AeroElectric-Archive.digest.vol-bp

January 28, 2003 - February 12, 2003



Date: Jan 28, 2003
From: "David Glauser" <david.glauser(at)xpsystems.com>
I'll have Scotch, please. And get your elbows off my table. :-) David -----Original Message-----
From: DHPHKH(at)aol.com [mailto:DHPHKH(at)aol.com]
Subject: Re: AeroElectric-List: Re: be nice, please Gang, As I understand it, most of the great minds of the 20th century really enjoyed sitting around a kitchen table, arguing the fine points of their specialties with their peers. I'm sure sure everyone gained in the process. I'm equally sure the debate got heated at times, with "prove it" being the classic challenge. SIG e-mail lists are the world's largest kitchen tables. Enjoy and learn. Anybody need another beer? Dan Horton ________________________________________________________________________________
From: "Ron Raby" <ronr(at)advanceddesign.com>
Subject: Re: wiring switches
Date: Jan 28, 2003
Robert In our buisness we call that skywiring and we try to avoid it if possible. although I do not see a problem with what you are doing. Here are my suggestions: You may want to make the switch wires longer and ty them to the panel somehow or even tywrap them to the switch and loop them back to make the connection. Try to make the branches off the main trunk for two or more switches each. If you had to reach up behind the panel this would give you a little more room to get your hand by. another way I seen is to put a peice of heat shrink on the 6" branch for neatness. This looks better than using small tywraps or lacing cord. Ron Raby N829R ----- Original Message ----- From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: wiring switches > > ><robert@thenews-journal.com> > > > >I'm wiring the toggle switches for my RV-6A and have a question about > >whether I'm doing so "acceptably." I'm using switches from B&C with fast-on > >connections, and have a row of 14 switches along the bottom left of my > >panel. > >I've secured the main bundle of wires running to these switches with adel > >clamps along the bottom of the bulkhead behind the panel. This makes the > >distance from where the wires leave the bundle to the switch connections at > >about 6", maybe a little less. > >I'm planning on tying the wires in smaller bundles between the clamps and > >the switches, but what I really want to know is whether it's ok to have this > >kind of setup behind my switches. > >I could, with some considerable effort, re-route the main bundle closer to > >the rear of the panel, but it would mean somehow actually clamping that > >bundle to the panel itself. For removability reasons I'd much prefer not to > >do this. > >It seems like I'm always thinking about something like this after I've > >started do it another way. The way I've got the switches wired now really > >looks fine to me just the way they are, but I thought I ought to ask. Just > >another reason (besides having to learn *everything*) I'm so darned slow at > >building this thing. > > What you are proposing sounds fine. > > Bob . . . > > ________________________________________________________________________________
Date: Jan 28, 2003
From: richard(at)riley.net
Subject: Re: Electric fuel valves
> >Mark et al, > >Thanks for the note. > >As co-owner or N812SP and primary designer of the electric fuel valve >installation, let me share some facts about our experience with the valves >... so far. Was 812SP also known as "Ten Forward?" Richard Riley N1701V ________________________________________________________________________________
Date: Jan 28, 2003
Subject: Re: Electric fuel valves
From: czechsix(at)juno.com
Guys, FYI, if anyone else is interested in contacting Bernie Hayes about the electric fuel valves in his Long-EZ, please write him at ebhayes(at)rockwellcollins.com. I work with him and forwarded his comments to the List yesterday, but he is not on the List and if you reply to yesterday's message you'll be sending the e-mail to me, not him. Thanks, --Mark Navratil (czechsix(at)juno.com) Cedar Rapids, Iowa RV-8A N2D finishing... ________________________________________________________________________________
Date: Jan 28, 2003
Subject: Re: wiring switches
From: "Robert Dickson" <robert@thenews-journal.com>
thanks, Ron, that's a great reply and pretty much what I was looking for. Is it better to run the bundle just behind the switches leaving it supported only by the switches, but with very short runs to the connectors? I've checked several web sites since I posted my query and have seen what look to be bundles right behind the row of switches with perhaps the only support at the start of the run behind the row. Does this make any sense? I could probably make this modification if it is a clearly more acceptable (read more durable) way to do it. I really appreciate your input. Robert Dickson RV-6A electrical ---------- >From: "Ron Raby" <ronr(at)advanceddesign.com> >To: >Subject: Re: AeroElectric-List: wiring switches >Date: Tue, Jan 28, 2003, 1:10 PM > > > > Robert > > In our buisness we call that skywiring and we try to avoid it if possible. > although I do not see a problem with what you are doing. > Here are my suggestions: > You may want to make the switch wires longer and ty them to the panel > somehow or even tywrap them to the switch and loop them back to make the > connection. Try to make the branches off the main trunk for two or more > switches each. If you had to reach up behind the panel this would give you a > little more room to get your hand by. another way I seen is to put a peice > of heat shrink on the 6" branch for neatness. This looks better than using > small tywraps or lacing cord. > > Ron Raby > > N829R > > > ----- Original Message ----- > From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> > To: > Subject: Re: AeroElectric-List: wiring switches > > > >> >> ><robert@thenews-journal.com> >> > >> >I'm wiring the toggle switches for my RV-6A and have a question about >> >whether I'm doing so "acceptably." I'm using switches from B&C with > fast-on >> >connections, and have a row of 14 switches along the bottom left of my >> >panel. >> >I've secured the main bundle of wires running to these switches with adel >> >clamps along the bottom of the bulkhead behind the panel. This makes the >> >distance from where the wires leave the bundle to the switch connections > at >> >about 6", maybe a little less. >> >I'm planning on tying the wires in smaller bundles between the clamps and >> >the switches, but what I really want to know is whether it's ok to have > this >> >kind of setup behind my switches. >> >I could, with some considerable effort, re-route the main bundle closer > to >> >the rear of the panel, but it would mean somehow actually clamping that >> >bundle to the panel itself. For removability reasons I'd much prefer not > to >> >do this. >> >It seems like I'm always thinking about something like this after I've >> >started do it another way. The way I've got the switches wired now really >> >looks fine to me just the way they are, but I thought I ought to ask. > Just >> >another reason (besides having to learn *everything*) I'm so darned slow > at >> >building this thing. >> >> What you are proposing sounds fine. >> >> Bob . . . >> >> > > > ________________________________________________________________________________
From: "Tony Babb" <tonybabb(at)alejandra.net>
Subject: Re: be nice, please
Date: Jan 28, 2003
> SIG e-mail lists are the world's largest kitchen tables. Enjoy and > learn. Anybody need another beer? I'll drink to that. ________________________________________________________________________________
From: "Ron Raby" <ronr(at)advanceddesign.com>
Subject: Re: wiring switches
Date: Jan 28, 2003
Robert This is what I would do. If you could come on to the switch panel from one side and run the wires either over the top or underneath the switches that would be good. If the switch panel can be removed try and make it so that you can pull this panel off to work on it with out taking the wires off. I would try not to use the switches for support of the wiring bundle if possible. Use Adel clamps, wallmounts etc. Try this catalog they have all kinds of mounts you can use. Branch the wires out at each switch aprox 4" long and put on your lugs. Make sure that this service loop will allow you to change these lugs a couple of times if needed. Make all the branched wires the same length for looks. http://onlinecatalog.panduit.com/Panduit/Templates/Panduit/browse.asp?newrec ordset=yes&classlevel=316 Ron Raby N829R ----- Original Message ----- From: "Robert Dickson" <robert@thenews-journal.com> Subject: Re: AeroElectric-List: wiring switches <robert@thenews-journal.com> > > thanks, Ron, that's a great reply and pretty much what I was looking for. Is > it better to run the bundle just behind the switches leaving it supported > only by the switches, but with very short runs to the connectors? I've > checked several web sites since I posted my query and have seen what look to > be bundles right behind the row of switches with perhaps the only support at > the start of the run behind the row. Does this make any sense? > I could probably make this modification if it is a clearly more acceptable > (read more durable) way to do it. > I really appreciate your input. > > Robert Dickson > RV-6A electrical > > ---------- > >From: "Ron Raby" <ronr(at)advanceddesign.com> > >To: > >Subject: Re: AeroElectric-List: wiring switches > >Date: Tue, Jan 28, 2003, 1:10 PM > > > > > > > > > Robert > > > > In our buisness we call that skywiring and we try to avoid it if possible. > > although I do not see a problem with what you are doing. > > Here are my suggestions: > > You may want to make the switch wires longer and ty them to the panel > > somehow or even tywrap them to the switch and loop them back to make the > > connection. Try to make the branches off the main trunk for two or more > > switches each. If you had to reach up behind the panel this would give you a > > little more room to get your hand by. another way I seen is to put a peice > > of heat shrink on the 6" branch for neatness. This looks better than using > > small tywraps or lacing cord. > > > > Ron Raby > > > > N829R > > > > > > ----- Original Message ----- > > From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> > > To: > > Subject: Re: AeroElectric-List: wiring switches > > > > > > > >> > >> ><robert@thenews-journal.com> > >> > > >> >I'm wiring the toggle switches for my RV-6A and have a question about > >> >whether I'm doing so "acceptably." I'm using switches from B&C with > > fast-on > >> >connections, and have a row of 14 switches along the bottom left of my > >> >panel. > >> >I've secured the main bundle of wires running to these switches with adel > >> >clamps along the bottom of the bulkhead behind the panel. This makes the > >> >distance from where the wires leave the bundle to the switch connections > > at > >> >about 6", maybe a little less. > >> >I'm planning on tying the wires in smaller bundles between the clamps and > >> >the switches, but what I really want to know is whether it's ok to have > > this > >> >kind of setup behind my switches. > >> >I could, with some considerable effort, re-route the main bundle closer > > to > >> >the rear of the panel, but it would mean somehow actually clamping that > >> >bundle to the panel itself. For removability reasons I'd much prefer not > > to > >> >do this. > >> >It seems like I'm always thinking about something like this after I've > >> >started do it another way. The way I've got the switches wired now really > >> >looks fine to me just the way they are, but I thought I ought to ask. > > Just > >> >another reason (besides having to learn *everything*) I'm so darned slow > > at > >> >building this thing. > >> > >> What you are proposing sounds fine. > >> > >> Bob . . . > >> > >> > > > > > > > > ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)BowenAero.com>
Subject: Howto d-sub machined pins
Date: Jan 28, 2003
