating > procedure with two valves is to open the valve for the new tank, > confirming that it actually moved, and then shutting off the valve > from the old tank. Never shut the old one off before turning the > new one on. Also, I know that there have been some postings > advocating, or at least acknowledging, running a tank dry as a > routine operating mode. I suppose if there were more than two > tanks this isn't so bad, but with only two tanks doing that gives > up one of the redundancies in the system - two independent sources > of fuel. I personally don't like the idea of running a tank dry. > My own standard is to never run either tank lower than what is > required to get to the nearest airport. FWIW. > > Gary Casey > Lancair ES > On Sep 12, 2006, at 11:55 PM, AeroElectric-List Digest Server wrote: > > >> >> You are worried about fuel valve handles breaking. With your design, >> what happens if you have run one tank down low, want to switch to the >> other tank, and the valve handle on the tank that is feeding breaks >> so you can't close that valve? Won't the engine quit once that tank >> is empty and the engine starts sucking air? How is this better than >> a valve handle failure with the normal design? >> >> Kevin Horton RV-8 (finishing kit) >> Ottawa, Canada >


    Message 18


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    Time: 06:11:07 PM PST US
    From: "Dennis Jones" <djones@northboone.net>
    Subject: Transponders
    In a transponder what is considered suppression out and remote ground when used in the wire harness. Dennis


    Message 19


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    Time: 06:35:56 PM PST US
    From: "Dennis Jones" <djones@northboone.net>
    Subject:
    Bob Here is the drawings for the Terra 760-D in regards to dealing with the shields and grounds. Thanks Dennis


    Message 20


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    Time: 07:10:37 PM PST US
    From: "B Tomm" <fvalarm@rapidnet.net>
    Subject: Replacement led lights
    --> AeroElectric-List message posted by: "B Tomm" <fvalarm@rapidnet.net> Bob, Do you have a suggestion for a source for reasonably priced LED replacement bulbs for my non aircraft related project. T3-1/4 and T1-3/4 cases, 14 or 28V. Bevan RV7A finish kit -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, September 13, 2006 4:08 PM Subject: Re: AeroElectric-List: Glowing Warning Lights --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" --> <nuckollsr@cox.net> At 08:16 AM 9/13/2006 -0400, you wrote: >After studying the schematic (I'm a little slow with this stuff), it >appears that the resistors can be installed at the regulator, one >across terminals 3 and 5, and the other in series from the wire running >from terminal 5 to the LED. Look at it again. The two resistors would go in series between 3 and 5 and the LED fed from the protected end of the fuse and the TAP BETWEEN the two resistors. > I'm assuming some heat will be generated by the resistors and > installing them at the regular would work better for me with cooling. The RECOMMENDED resistors are at least 1/2 watt and 1 watt is preferred. Like the selection of 1N540X series diodes over 1N400X series is their mechanical robustness. The actual power dissipated in the 220 watt series resistor is about 11(squared)/220 = 550 milliwatts which is divided in two again due to the approx 50% duty cycle of the flashing lamp. So heating is an insignificant concern. > >One other question, why not use a relay? I understand the added >complexity issue, but that would give you a dark LED without >sacrificing any brightness when it's illuminated. Right? Any part >number recommendations would be appreciated. LED's are current operated devices, the resistors don't sacrifice brightness, they prevent darkness by keeping the LED from being destroyed by using it to directly replace an incandescent lamp sans resistors. A relay would suffer from the same kinds of issues as a barefoot LED. Relays can be held closed by a tiny fraction of the current that it takes to energize it. Further, you would still need at least one of the two resistors to set the LED's operating current. Finally, relays are rated amongst the least reliable of components. It behoves us to limit their use where ever practical. Bob . . .


    Message 21


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    Time: 07:20:52 PM PST US
    From: "William Gill" <wgill10@comcast.net>
    Subject: Transponders
    Hello Dennis, What brand of transponder are you dealing with? Bill -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Dennis Jones Sent: Wednesday, September 13, 2006 8:03 PM Subject: AeroElectric-List: Transponders In a transponder what is considered suppression out and remote ground when used in the wire harness. Dennis


    Message 22


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    Time: 07:21:51 PM PST US
    From: Ken <klehman@albedo.net>
    Subject: Re: John Deere PM alternator regulator
    --> AeroElectric-List message posted by: Ken <klehman@albedo.net> I can add one more interesting tidbit to this thread. Disconnecting the Battery wire from the failed regulator does NOT stop the overvoltage. I'm told it does stop the alternator output with a good regulator but it does not do that on this failed unit. Sounds similar to the automotive IR alternator where we also can not guarantee that disconnecting the IGN wire will stop the alternator output if the VR has already failed and is causing an overvoltage. Ken Dave N6030X wrote: > --> AeroElectric-List message posted by: Dave N6030X > <N6030X@DaveMorris.com> > > Many in the Corvair group (www.FlyCorvair.com) are using this same > John Deere generator/VR combo. You might take up the question there > and find out what people have witnessed. The guy who's probably flown > more hours with that combo than anybody is Gus Warren down at William > Wynne's hangar in Florida. > > Dave Morris


    Message 23


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    Time: 07:21:55 PM PST US
    From: Tony Gibson <umgibso1@yahoo.com>
    Subject: Re: alternator vs. second battery
    Thanx for the reply Ken, sounds like good advice! I'll take it! Tony From: Ken <klehman@albedo.net> Subject: Re: AeroElectric-List: Debating on an alternator or two batteries? --> AeroElectric-List message posted by: Ken <klehman@albedo.net> Hello Tony Personally with an electric dependant engine, I'd happily trade 4 lbs or so of battery for a small permanent magnet alternator and I suspect the alternator would be the lighter option if you have a few hours of fuel on board. Bob just posted some references on battery discharging that you will want to look at. For a primary battery with no alternator I'd suggest multiplying your hours of fuel by 2.5 amps and then picking a battery that can supply that (from its spec. sheet) and then doubling it. Another battery characteristic is that the deeper you discharge them, the fewer discharge - charge cycles they last so planning for a 50% discharge when the fuel runs out might be reasonable. That would also allow for other sub optimal conditions such as temperature. Ken Tony Gibson wrote: > Hi Group, my name's Tony Gibson, I've been a lurker on the list for > almost a year now and am building a Sonerai 2L - read 550lb slightly > underpowered two place! :) > > I'm trying to take as much weight out of the plane as I can by keeping > it simple. There's a lot of reasons I'm considering two batteries > rather than a battery and an alternator. But saving a bit of weight > isn't the main reason, the fact that I can move the weight of battery > where ever I want in the plane is a big bonus for servicing it > nevermind balancing, and ....the last thing I will do is put lead > weight back into it! > > I have an ignition system that draws ~1 amp and a single fuel pump > that draws another amp. I decided against the starter and the only > other amp draws will be two small Stratomaster instruments drawing > less than half an amp together. Total draw would be less than 2.5 Amps > > With the right warning system to indicate a low primary battery > I'm wondering if something like a 3 - 5 Ah battery would be large > enough for a backup? What about the primary? > > The downside of course is what would I do on a crosscountry trip? > Argh! :) > > Thanx a lot, appreciate any help and opinions! > Tony > ---------------------------------


    Message 24


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    Time: 07:44:10 PM PST US
    From: "Dennis Jones" <djones@northboone.net>
    Subject: Transponders
    Terra TRT 250D _____ From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of William Gill Sent: Wednesday, September 13, 2006 9:20 PM Subject: RE: AeroElectric-List: Transponders Hello Dennis, What brand of transponder are you dealing with? Bill -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Dennis Jones Sent: Wednesday, September 13, 2006 8:03 PM Subject: AeroElectric-List: Transponders In a transponder what is considered suppression out and remote ground when used in the wire harness. Dennis - The AeroElectric-List Email Forum - --> - NEW MATRONICS WEB FORUMS - --> - NEW MATRONICS LIST WIKI - --> - List Contribution Web Site - Thank you for your generous support! -Matt Dralle, List Admin. -->




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