That what I did on my AP wiring and it worked out nice. I put 1/4" flex-sleeve on the entire bundle. It made a 10', 7-wire bundle very manageable and clean looking. Without it it was chaos. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com 2003 - The year of flight! > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On > Behalf Of Robert L. Nuckolls, III > > Heat shrink will increase the diameter of the assembly to > an extent that will prevent the pin from being inserted > into the connector. Heat shrink is not necessary on > crimped connectors. If you're concerned about mechanical > support, you can put a back shell on the connector. > However, a string tie or tye-wrap on the wire bundle > within an inch or so of the connector body stiffens up > the wire bundle to provide adequate support. > > Bob . . . ________________________________________________________________________________
From: "Ronald Cox" <racox(at)ix.netcom.com>
Subject: Re: AeroElectric-List Digest: 10 Msgs - 01/27/03
Date: Jan 29, 2003
Hey guys, let these things sit on your computers a minute before you click SEND and I'll bet most of them don't get sent at all. "Old Bob" asked if folks wanted his repeated discussion on the T&B vs. TC debate. Folks said yes, so he re-posted it. Not a problem for anyone, IMHO. As for the "Go ahead, make my day" line from the OTHER Bob, if you think it's arrogant, you obviously don't get it at all. Bob (Nuckolls) enjoys nothing more than having someone show him if/when he's wrong, and that's why he says that. It really does make his day. It's not arrogance, though he would have the right to be so. I've never met anyone who knows so much about a subject who is so willing to explain and support his opinions, and identify them as such, WITHOUT being arrogant. And he does it all for free. I, for one, greatly appreciate what he, and others here, post for us all to wade through. As for the "off topic" posts, that's not nearly as annoying to me as the endless complaining about the occasional "off topic" posts. And the endless, indiscriminate "quoting" of messages one is responding to. (One list a week or so ago was over 75% "quoted" material.) I dug through it and deleted the "chaff". If something on this list bugs you, just delete it. Just like this message. And you can have back the money you paid for mine... And yes, lighten up, "all y'all"... There's far too much good info here (among the other) to chase so many knowledgeable folks away. Ron From: "Rick D." <rsdec1(at)msn.com> Subject: AeroElectric-List: Re: be nice, please What the heck, we are now getting health and academic reports from all over, why not some discussion about something that is at least an electrical component in an airplane. God, we have had all kinds of topics here. At one point some non-aircraft related software topics dominated days of the list. Arrogance? GO AHEAD, MAKE MY DAY, SHOW ME WHERE I"M WRONG! Wow, is that genuine arrogance or what? I could point out hundreds of mistakes made here on this site and related literature but I don't feel as though I need to rub anyone's nose in it. Mistakes are made by EVERYONE. This list is frequented by some of the most arrogant, pompous, know-it-all individuals that I have ever had the displeasure of reading. It seems as though someone is always looking for an argument and/or a fight at this list. Simple suggestions or opinions are met with arrogant, discourteous responses because they have not been supported and backed up by scienticific fact. Opinions offered by some individuals here are offered as gospel and to disagree with them or to offer alternatives only opens one up to more arrogant responses. One only needs to go back and read some of the past posts to verify this. Fortunatly, there are still some intelligent, courteous, non-arrogant and genuine opinions that people such as "Old Bob" can contribute. And, N919RV, just who DO you think is responsible for the mentioned pilot differences noted by "Old Bob"? Never mind I don't want your OPINION unless you can back it up with hard data. I don't think Denny was arrogant or rude at all, he simply asks a question. He did not state his opinion that it was "old Bob's" fault. You interpreted Denny's question for him. If Denny wanted to say he thought it was Bob's fault, he probably would have said just that. How about some discussion about some of the solid state gyro's from people like the Icarus/IPAQ. Will these replace the dreaded T/C and AI? Lighten up yourself N919RV, see ya later, ha, ha, ha, ________________________________________________________________________________
Date: Jan 28, 2003
From: Frank Smidler <smidler(at)dcwi.com>
Subject: Wig-Wag switching
I have been looking at Bobs schmatics for Wig-Wag and I was wondering if it is feasable on the third layout to split the 4LT1-10 switch into tow 2-10 switches, one for taxi and one for landing lights. The idea is to be able to have both lights on, just the taxi light, wig-wag or off with only two switches. I prefer not to use three switches as on the first layout to save panel room. As I see it only when BOTH switches are at the center will wig-wag work. If the taxi switch is up then it will be on, no matter what position the landing lt switch is at and visa-versa. I came to this conclusion based on Note #1 that states both 2 & 3 pins of the SSF-1 flasher must be loaded to a lamp in order for it to actually flash. The only reason I am looking at seperating the taxi and landing light is that I have a tail dragging RV-6 that I am assuming I will have to adjust the taxi light different then the landing light. The second assumption I am making is that I will need to turn off the landing light on the ground since it will be pointing up and may blind other pilots. Are these valid assumptions? Any comments would be appreciated. ________________________________________________________________________________
Date: Jan 28, 2003
From: Frank Smidler <smidler(at)dcwi.com>
Subject: Position Lt and Inst Lt Switches
Has anyone set up a single switch to turn on both the position lights and the instrument lights (still two circuits)? I am thinking of doing this with a 2-2 switch but I would like to hear of any down side to doing it, such as a need to shut off the instrument lights when the position lights are on. I will state that I plan on utilizing an AEC dimmer on the instrument light circuit. This is another attempt to simplify the instrument panel and to save space. While we are on the subject, I am assuming that the AEC dimmer does not have an off function. Thank You Frank Smidler RV-6 ________________________________________________________________________________
Date: Jan 29, 2003
Subject: Re: Position Lt and Inst Lt Switches
From: "Matt Prather" <mprather(at)spro.net>
As has been discussed on the list before, for completion of flight, the position lights aren't all that important. Conversely, I think it would somewhat more inconvenient to do a night flight without your panel lights. If you lose your main source of power (alternator) I think you will want to turn off everything not necessary for continued flight. That would include your position lights. Maybe you could have a single switch, and have the panel lights and position lights being fed from two different busses. The bus that feeds your position lights (main?) could also feed other non-essential (non- endurance) consumers. Regards, Matt Prather N34RD > > > Has anyone set up a single switch to turn on both the position lights > and the instrument lights (still two circuits)? I am thinking of doing > this with a 2-2 switch but I would like to hear of any down side to > doing it, such as a need to shut off the instrument lights when the > position lights are on. I will state that I plan on utilizing an AEC > dimmer on the instrument light circuit. This is another attempt to > simplify the instrument panel and to save space. > > While we are on the subject, I am assuming that the AEC dimmer does not > have an off function. > > Thank You > > Frank Smidler > RV-6 > > ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: gooseneck lamp
Date: Jan 27, 2003
I installed mine between the landing gear weldment and the longeron attached to the sidewall. I manufactured a plate that sits on top of these two items. This plate has the gooseneck adapteer and dimmer attached to it. Very convienent. Ross Mickey RV6A ----- Original Message ----- From: "Robert Dickson" <robert@thenews-journal.com> Subject: AeroElectric-List: gooseneck lamp <robert@thenews-journal.com> > > I've bought one of Bob's gooseneck lights for my RV-6A, with the intention > of mounting it on the forward canopy rail, just forward of the roll bar > base. For you folks that have installed (or are considering installing) one > of these lights, does this sound like a reasonable place to put it? I've > also thought about mounting it on the forward end of the pilot's armrest. My > thought is to put it someplace where it can illuminate either the panel (in > an E bus-only situation) or a chart in my lap. Other/better ideas? > > thanks, > > Robert Dickson > RV-6A electrical ________________________________________________________________________________
From: "Mark Means" <rgvelocity(at)lmf.net>
Subject: GM alternator
Date: Jan 29, 2003
Bob, Back to the overvoltage disconnect for my late model GM alternator (they call it a generator as it puts out DC) and is internally regulated. To recap, you advised that wiring the crowbar overvoltage device in the field circuit may or may not actually take the alternator off- line, correct? Your recommended addition of an extra circuit with a heavy duty contactor (105 amp) to disconnect the alternator output will complicate the installation but is doable. Currently I have the output going direct to the starter contactor via a fuse as per your recommendation. I suppose my question is what are the chances that (1) an overcharge condition will occur to begin with; and (2) if it does happen what are the chances that the elimination of the field voltage will not solve the problem. I suppose an alternative is to modify the alternator for use of an external voltage regulator.... how hard and/or expensive is this? Changing the alternator is not an option. Any comments or advice is welcome, thanks. Mark Means ________________________________________________________________________________
Date: Jan 29, 2003
From: "William Yamokoski" <yamokosk(at)lmc.cc.mi.us>
Subject: Re: Microair Piggyback module
I also have this combination, with a whole bunch of radio noise to boot. Any time I throw a switch I get input in the headphones (engine off.) I've spent these cold winter weeks reading and re-reading Bob's book on the subject. Unfortunately it's too cold to stand in the hangar and experiment. One question comes to mind though. Flightcom manual calls for headphone grounds to return to the unit, which is itself grounded. I ran the headphone grounds directly to the firewall-mounted B & C groundblock. Any chance that's the culprit? Headphone and microphone jacks are mounted in a piece of angle aluminum which is mounted to my steel fuselage cage with rubber-cushioned Adel clamps. Jacks themselves are mounted with the plastic and insulated washers prescribed by Flightcom. No shielded wire was used except between the radio and intercom. I've been scratching my head about this for quite a while. Warm weather can't come soon enough. Thanks very much. Bill Yamokoski ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Wig-Wag switching
> >I have been looking at Bobs schmatics for Wig-Wag and I was wondering if >it is feasable on the third >layout to split the 4LT1-10 switch into tow 2-10 switches, one for taxi >and one for landing lights. >The idea is to be able to have both lights on, just the taxi light, >wig-wag or off with only two >switches. I prefer not to use three switches as on the first layout to >save panel room. > >As I see it only when BOTH switches are at the center will wig-wag >work. If the taxi switch is up >then it will be on, no matter what position the landing lt switch is at >and visa-versa. I came to >this conclusion based on Note #1 that states both 2 & 3 pins of the SSF-1 >flasher must be loaded to >a lamp in order for it to actually flash. > >The only reason I am looking at seperating the taxi and landing light is >that I have a tail dragging >RV-6 that I am assuming I will have to adjust the taxi light different >then the landing light. The >second assumption I am making is that I will need to turn off the landing >light on the ground since >it will be pointing up and may blind other pilots. Are these valid >assumptions? You betcha. What you propose will work. I've added the option to the collection of drawings at: http://216.55.140.222/articles/WigWag/WigWag.pdf Bob . . . ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Position Lt and Inst Lt Switches
> >Has anyone set up a single switch to turn on both the position lights and >the instrument lights >(still two circuits)? I am thinking of doing this with a 2-2 switch but I >would like to hear of any >down side to doing it, such as a need to shut off the instrument lights >when the position lights are >on. I will state that I plan on utilizing an AEC dimmer on the instrument >light circuit. This is >another attempt to simplify the instrument panel and to save space. Builders have used the 2-10 switch to control strobes and position lights. Down is OFF, mid position is STROBE, up is strobe + position lights. >While we are on the subject, I am assuming that the AEC dimmer does not >have an off function. Correct. The dimmer is designed to have the max counter-clockwise position of the dimmer pot to bias the lamps up at a voltage just below usable output (about 4v). This means that as you rotate the control, you get immediate perceived response from the action. Dimmers that go to zero volts "waste" the first few degrees of control rotation doing nothing but bringing the lamps up from zero to first visible light. There is no practical reason to include additional switching to turn the lamps OFF . . . lamp life in the keep-warm mode is about 10x the life of your airplane. See chapter on lighting. Bob . . . ________________________________________________________________________________
Date: Jan 29, 2003
Subject: Re: Microair Piggyback module
From: "Matt Prather" <mprather(at)spro.net>
When you say headphone, are you referring to both jacks (to include the mic)? Or, this another way of asking whether you grounded the mic back to the radio, or to the firewall? If you grounded the mic to the firewall, I could see this being the problem. I would be a little surprised if the noise is coming directly from a faulty ground for the headphone (the big plug) but not the mic. From my limited experience, it seems like you are likely to pick up noise on the input to a buffered or amplified circuit. The mic side qualifies, but the headphone side does not. That's why I can see using sheilded wire on the mics, but not on the headphone. On the headphone side, the electronics are already done amplifying the signal, and noise will probably be of the low voltage/ current variety. All bets are off if the headphone amplifier doesn't use a common ground, ie, the negative headphone output needs to be grounded, instead of floating, by design. If that were the case, returning the negative lead of the headphone back to the radio would be critical. I doubt this is an issue. Interesting question. Please let us know what you find. Regards, Matt Prather N34RD > > > I also have this combination, with a whole bunch of radio noise to boot. > Any time I throw a switch I get input in the headphones (engine off.) > I've spent these cold winter weeks reading and re-reading Bob's book on > the subject. Unfortunately it's too cold to stand in the hangar and > experiment. One question comes to mind though. Flightcom manual > calls for headphone grounds to return to the unit, which is itself > grounded. I ran the headphone grounds directly to the firewall-mounted > B & C groundblock. Any chance that's the culprit? Headphone and > microphone jacks are mounted in a piece of angle aluminum which is > mounted to my steel fuselage cage with rubber-cushioned Adel clamps. > Jacks themselves are mounted with the plastic and insulated washers > prescribed by Flightcom. No shielded wire was used except between the > radio and intercom. > I've been scratching my head about this for quite a while. Warm > weather can't come soon enough. Thanks very much. > Bill Yamokoski > > ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Re: Position Lt and Inst Lt Switches
Date: Jan 29, 2003
Do the lamps drain battery when they are "Turned Down"? If so, I assume you would not want them on the battery bus without some additional switch? - Jim > There is no practical reason to include additional switching > to turn the lamps OFF . . . lamp life in the keep-warm mode > is about 10x the life of your airplane. See chapter on lighting. > > Bob . . . > ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: GM alternator
> >Bob, > >Back to the overvoltage disconnect for my late model GM alternator (they >call it a generator as it puts out DC) and is internally regulated. To >recap, you advised that wiring the crowbar overvoltage device in the field >circuit may or may not actually take the alternator off- line, correct? >Your recommended addition of an extra circuit with a heavy duty contactor >(105 amp) to disconnect the alternator output will complicate the >installation but is doable. Currently I have the output going direct to >the starter contactor via a fuse as per your recommendation. > >I suppose my question is what are the chances that >(1) an overcharge condition will occur to begin with; . . . it is low but NOT zero . . . > and (2) if it does happen what are the chances that the > elimination of the field voltage will not solve the problem. 100% >I suppose an alternative is to modify the alternator for use of an >external voltage regulator.... how hard and/or expensive is this? >Changing the alternator is not an option. Depends on the alternator and experience of who's doing it. B&C routinely modifies hundreds of brand new ND alternators to turn them into aircraft alternators . . . but their tooling and experience level makes this a fairly easy task . . . however, I wouldn't try it myself. I have modified some older machines with reasonable success but nature of the task can vary widely from model to model even within the same brand. I'm not familiar with your particular part, you can ask an alternator shop about the task and see if they would like to take it on. Many of my builders have gone this route over the years. I cannot recall hearing any negative feedback on the experience so this is certainly an option to consider. Bob . . . ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: 10258 Sherick
>Hi Bob, > >Quick question on antenna ground planes: Is it acceptable for an external >COMM antenna, mounted on the belly pan of a composite fuselage (E-Glass), >to have a ground plane made from 2" wide aluminum tape, the kind you can >buy in the hardware store? See chapter on antennas in the AeroElectric Connection. The technique you describe is detailed there. >The aluminum tape seems to conform well to the slightly curved surface of >the belly pan and can be taped in sections to tape up a rather large >ground plane. It seems to be conductive on all strips when overlapped and >pressed into place. I suppose soldering a braided wire across all strips >would ensure conductivity even better. Soft aluminum tape is VERY difficult to make an electrical connection to that is also mechanically robust . . . use copper strip. Hobby shops like Hobby Lobby offer rolled, sheet copper that can be cut into strips about 1" wide and then bonded to the inside of your fuselage with something like ShoGoo or perhaps an overlayment of glass and epoxy. Bob . . . ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: What is flex-sleeve?
><robert@thenews-journal.com> > >what is flex-sleeve? > >Robert Dickson >RV-6A Here are some useful examples: http://www.alphawire.com/pages/153.cfm http://www.alphawire.com/pages/154.cfm which you can buy from these folks http://www.alphawire.com/index_8.cfm Bob . . . ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Wiring headset jacks
Date: Jan 29, 2003
Dear all, another question where I'm a bit uncertain, even after reading Bob's Shop Notes and comparing them with the Seminar wirebook. Maybe Bob, if you read this could you comment? Bob, in the shop note you say, that you use 3 wire shielded, and the shield itself is connected on both (?) sides to the Mic LO, did you use the 3 wire because of wiring both mic's to only 4 ports? (You used the shielding instead of one wire). I have a used Garmin 340, where I have a separate port for each mic/phone, should I use a 2wire shielded for each mic using the shield as the third wire (if yes, which contact should be wired with the shield)? Same for the phones, if I use the same approach I could use a 1wire shielded wire for the two contacts. It would save weight and money. Many thanks for your feedback Werner ________________________________________________________________________________
From: "Stan Blanton" <stanb(at)door.net>
Subject: Wig Wag flasher
Date: Jan 29, 2003
Bob, Do you know what the flash rate is of the wig wag unit that B&C is stocking? Thanks, Stan Blanton ________________________________________________________________________________
Subject: Dual battery / Dual Alternator in composite canard
pusher
Date: Jan 29, 2003
From: "I-Blackler, Wayne R" <wayne.blackler(at)boeing.com>
"Robert L. Nuckolls, III" G'Day Bob, I have a question regarding grounding - How do you suggest running the grounds for a dual battery (both 12V/17AH) / dual alternator (40A main/20A aux) (similar to Z14) setup in a single engine composite canard pusher? I have B&C fast on ground buses on the panel and the firewall, and both batteries in the nose(FYIO - I would have used one battery / two alternators but need the weight up front, and figured a battery is better than ballast). I was thinking: 1. 2AWG from Main Battery -ve to firewall fast on ground bus (5/16" brass bolt). 2. 2AWG from firewall ground bus (bolt) to engine crankcase. 3. 4AWG from Main battery -ve to instrument panel fast on ground bus (5/16" brass bolt). 4. 4AWG from Aux battery to firewall. Do I need anything further? I'd like to avoid the installation complexities of copper conduit - What would you do if designing grounds for this system? I very much appreciate your time, and forbearance. Cheers Wayne Blackler IO-360 Long EZ ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Wig Wag flasher
> >Bob, > >Do you know what the flash rate is of the wig wag unit that B&C is >stocking? I should have measured them while they were here. Sorry 'bout that. I would estimate each light flashes 2 times per second alternating. Bob . . . ________________________________________________________________________________
Date: Jan 29, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Position Lt and Inst Lt Switches
> >Do the lamps drain battery when they are "Turned Down"? If so, I assume you >would not want them on the battery bus without some additional switch? Sure . . . which configuration are you considering for system architecture? Why would you run the lighting from a battery bus? Bob . . . ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Re: Position Lt and Inst Lt Switches
Date: Jan 29, 2003
Dual Battery / Dual Alt configuration. Was thinking that cabin lights would be nice for night cabin/flight prep without requiring the batteries to be turned on. - Jim > > > >Do the lamps drain battery when they are "Turned Down"? If so, I assume you > >would not want them on the battery bus without some additional switch? > > Sure . . . which configuration are you considering for system > architecture? Why would you run the lighting from a > battery bus? > > Bob . . . > > ________________________________________________________________________________
From: N2165v(at)aol.com
Date: Jan 30, 2003
Subject: King connector
I just got a price on a King 030-00101-0002 coax connector of $46. First question is why so much? Second question would be is there a "generic" replacement for this connector? It is the antenna connector on the KT-76C and the KY-97A. Using RG-400 coax. Thanks ________________________________________________________________________________
From: "Stucklen, Frederic IFC" <Fred.Stucklen(at)UTCFuelCells.com>
Subject: Position Lt and Inst Lt Switches
Date: Jan 30, 2003
Listers, In the RV-6A I'm building, I'm using the switched NAV light voltage to drive the panel dimmer circuit. Whenever the NAV lights are ON, the panel dimmer circuit is active. ( The fallback to a blown NAV circuit fuse is the cockpit flood LED's..) The NAV circuit voltage is also used to power a relay whose contacts select fixed 12V instrument backlighting (default mode), or dimmer circuit backlighting. Some instruments require back lighting for sunlight operations, that is too bright for night operations. The Electronics International engine instruments are a good example of this requirement (and there's nothing in their operational manual suggesting how it should be done...) Their LCD display requires 12V backlighting in the sunlight, and a variable voltage at night (i.e., the dimmer output).. Also, the LED's go into a dim mode when 12V is applied to an input (which is internally overridden if an alarm condition occurs). So by tying in the backlight/LED power requirements into the NAV circuit voltage, both modes of operation are obtained. I used this same circuit concept on my last RV-6A. Never had a problem in over 2000 hrs of operation...... Fred Stucklen RV-6A > >Has anyone set up a single switch to turn on both the position lights and >the instrument lights >(still two circuits)? I am thinking of doing this with a 2-2 switch but I >would like to hear of any >down side to doing it, such as a need to shut off the instrument lights >when the position lights are >on. I will state that I plan on utilizing an AEC dimmer on the instrument >light circuit. This is >another attempt to simplify the instrument panel and to save space. Builders have used the 2-10 switch to control strobes and position lights. Down is OFF, mid position is STROBE, up is strobe + position lights. >While we are on the subject, I am assuming that the AEC dimmer does not >have an off function. Correct. The dimmer is designed to have the max counter-clockwise position of the dimmer pot to bias the lamps up at a voltage just below usable output (about 4v). This means that as you rotate the control, you get immediate perceived response from the action. Dimmers that go to zero volts "waste" the first few degrees of control rotation doing nothing but bringing the lamps up from zero to first visible light. There is no practical reason to include additional switching to turn the lamps OFF . . . lamp life in the keep-warm mode is about 10x the life of your airplane. See chapter on lighting. Bob . . . ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Position Lt and Inst Lt Switches
> >Dual Battery / Dual Alt configuration. Was thinking that cabin lights would >be nice for night cabin/flight prep without requiring the batteries to be >turned on. Okay, if those are going to be on dimmers, you'll also need to add a switch. They're increasingly hard to find but some potentiometers can be fitted with switches like the old volume control switches on radios of old. Bob . . . ________________________________________________________________________________
From: "Tom Parks" <flightwork2(at)msn.com>
Subject: LVMM Wiring
Date: Jan 30, 2003
Bob! I've started wiring my main and aux battery contactors per your schematic Fig. 7 that came with the LVMM kit. Running a wire from the contactor to DC master switch term 5 and term 4 to gnd will only close contractor with switch in alt position. Contactor will not not close in the bat position. Before adding any more wires to the switch, thought I would query whether this is normal. Have not wired the Alt Fld breaker, fuselink and OVM-14 to the switch as yet. regards Tom Parks RV-7 N620CF ________________________________________________________________________________
Date: Jan 30, 2003
From: DHPHKH(at)aol.com
Subject: Right Angle BNC
Gang, A few months ago somebody asked about crimp-on right angle female BNC connectors. Bob mentioned using a right angle adapter. Has anyone yet found a source for a decent crimp-on right angle? Dan ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Re: Inst Lt Switches
Date: Jan 30, 2003
Perhaps I could just unplug the gooseneck from the socket (instead of a switch)? Would not be good if I forget to take it out, but should work? > > > >Dual Battery / Dual Alt configuration. Was thinking that cabin lights would > >be nice for night cabin/flight prep without requiring the batteries to be > >turned on. > > Okay, if those are going to be on dimmers, you'll also > need to add a switch. They're increasingly hard to find > but some potentiometers can be fitted with switches > like the old volume control switches on radios of old. > > Bob . . . > ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: King connector
> >I just got a price on a King 030-00101-0002 coax connector of $46. First >question is why so much? Second question would be is there a "generic" >replacement for this connector? It is the antenna connector on the KT-76C >and the KY-97A. Using RG-400 coax. >Thanks Most connectors offered with "certified" radios are generic to some commercial catalog. Unfortunately, the FAA frowns on the idea of buying a connector from the original manufacturer under their part number . . . gotta be sure you get the "right" part. Hence, manufacturers put their numbers on lots of generic parts at multiples of what they're really worth. At one time, Cessna had tens of thousands of dollars tied up in lowly U/G-21 coax connectors stocked in 8-10 different places under a manufacturer's part number. I presume you're talking about a blind-mate tray connector that fastens to the tray with a snap ring and solders onto the coax. The tray connector mates with radio connector as the radio seats fully in the tray. I poked around on the 'net and couldn't find these in the time I had to look. Seems like they were a U/G-1085 . . or some such 4-digit callout. Call an avionics shop and see if they can help you. I think this is the same connector used on ARC's tray mounted radios too. I'll check some of my info resources next week. Bob . . . ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: LVMM Wiring
> >Bob! > >I've started wiring my main and aux battery contactors per your schematic >Fig. 7 that came with the LVMM kit. Running a wire from the contactor to >DC master switch term 5 and term 4 to gnd will only close contractor with >switch in alt position. Contactor will not not close in the bat position. >Before adding any more wires to the switch, thought I would query whether >this is normal. Have not wired the Alt Fld breaker, fuselink and OVM-14 to >the switch as yet. Hmmm. . . numbering of the switch pins is different on various schematics depending on whether I was referring to a Microswitch 2TL1-10 or a AEC S700-2-10 switch. Looking into the back of the switch, the columns are swapped. Try moving the contactor leads to the other side of the switch . . . sounds like they're wired to the side that is sequenced to control the ALT FIELD line. Bob . . . ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Dee is home and on the mend . . .
Brought her home just before lunch today. Now, I've got about 36 hours to try and convert back to a "1st shift person" for the seminar scheduled next Saturday in Nashville! Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Inst Lt Switches
> >Perhaps I could just unplug the gooseneck from the socket (instead of a >switch)? Would not be good if I forget to take it out, but should work? You could do that too . . . Bob . . . ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Right Angle BNC
> >Gang, > A few months ago somebody asked about crimp-on right angle female BNC > connectors. Bob mentioned using a right angle adapter. Has anyone yet > found a source for a decent crimp-on right angle? There are a number of sources . . . but none that I know of that will install with the tool we sell. AMP 225974-2 is a suitable part that sells for $22.00 qty of 1. The hand tool that installs it is about $400.00 If it were my airplane, I'd install a cable male connector, mate it with a right angle adapter and shrink a chunk of double walled tubing over the interface to make it permanent. . . . the po' boy's right angle connector. Bob . . ________________________________________________________________________________
Date: Jan 30, 2003
Subject: landing lights
From: "Robert Dickson" <robert@thenews-journal.com>
I've installed the RMD wingtip landing lights on my RV. These use H7604 50w bulbs. I would like to wire these to one switch, but I've got a couple of issues. First, RMD supplied #12 wire for these lights, which seems too large for the wattage and length of run. Second, in searching the RV list archive for what other folks have done for wiring these lights, I came across the following post from Bob (Aug 99): If you're going to have a landing light in each wing, you need a breaker/fuse and switch for EACH light. 50 watt bulbs draw 4.5 amps, 100 watt bulbs 9 amps, 150 watt bulbs draw 13.5 amps. Wire sizes and breakers purely for current carrying considerations are 20AWG/7A; 18AWG/10A, and 14AWG/15A for each lamp. In a metal airplane, voltage drops in wires selected for current rating alone are generally insignificant. You need to be looking at runs of 20+ feet before I'd be concerned about voltage drops. So, do I really need to have a switch for each light? If I don't, would 14awg wire and a 10amp fuse be appropriate for the 2 light circuit? thanks, Robert Dickson RV-6A electrical ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: landing lights
Date: Jan 30, 2003
Interesting. I plan a 75W taxi light and a 75W landing light on each gear door, so 2 light per side, 4 total. If I understand correctly, you are saying I should have 4 breakers and 4 switches? I don't understand why, so please "learn" me :) If you're going to have a landing light in each wing, you need a breaker/fuse and switch for EACH light. ________________________________________________________________________________
Date: Jan 30, 2003
From: emrath <emrath(at)comcast.net>
Subject: Re: Wig-Wag switching
Bob, this is getting interesting. On drawing #5, both switches need to be in the middle position to turn the wigwag on. Instead, how about taking circuit shown on drawing #4 and add a Switch downstream of the the 4TL1-10 device to switch either the right or left light off (use pin 2 and 5 as powered inputs). That way one could set up one light to be the taxi and one to be the landing light if desired on a tail dragger or one could just shut off one of the landing lights so as not to blind observers or other pilots while in ground ops? What kind of switch could one use, S700-2-10 (right-on-left or taxi-on-right)? Seems like this switch could be left "on" unless one has to turn off one of the lights. Marty in Brentwood, TN From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: Wig-Wag switching --> >--> > >I have been looking at Bobs schmatics for Wig-Wag and I was wondering >if >it is feasable on the third >layout to split the 4LT1-10 switch into tow 2-10 switches, one for taxi >and one for landing lights. >The idea is to be able to have both lights on, just the taxi light, >wig-wag or off with only two >switches. I prefer not to use three switches as on the first layout to >save panel room. > >As I see it only when BOTH switches are at the center will wig-wag >work. If the taxi switch is up >then it will be on, no matter what position the landing lt switch is at >and visa-versa. I came to >this conclusion based on Note #1 that states both 2 & 3 pins of the SSF-1 >flasher must be loaded to >a lamp in order for it to actually flash. > >The only reason I am looking at seperating the taxi and landing light >is >that I have a tail dragging >RV-6 that I am assuming I will have to adjust the taxi light different >then the landing light. The >second assumption I am making is that I will need to turn off the landing >light on the ground since >it will be pointing up and may blind other pilots. Are these valid >assumptions? You betcha. What you propose will work. I've added the option to the collection of drawings at: http://216.55.140.222/articles/WigWag/WigWag.pdf Bob . . . ________________________________________________________________________________
Date: Jan 30, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Off line again . . .
This time for something more enjoyable. Will be hopping on the big iron bird bound for Nashville in the morning. Be back on the list Monday morning. Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
From: TSaccio(at)aol.com
Date: Jan 30, 2003
Subject: Re: landing lights
I'm installing Whalen strobes and landing lights on a Seawind that I'm building. Do all wires including the ones going to the landing lights have to be shielded. I can't seam to find any information on this. Tom Saccio ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)BowenAero.com>
Subject: landing lights
Date: Jan 30, 2003
Just the strobes, from the power supply to the light. At least that's my understanding. - Larry Bowen RV-8 electrical Larry(at)BowenAero.com http://BowenAero.com 2003 - The year of flight! > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On > Behalf Of TSaccio(at)aol.com > Sent: Thursday, January 30, 2003 11:20 PM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: landing lights > > > > I'm installing Whalen strobes and landing lights on a Seawind > that I'm > building. Do all wires including the ones going to the > landing lights have to > be shielded. I can't seam to find any information on this. Tom Saccio > > > ========== > Matronics Forums. > ========== > List members. > ========== > ========== > > > ________________________________________________________________________________
From: "Kyle Boatright" <kyle.boatright(at)adelphia.net>
Subject: Re: landing lights
Date: Jan 31, 2003
Neither landing light or position light wires need to be shielded. Whelen supplies a 3 conductor wire that shields the wires for the position lights and strobe, but you only really need to shield the strobe wires. ----- Original Message ----- From: <TSaccio(at)aol.com> Subject: Re: AeroElectric-List: landing lights > > I'm installing Whalen strobes and landing lights on a Seawind that I'm > building. Do all wires including the ones going to the landing lights have to > be shielded. I can't seam to find any information on this. Tom Saccio > > ________________________________________________________________________________
Date: Jan 31, 2003
From: Rick <rick.pitcher(at)verizon.net>
Subject: Narco Com 120 gears
I need to replace one of the little plastic gears in the frequency selector mechanism on a Narco Com 120.I called the factory and they want me to ship them the radio and $400 or $500. It's obviously not worth spending that much on a 20 year old radio. Is there another source for these gears? Rick Pitcher ________________________________________________________________________________
From: "Wendell & Jean Durr" <legacy147(at)cableone.net>
Subject: Re: landing lights
Date: Jan 31, 2003
Interesting. I plan a 75W taxi light and a 75W landing light on each gear door, so 2 light per side, 4 total Will the added weight on the doors impact their remaining closed under air loads? 'Twas Lancair's concern Wendell Durr ________________________________________________________________________________
From: N223RV(at)aol.com
Date: Jan 31, 2003
Subject: cycling voltmeter and ammeter
have about 16 hours on my RV-4 and have a question.=A0 My voltmeter and ammeter cycle between 13-14.5 V on the voltmeter and between 5-10 amps every 1/2 second or so.=A0 The volt meter rapidly rises from 13 volts to 14.5 volts and back almost like the voltage is rising, gets too high, cuts out, drops below 13 volts, kicks back in, rises to 14.5 volts, cuts out......=A0 It just rapidly cycles up and down.=A0 I have tried adjusting the voltage regulator lower but does not seem to help the cycling..... I have a 35 amp Van's supplied alternator, a Van's supplied $35ish voltage regulator, and an Aeroelectric overvoltage protection device.=A0 This issue does not seem to cause any problems, but it does not seem right.=A0 Last night I turned on all my electrical accessories and it seemed to steady out at about 13 V, but if I turn off just a couple of items, it goes right back to cycling.=A0 I don't understand what is going on or if it is an issue, but it just does not seem right. Does anyone have any ideas on what to check? Thanks Mike Kraus N223RV - 16 hours and loving it! ________________________________________________________________________________
From: "Ron Raby" <ronr(at)advanceddesign.com>
Subject: Re: King connector
Date: Jan 31, 2003
amphenol or amp should have a cheaper version. Ron Raby N829R ----- Original Message ----- From: <N2165v(at)aol.com> Subject: AeroElectric-List: King connector > > I just got a price on a King 030-00101-0002 coax connector of $46. First > question is why so much? Second question would be is there a "generic" > replacement for this connector? It is the antenna connector on the KT-76C > and the KY-97A. Using RG-400 coax. > Thanks > > ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: landing lights
Date: Jan 30, 2003
They are on the outer gear door which is directly connected to the strut, so I think they will be alright....we'll see. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Wendell & Jean Durr Subject: Re: AeroElectric-List: landing lights Interesting. I plan a 75W taxi light and a 75W landing light on each gear door, so 2 light per side, 4 total Will the added weight on the doors impact their remaining closed under air loads? 'Twas Lancair's concern Wendell Durr ________________________________________________________________________________
Date: Jan 31, 2003
From: Richard Dudley <rhdudley(at)att.net>
Subject: Low Cost Ground Power Jack .....
Bob, I like the idea of having a ground power jack for the reasons you list in your paper. I have ordered the parts to install one. In re-reviewing the schematic (Fig. 3) I am having a problem understanding how the ground power contactor can release when the external power is removed. It seems to me that, since it is connected to the aircraft battery positive, that contactor will remain energized after the external power is removed; with the only recourse being to pull the circuit breaker to unlatch the contactor. What am I missing? Regards, Richard Dudley ________________________________________________________________________________
Date: Jan 31, 2003
Subject: Re: landing lights
From: "Matt Prather" <mprather(at)spro.net>
I can't see any reason to sheild the wiring for the landing lights. > > I'm installing Whalen strobes and landing lights on a Seawind that I'm > building. Do all wires including the ones going to the landing lights > have to be shielded. I can't seam to find any information on this. Tom > Saccio > > ________________________________________________________________________________
From: "Stucklen, Frederic IFC" <Fred.Stucklen(at)UTCFuelCells.com>
Subject: Subject:
Date: Jan 31, 2003
Rick, NARCO now does all their own repairs - no dealer repairs anymore, so you're stuck with them unless you can find a avionics repair shop that has some old ones laying around....... Fred Stucklen RV-6A I need to replace one of the little plastic gears in the frequency selector mechanism on a Narco Com 120.I called the factory and they want me to ship them the radio and $400 or $500. It's obviously not worth spending that much on a 20 year old radio. Is there another source for these gears? Rick Pitcher ________________________________________________________________________________
Subject: Narco Com 120 gears
Date: Jan 31, 2003
From: "I-Blackler, Wayne R" <wayne.blackler(at)boeing.com>
Rick, A mate of mine back in Australia had the same problem with his Narco transponder. He was quoted same, except US$500 is $1000 to an Australian.. Solution: He made an aluminium version of the gear on his lathe, installed it, and is living happily ever after. NB: He had to synchronise the actual frequency with the number on the dial (Note: It was only one XPDR dial of the four). You could probably get an Avionics shop to install your own gear and bench synchronise. The tech wont look twice when he sees the stripped plastic version he's replacing. Personally, if your not breaking a warranty seal on the old box, I'd do it mys.... (Ooops, can I say that?) - Wayne -----Original Message----- From: Rick [mailto:rick.pitcher(at)verizon.net] Subject: AeroElectric-List: Narco Com 120 gears I need to replace one of the little plastic gears in the frequency selector mechanism on a Narco Com 120.I called the factory and they want me to ship them the radio and $400 or $500. It's obviously not worth spending that much on a 20 year old radio. Is there another source for these gears? Rick Pitcher ________________________________________________________________________________
Date: Jan 31, 2003
From: "Brad Benson" <brad@cds-inc.com>
Subject: Re: Narco Com 120 gears
I don't know about the gears, but I've seen Com 120s on Ebay for relatively cheap : http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&item=2401916981&category=26436 Certainly better than handing over a fistful of cash to Narco or redoing your panel around something else.... Thanks! Brad "Sharpie" Benson RV6AQB underway... "Please buy my software, it's funding my RV6A project!" - http://www.notamd.com *********** REPLY SEPARATOR *********** On 1/31/2003 at 12:07 AM Rick wrote: > > >I need to replace one of the little plastic gears in the frequency >selector mechanism on a Narco Com 120.I called the factory and they want >me to ship them the radio and $400 or $500. >It's obviously not worth spending that much on a 20 year old radio. Is >there another source for these gears? > >Rick Pitcher > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Narco Com 120 gears
Date: Jan 31, 2003
Might check to see if the older non-approved COMs have the same gears. Cy Galley - Bellanca Champion Club Newsletter Editor & EAA TC www.bellanca-championclub.com We support Aeroncas ----- Original Message ----- From: "Brad Benson" <brad@cds-inc.com> Subject: Re: AeroElectric-List: Narco Com 120 gears > > > I don't know about the gears, but I've seen Com 120s on Ebay for relatively cheap : > > http://cgi.ebay.com/ebaymotors/ws/eBayISAPI.dll?ViewItem&item=2401916981&cat egory=26436 > > Certainly better than handing over a fistful of cash to Narco or redoing your panel around something else.... > > Thanks! > Brad "Sharpie" Benson > RV6AQB underway... > "Please buy my software, it's funding my RV6A project!" - http://www.notamd.com > > *********** REPLY SEPARATOR *********** > > On 1/31/2003 at 12:07 AM Rick wrote: > > > > > > >I need to replace one of the little plastic gears in the frequency > >selector mechanism on a Narco Com 120.I called the factory and they want > >me to ship them the radio and $400 or $500. > >It's obviously not worth spending that much on a 20 year old radio. Is > >there another source for these gears? > > > >Rick Pitcher > > > > > > ________________________________________________________________________________
From: "Jim & Jeanette Oberst" <joberst@cox-internet.com>
Subject: Re: Right Angle BNC
Date: Jan 31, 2003
I recently bought a male-to-female right angle BNC connector at Radio Shack. Jim Oberst ----- Original Message ----- From: <DHPHKH(at)aol.com> Subject: AeroElectric-List: Right Angle BNC > > Gang, > A few months ago somebody asked about crimp-on right angle female BNC connectors. Bob mentioned using a right angle adapter. Has anyone yet found a source for a decent crimp-on right angle? > > Dan > > ________________________________________________________________________________
Date: Jan 31, 2003
From: Richard Dudley <rhdudley(at)att.net>
Subject: Re: Low Cost Ground Power Jack .....
Bob, I believe that I have found the answer to my own question. The symbol that I took as a circuit breaker is a switch breaker. Then the operating procedure would be to connect the external power which could be confirmed by the push-to-test light. The switch breaker would have control of the contactor and would have to be switched off at the end of the transfer to avoid the battery holding the contactor closed. Regards, Richard Dudley Richard Dudley wrote: > > > Bob, > > I like the idea of having a ground power jack for the reasons you list > in your paper. I have ordered the parts to install one. > > In re-reviewing the schematic (Fig. 3) I am having a problem > understanding how the ground power contactor can release when the > external power is removed. It seems to me that, since it is connected to > the aircraft battery positive, that contactor will remain energized > after the external power is removed; with the only recourse being to > pull the circuit breaker to unlatch the contactor. > > What am I missing? > > Regards, > > Richard Dudley > ________________________________________________________________________________
Date: Jan 31, 2003
From: Rick <rick.pitcher(at)verizon.net>
Subject: Re: Narco Com 120 gears
You guys sure are a helpful lot : ) Besides the answers I got here on the list, I got several more emails at home with suggestions. I was thinking about making an aluminum replacement on a lathe, but went out to the local avionics shop and was able to buy a "core" with a decent set of gears in it. I went through 3 radios before I found one that didn't have too much damage on the same gear. The one I ended up buying had a little crack already starting, but I laid a bead of epoxy alongside the gear and bonded it to the aluminum hub it is pressed onto. It works great, hopefully it will KEEP working. Thanks, Rick Pitcher http://lightflyers.com/Zodiac.html ________________________________________________________________________________
From: "Wayne Sweet" <wsweet(at)attbi.com>
Subject: Coaxial cables
Date: Jan 31, 2003
The Chief Aircraft catalog has 3 different types of coaxial cable: RG-58 (50 ohm), RG-142 (low loss for DME/TPX/GPS) and RG-400(low loss for GPS). I have used only the multi-stranded RG58 in my homebuilt for all the radios, not knowing about the other two. Why the other two??? Wayne ________________________________________________________________________________
Date: Jan 31, 2003
From: richard(at)riley.net
Subject: Re: Right Angle BNC
> > > > > >Gang, > > A few months ago somebody asked about crimp-on right angle female BNC > > connectors. Bob mentioned using a right angle adapter. Has anyone yet > > found a source for a decent crimp-on right angle? > > There are a number of sources . . . but none that > I know of that will install with the tool we sell. > AMP 225974-2 is a suitable part that sells for $22.00 > qty of 1. The hand tool that installs it is about $400.00 Ouch. > If it were my airplane, I'd install a cable male connector, > mate it with a right angle adapter and shrink a chunk > of double walled tubing over the interface to make it > permanent. . . . the po' boy's right angle connector. I've done that in the past, and it's seemed to work fine for me. But someone who *says* that they know RF tells me that you loose a lot of energy out the angle unless it's a super special very expensive right angle that has a little horseshoe magnet in it. Any truth to that? ________________________________________________________________________________
From: N2165v(at)aol.com
Date: Feb 01, 2003
Subject: King connector
Gulf Coast Avionics sells a compatible coax connector (p/n 9-30-10 tray mount connector) for $20. Thanks ________________________________________________________________________________
From: "Cliff Shaw" <flyinggpa(at)attbi.com>
Subject: KX125 wireing
Date: Feb 01, 2003
All I am wiring my Panel. My Bendix/King KX125 has three output lines labeled "AUX AUDIO 1 , 2 , 3 ". What are they used for? I am trying to figure out the audio wiring of this thing. Cliff Shaw 1041 Euclid ave. Edmonds WA 98020 (425) 776-5555 Europa XS N229WC "Wile E Coyote" ________________________________________________________________________________
Date: Feb 01, 2003
From: Bernie_C(at)erols.com
Subject: Re: Right Angle BNC
What about these guys?? <<http://www.pasternack.com/catalog.asp?RecNo=0&partNum=pe4345>> <<http://www.pasternack.com/catalog.asp?RecNo=0&partNum=pe4053>> The 4053 is solder. No special tools. Bernie C. "Robert L. Nuckolls, III" wrote: > > > > > >Gang, > > A few months ago somebody asked about crimp-on right angle female BNC > > connectors. Bob mentioned using a right angle adapter. Has anyone yet > > found a source for a decent crimp-on right angle? > > There are a number of sources . . . but none that > I know of that will install with the tool we sell. > AMP 225974-2 is a suitable part that sells for $22.00 > qty of 1. The hand tool that installs it is about $400.00 > > If it were my airplane, I'd install a cable male connector, > mate it with a right angle adapter and shrink a chunk > of double walled tubing over the interface to make it > permanent. . . . the po' boy's right angle connector. > > Bob . . ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: RF right angle
Date: Feb 01, 2003
Rick, "I've done that in the past, and it's seemed to work fine for me. But someone who *says* that they know RF tells me that you lose a lot of energy out the angle unless it's a super special very expensive right angle that has a little horseshoe magnet in it. Any truth to that? " Maybe that little horseshoe is an Omega sign - ohms impedance? The ideal is 50ohms for RF. I have one marked "CBWU UG306A". I think that's OK for impedance but beware of rim-etched "CARO UG306/U" as no record of producer. Not a horseshoe in a barrel, nor could I find a crimp version. These are all twist&lock for RG58 coaxial cable. Good Luck, Ferg ________________________________________________________________________________
From: "Rob W M Shipley" <Rob(at)RobsGlass.com>
Subject: Switches and AC
Date: Feb 01, 2003
Hey Bob, I saw this in the RV digest and would like your comments. Subject: RV-List: Re: [ExperimentalAvionics] off topic request Hi.. I agree completely with what Marshall just said about using a relay to handle current, but would add that believing the rating of a switch can be VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the ground twice before realizing that the Mag switch that was rated at 20Amps AC is only good for about 1/10th that in DC. It arched across the contacts and shut the magneto off by grounding it. If you do go with a switch and it operates on DC, make sure the switch has the current rating you need for DC Hope this helps someone avoid my impromptu soaring lession Ron DeWees Atlanta, Ga ----- Original Message ----- From: "Marshall M. Dues" <mmdues@hal-pc.org > For switching rather high current (10 to 20 amp) circuits, it is better > to use a lesser rated switch to control a small Bosch type relay that > uses 30 to 40 amp contacts to turn on the heavier loads, like landing > lights, etc. These little relays are popular in most German vehicles. > They are available at most auto parts stores. I used them exclusively > to turn on halogen type landing and taxi lights on my RV-6. Never had a > failure in 675 hours. Switching heavy currents through a toggle switch > makes for relatively short life of the switch. The contacts arc each > time they make and break, and soon they either weld themselves shut, or > simply carbon themselves over and won't make next time they are turned > on. > Marshall Dues Katy, Texas RV-6 N243MD It sounds like a way of ontroducing more failure points if the available switches are actually up to snuff. How's Dee? Making good progress I hope. Rob Rob W M Shipley RV9A N919RV Fuselage. ________________________________________________________________________________
Date: Feb 01, 2003
Subject: Re: landing lights
From: "Robert Dickson" <robert@thenews-journal.com>
Bernie thanks for the reply. I think you're right about a larger fuse being needed. I've got another question, however. Given that I'm going to run the two landing lights to one switch using 14awg wires, is it ok to power that switch using 14awg or should I bump that part of the run from the main bus(very short) to a larger size? The answer to this is probably in the Connection, but I'm just not sure what's going on with a two-branch circuit like this. Robert Dickson RV-6A electrical ---------- >From: deltaB(at)erols.com >To: robert@thenews-journal.com >Subject: Re: AeroElectric-List: landing lights >Date: Fri, Jan 31, 2003, 7:22 PM > > I didn't see any replies to your question on this thread. > > You still only need to protect the 12 gauge wire with a single > fuse. I'm sure you will find a rating that is low enough to protect > the wire, yet high enough not to nuisance trip on the 100 watt > load. (15 amps if the numbers below are to be believed) The > proponents of the independent fusing/switching are allowing for > failures to affect one light without the other. A 10 amp fuse may > be a little close to the inrush current of the 9 amp load to use. > > Bernie C. > > Robert Dickson wrote: >> > <robert@thenews-journal.com> >> >> I've installed the RMD wingtip landing lights on my RV. These use H7604 50w >> bulbs. I would like to wire these to one switch, but I've got a couple of >> issues. >> First, RMD supplied #12 wire for these lights, which seems too large for the >> wattage and length of run. >> Second, in searching the RV list archive for what other folks have done for >> wiring these lights, I came across the following post from Bob (Aug 99): >> >> If you're going to have a landing light in each >> wing, you need a breaker/fuse and switch for EACH light. >> 50 watt bulbs draw 4.5 amps, 100 watt bulbs 9 amps, 150 >> watt bulbs draw 13.5 amps. Wire sizes and breakers >> purely for current carrying considerations are 20AWG/7A; >> 18AWG/10A, and 14AWG/15A for each lamp. >> >> In a metal airplane, voltage drops in wires selected >> for current rating alone are generally insignificant. >> You need to be looking at runs of 20+ feet before I'd >> be concerned about voltage drops. >> >> So, do I really need to have a switch for each light? If I don't, would >> 14awg wire and a 10amp fuse be appropriate for the 2 light circuit? >> >> thanks, >> >> Robert Dickson >> RV-6A electrical >> ________________________________________________________________________________
Date: Feb 01, 2003
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Bar Lamps from MPJA
Here's a link to the bar lamps I purchased from MPJA last year after seeing a message to the A-list from Jim Foerster about them. (thanks for the tip, Jim!) They are apparently still available and are rectangular, modular units that have grooves on the top and sides so they can be "stacked" together, as many as you like, and have 2 parallel bulbs in each- for details see: http://www.mpja.com/product.asp?product=5072+LA I am using these to assemble a "poor mans" annunciator and they may work out just fine- for fifteen cents each, I bought 50 of 'em! I measured them at about 160ma @14VDC, or about 2.25 watts (if my math is correct!). Not assembled yet, but we'll see... From The PossumWorks in TN Mark - Jim's original message below: For those who want to build their own annunciator lights, the nicest system I have seen uses 1.5in by 3/8 in bar lights, which have two 12 volt bulbs, draw 180 ma, and have stacking tongue and groove slots so that they can be stacked horizontally, vertically, or variations of these. A colored plastic sheet with lettering can be run through your laser printer to make whatever lable you want, and because the lighted area is 1.5 by 1/4, the lable can have 6 to 10 letters. The lamps glow at a medium intensity, suggesting that they should be good for thousands of hours. The price? 20 cents each, 15 cents for 10 or more. I got 30 of them. see http://www.mpja.com/product.asp?product5072+LA for the picture. These use 0.187 faston tabs. Jim Foerster ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: KX125 wireing
> >All > >I am wiring my Panel. My Bendix/King KX125 has three output lines labeled >"AUX AUDIO 1 , 2 , 3 ". What are they used for? I am trying to figure out >the audio wiring of this thing. > > >Cliff Shaw >1041 Euclid ave. >Edmonds WA 98020 >(425) 776-5555 > Europa XS N229WC "Wile E Coyote" Many nav/coms of years gone by had auxiliary audio INPUTS to their audio amplifiers that could be used to mix outputs from other sources together into the same headphone/speaker signals. I suspect that's what these are. Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Right Angle BNC
> > > If it were my airplane, I'd install a cable male connector, > > mate it with a right angle adapter and shrink a chunk > > of double walled tubing over the interface to make it > > permanent. . . . the po' boy's right angle connector. > >I've done that in the past, and it's seemed to work fine for me. But >someone who *says* that they know RF tells me that you loose a lot of >energy out the angle unless it's a super special very expensive right angle >that has a little horseshoe magnet in it. Any truth to that? Nope . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Coaxial cables
> >The Chief Aircraft catalog has 3 different types of coaxial cable: RG-58 >(50 ohm), RG-142 (low loss for DME/TPX/GPS) and RG-400(low loss for GPS). >I have used only the multi-stranded RG58 in my homebuilt for all the >radios, not knowing about the other two. Why the other two??? >Wayne RG-58 is an obsolete spec coax of WWII era using PVC and polyethylene insulations and single braid shield. Hasn't been used in a production aircraft for decades. RG400 cousins are lower loss, double shielded, modern insulation products that march along hand-in-hand with tefzel insulated wires for the rest of your airplane. It's the year-2003 way to go. Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Right Angle BNC
> >To: aeroelectric-list(at)matronics.com > >What about these guys?? > > ><<http://www.pasternack.com/catalog.asp?RecNo=0&partNum=pe4345>> > > ><<http://www.pasternack.com/catalog.asp?RecNo=0&partNum=pe4053>> > >The 4053 is solder. No special tools. That will work. ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Switches and AC
Date: Feb 02, 2003
For an application like this, I would suggest the Perfect Cubes, which are solid state devices that Eric Jones is building. I have been testing these units the past couple weeks, and have found their performance to be great. They draw very little current to turn them on, so your switches should last for a long time with little degradation. The cubes themselves, being solid state, will far outlast any relay. Just something to think about. I'm using these for my taxi lights (11A), landing lights (11A), pitot heat (7A), Navs (5A), and strobes (7A). I'm using Eric's larger units called the Powerlink JR on my gear up and down (35A) and my avionics busses (15A and 22A). No relays in my plane :) (well, hopefully someday) Eric is also working on a larger unit, called a Powerlink, that will hopefully be able to replace the stardard battery contactors and handle 200A+. I have a prototype, and hope to test it soon. Eric has some other cool products too, like the super diodes, a wig wag flasher, and is working on LED bulbs. All kinds of cool electronic gadgets that should make our planes safer. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rob W M Shipley Subject: AeroElectric-List: Switches and AC Hey Bob, I saw this in the RV digest and would like your comments. Subject: RV-List: Re: [ExperimentalAvionics] off topic request Hi.. I agree completely with what Marshall just said about using a relay to handle current, but would add that believing the rating of a switch can be VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the ground twice before realizing that the Mag switch that was rated at 20Amps AC is only good for about 1/10th that in DC. It arched across the contacts and shut the magneto off by grounding it. If you do go with a switch and it operates on DC, make sure the switch has the current rating you need for DC Hope this helps someone avoid my impromptu soaring lession Ron DeWees Atlanta, Ga ----- Original Message ----- From: "Marshall M. Dues" <mmdues@hal-pc.org > For switching rather high current (10 to 20 amp) circuits, it is better > to use a lesser rated switch to control a small Bosch type relay that > uses 30 to 40 amp contacts to turn on the heavier loads, like landing > lights, etc. These little relays are popular in most German vehicles. > They are available at most auto parts stores. I used them exclusively > to turn on halogen type landing and taxi lights on my RV-6. Never had a > failure in 675 hours. Switching heavy currents through a toggle switch > makes for relatively short life of the switch. The contacts arc each > time they make and break, and soon they either weld themselves shut, or > simply carbon themselves over and won't make next time they are turned > on. > Marshall Dues Katy, Texas RV-6 N243MD It sounds like a way of ontroducing more failure points if the available switches are actually up to snuff. How's Dee? Making good progress I hope. Rob Rob W M Shipley RV9A N919RV Fuselage. ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Wiring headset jacks 2nd try
Date: Feb 03, 2003
As I've got no answer I repost this message Dear all, another question where I'm a bit uncertain, even after reading Bob's Shop Notes and comparing them with the Seminar wirebook. Maybe Bob, if you read this could you comment? Bob, in the shop note you say, that you use 3 wire shielded, and the shield itself is connected on both (?) sides to the Mic LO, did you use the 3 wire because of wiring both mic's to only 4 ports? (You used the shielding instead of one wire). I have a used Garmin 340, where I have a separate port for each mic/phone, should I use a 2wire shielded for each mic using the shield as the third wire (if yes, which contact should be wired with the shield)? Same for the phones, if I use the same approach I could use a 1wire shielded wire for the two contacts. It would save weight and money. Many thanks for your feedback Werner ________________________________________________________________________________
From: PTACKABURY(at)aol.com
Date: Feb 03, 2003
Subject: Re: Dual Alt, Dual Battery Installation
Bob: I am building an unpressurized Lancair IV and am designing the power distribution to support all electric dual electronic ignition operation (no vacuum, no mags). I am therefore using your Z-14 diagram as the foundation for the dual alt, dual battery installation. My question: what criteria should I use to size the second alternator and second battery? I would like to save weight where possible and yet insure these devices are capable of supporting what ever load an emergency might require. thank you, paul ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: 10265 Sherick
> >Thanks for the reply to my previous email concerning antenna ground >planes. I did review the antenna section in your (nicely done) book and >it brings up a couple more questions that I hope you will comment on. > >I am using a Comant COMM antenna (swept back version) on the e-glass belly >pan. I have a total space of 24" wide x 48" long for a ground plane >area. The Comm antenna is back from a Transponder antenna, which is >placed forward on the belly pan. > >Question: Can I use the copper tape approach for the COMM antenna with the >limited belly pan width of 24 inches? Or, is it possible to just use a >single piece of aluminum 24" x 48" for the ground plane for both the COMM >and Transponder antennas? Which approach might be more effective as a >ground plane? One never achieves an ideal ground plane on small aircraft. ANY ground plane is better than NO ground plane. Do the best you can and don't worry about it. Radials can run up the contours and still be VERY effective. It's the length that is magic, not the "flatness" . . . any hunk of aluminum you can fit in there will probably be adequate also. >Regarding the Marker Beacon antenna: You indicate a "sled" type approach >75" in length. Bob Archer has a 1" wide copper tape version 40" long. Is >either approach OK the the Marker Beacon antenna requirement? Also, how >for from the COMM ground plane should the Marker Beacon antenna be located? That 75" figure is an error . . . which you are the first one to bring it to my attention. 75MHz marker beacon is 4 meters full wavelength making a 1/4 wave antenna 1 meter long or 40". The 40" internal antenna wire would be fine. It can begin at the edge of your aluminum sheet ground plane. Ground shield of marker beacon coax to ground plane and connect center conductor of coax to 40' piece of wire that is straight as possible but again, length is magic, straightness is less important. Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Low Cost Ground Power Jack .....
> >Bob, >I believe that I have found the answer to my own question. The symbol >that I took as a circuit breaker is a switch breaker. Then the operating >procedure would be to connect the external power which could be >confirmed by the push-to-test light. The switch breaker would have >control of the contactor and would have to be switched off at the end of >the transfer to avoid the battery holding the contactor closed. > >Regards, > >Richard Dudley You got it! ________________________________________________________________________________
Date: Feb 03, 2003
Subject: Re: Switches and AC
From: Walter Casey <mikec(at)caseyspm.com>
Shannon, How do we contact Eric Jones. On Sunday, February 2, 2003, at 10:04 AM, Shannon Knoepflein wrote: > > > For an application like this, I would suggest the Perfect Cubes, which > are solid state devices that Eric Jones is building. I have been > testing these units the past couple weeks, and have found their > performance to be great. They draw very little current to turn them > on, > so your switches should last for a long time with little degradation. > The cubes themselves, being solid state, will far outlast any relay. > Just something to think about. > > I'm using these for my taxi lights (11A), landing lights (11A), pitot > heat (7A), Navs (5A), and strobes (7A). I'm using Eric's larger units > called the Powerlink JR on my gear up and down (35A) and my avionics > busses (15A and 22A). No relays in my plane :) (well, hopefully > someday) > > Eric is also working on a larger unit, called a Powerlink, that will > hopefully be able to replace the stardard battery contactors and handle > 200A+. I have a prototype, and hope to test it soon. > > Eric has some other cool products too, like the super diodes, a wig wag > flasher, and is working on LED bulbs. All kinds of cool electronic > gadgets that should make our planes safer. > > --- > Shannon Knoepflein <---> kycshann(at)kyol.net > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rob > W > M Shipley > To: AeroElectric-List Digest Server > Subject: AeroElectric-List: Switches and AC > > > > Hey Bob, > I saw this in the RV digest and would like your comments. > > Subject: RV-List: Re: [ExperimentalAvionics] off topic request > Hi.. I agree completely with what Marshall just said about using a > relay > to > handle current, but would add that believing the rating of a switch can > be > VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the > ground > twice before realizing that the Mag switch that was rated at 20Amps AC > is > only good for about 1/10th that in DC. It arched across the contacts > and > shut the magneto off by grounding it. If you do go with a switch and > it > operates on DC, make sure the switch has the current rating you need > for > DC > Hope this helps someone avoid my impromptu soaring lession > Ron DeWees Atlanta, Ga > > ----- Original Message ----- From: "Marshall M. Dues" > <mmdues@hal-pc.org >> For switching rather high current (10 to 20 amp) circuits, it is > better >> to use a lesser rated switch to control a small Bosch type relay that >> uses 30 to 40 amp contacts to turn on the heavier loads, like landing >> lights, etc. These little relays are popular in most German vehicles. >> They are available at most auto parts stores. I used them exclusively >> to turn on halogen type landing and taxi lights on my RV-6. Never had > a >> failure in 675 hours. Switching heavy currents through a toggle > switch >> makes for relatively short life of the switch. The contacts arc each >> time they make and break, and soon they either weld themselves shut, > or >> simply carbon themselves over and won't make next time they are turned >> on. >> Marshall Dues Katy, Texas RV-6 N243MD > > It sounds like a way of ontroducing more failure points if the > available > switches are actually up to snuff. > > How's Dee? Making good progress I hope. > Rob > Rob W M Shipley > RV9A N919RV Fuselage. > > > _- > ====================================================================== > _- > ====================================================================== > _- > ====================================================================== > _- > ====================================================================== > > ________________________________________________________________________________
Date: Feb 03, 2003
From: "Mark A. Wood" <Mark.Wood(at)uvm.edu>
Subject: PTT switches
Hello all Forgive me if this has been addressed before, I am new to this list and did not have luck running the archives. I was wiring a PTT switch for my hand held 520 JRC radio. It seems to work better and shut off faster if I use only a single switch from the tip of the plug to the ground, and leave the center connector to center connector connection connected rather then disconnecting them with a second switch when I release the PTT switch. ( I hope that is understandable to people.) Does anyone have feelings on weather or not I should leave this as a single switch or double it up and disconnect the center connectors? _____________________ _____ l \/ \ ___________l_________/\_____/ ground center tip Thanks Mark Wood ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: 10267 Strickland
> >I'm an RV-6 builder and I'm building your dual alt/single battery >electrical system (Figure Z-12 in revision 10.) I have a couple of questions: > >1) I'm running a dual electronic ignition (Light Speed Engineering, Klaus >Saviors system) and he recommends I connect to the battery, by-passing any >busses. He also recommends a 5 amp circuit breaker. Your schematic shows >electronic ignition coming off the battery bus. I'm a total fan of your >design and was planning on running one electronic ignition, via the fuse >block, off the battery bus and the other off the essential bus, what >should I do? I think I'd run both of them off the battery bus. Each on with it's own fuse. . . . since this is an electrically dependent engine, you might consider adding a second battery, (even if just a small, 6-8 a.h. device), a battery relay (mini-contactor) to support one of ignition systems. >2)Your schematic shows a circuit braker for the alt fld, lv warn, and >start. How do I connect a circuit breaker to the fuse block? Those diagrams are generic depictions of architectures. If you use fuse blocks, then only the ALT FLD gets a breaker on an EXTENSION of the bus created by fusible link connection to the main feedpoint bolt of the fuseblock. (See Figure Z-11) If you use breakers as depicted in Z-12, then everything feeds from your fabricated bus via breakers. Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Switches and AC
> >Hey Bob, >I saw this in the RV digest and would like your comments. > >Subject: RV-List: Re: [ExperimentalAvionics] off topic request >Hi.. I agree completely with what Marshall just said about using a relay to >handle current, but would add that believing the rating of a switch can be >VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the ground >twice before realizing that the Mag switch that was rated at 20Amps AC is >only good for about 1/10th that in DC. It arched across the contacts and >shut the magneto off by grounding it. If you do go with a switch and it >operates on DC, make sure the switch has the current rating you need for DC >Hope this helps someone avoid my impromptu soaring lession >Ron DeWees Atlanta, Ga See: http://www.aeroelectric.com/articles/swtchrat.pdf ________________________________________________________________________________
From: "Steve Sampson" <SSampson.SLN21(at)london.edu>
Subject: LEDs
Date: Feb 03, 2003
I am about to order some LEDs. Roughly how many mcd do I need for the following: 1. For a red flood for the cabin if all else fails so I can see in dim light? 2. A white one to provide some light in the baggage compartement to find something in the dark when the plane is parked? Thanks, Steve. ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: RE: Dual battery / Dual Alternator in composite canard
pusher boeing.com> >Bob, > >I managed to work this one out myself (like I should have in the first >place). The listed connections in the email below are incorrect. I now have: > >1. 2AWG all the way from Main battery to engine crankcase ground. >2. Ground strap from engine crankcase ground to firewall fast on ground >bus (5/16" brass bolt). >3. 4AWG from firewall fast on ground bus (5/16" brass bolt) to instrument >panel fast on ground bus (5/16" brass bolt). >4. 2AWG from Aux battery to firewall fast on ground bus (5/16" brass bolt). > >Unless you have any further comment, I'll move fwd with this plan. > >- Wayne Take a look at http://216.55.140.222/temp/CPDBFB.pdf Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Switches and AC
> > >I'm using these for my taxi lights (11A), landing lights (11A), pitot >heat (7A), Navs (5A), and strobes (7A). A 7A "rated" toggle or rocker switch would run for thousands of cycles in any of these applications. > I'm using Eric's larger units >called the Powerlink JR on my gear up and down (35A) and my avionics >busses (15A and 22A). Avionics busses?????? how come? Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Dual Alt, Dual Battery Installation
> > >Bob: I am building an unpressurized Lancair IV and am designing the power >distribution to support all electric dual electronic ignition operation (no >vacuum, no mags). I am therefore using your Z-14 diagram as the foundation >for the dual alt, dual battery installation. My question: what criteria >should I use to size the second alternator and second battery? I would like >to save weight where possible and yet insure these devices are capable of >supporting what ever load an emergency might require. thank you, paul You haven't got many choices for vacuum pump driven alternators. There's an 8A and a 20A device currently on the market. The 8A is probably too small, so go with the SD-20. Bob . . . p.s. please don't think of ANY failure in your electrical system as being worthy of calling it an EMERGENCY. If we don't end up with a system that takes ANY failure as a ho-hum, no-sweat event, then we haven't done our homework. ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Wiring headset jacks 2nd try
> Bob, in the shop note you say, that you use 3 wire shielded, and the shield > itself is connected on both (?) sides to the Mic LO, did you use the 3 wire > because of wiring both mic's to only 4 ports? (You used the shielding > instead of one wire). The shop notes are one example of suitable wiring as it applies to the 760VHF that has one PTT and two mic inputs for the pair crew stations. This means I have three active wires departing the radio and the need for one ground return. I had some 3-conductor shielded and the drawing illustrates a technique for using wire on hand for this task. > I have a used Garmin 340, where I have a separate port for each mic/phone, > should I use a 2wire shielded for each mic using the shield as the third > wire (if yes, which contact should be wired with the shield)? Same for the > phones, if I use the same approach I could use a 1wire shielded wire for >the > two contacts. It would save weight and money. Here's a wirebook I did for a 430/340 combo in the AGATE Bonanza a few years ago. http://216.55.140.222/temp/gns430.pdf Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: PTT switches
> >Hello all >Forgive me if this has been addressed before, I am new to this list >and did not have luck running the archives. > >I was wiring a PTT switch for my hand held 520 JRC radio. It seems to >work better and shut off faster if I use only a single switch from >the tip of the plug to the ground, and leave the center connector to >center connector connection connected rather then disconnecting them >with a second switch when I release the PTT switch. ( I hope that is >understandable to people.) >Does anyone have feelings on weather or not I should leave this as a >single switch or double it up and disconnect the center connectors? > >_____________________ _____ > l \/ \ >___________l_________/\_____/ >ground center tip > >Thanks >Mark Wood You difficult to argue with success . . . but if what you're doing is contrary to manufacturer's instructions, there is some risk that requirements unknown to us are not being satisfied. Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: LEDs
> > >I am about to order some LEDs. Roughly how many mcd do I need for the >following: > >1. For a red flood for the cabin if all else fails so I can see in dim >light? >2. A white one to provide some light in the baggage compartement to >find something in the dark when the plane is parked? The human eye is an amazing device with a huge dynamic range. ANY high output led (600 MCD or more) will produce usable results for total light output. You may find that the light doesn't spread enough for convenient use which may drive a need for multiple lamps. It's a an experiment that may well dictate changes to whatever you put in the first time. Bob . . . ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Switches and AC
Date: Feb 02, 2003
Eric M. Jones emjones(at)charter.net He's on this list. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Walter Casey Subject: Re: AeroElectric-List: Switches and AC Shannon, How do we contact Eric Jones. On Sunday, February 2, 2003, at 10:04 AM, Shannon Knoepflein wrote: > > > For an application like this, I would suggest the Perfect Cubes, which > are solid state devices that Eric Jones is building. I have been > testing these units the past couple weeks, and have found their > performance to be great. They draw very little current to turn them > on, > so your switches should last for a long time with little degradation. > The cubes themselves, being solid state, will far outlast any relay. > Just something to think about. > > I'm using these for my taxi lights (11A), landing lights (11A), pitot > heat (7A), Navs (5A), and strobes (7A). I'm using Eric's larger units > called the Powerlink JR on my gear up and down (35A) and my avionics > busses (15A and 22A). No relays in my plane :) (well, hopefully > someday) > > Eric is also working on a larger unit, called a Powerlink, that will > hopefully be able to replace the stardard battery contactors and handle > 200A+. I have a prototype, and hope to test it soon. > > Eric has some other cool products too, like the super diodes, a wig wag > flasher, and is working on LED bulbs. All kinds of cool electronic > gadgets that should make our planes safer. > > --- > Shannon Knoepflein <---> kycshann(at)kyol.net > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rob > W > M Shipley > To: AeroElectric-List Digest Server > Subject: AeroElectric-List: Switches and AC > > > > Hey Bob, > I saw this in the RV digest and would like your comments. > > Subject: RV-List: Re: [ExperimentalAvionics] off topic request > Hi.. I agree completely with what Marshall just said about using a > relay > to > handle current, but would add that believing the rating of a switch can > be > VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the > ground > twice before realizing that the Mag switch that was rated at 20Amps AC > is > only good for about 1/10th that in DC. It arched across the contacts > and > shut the magneto off by grounding it. If you do go with a switch and > it > operates on DC, make sure the switch has the current rating you need > for > DC > Hope this helps someone avoid my impromptu soaring lession > Ron DeWees Atlanta, Ga > > ----- Original Message ----- From: "Marshall M. Dues" > <mmdues@hal-pc.org >> For switching rather high current (10 to 20 amp) circuits, it is > better >> to use a lesser rated switch to control a small Bosch type relay that >> uses 30 to 40 amp contacts to turn on the heavier loads, like landing >> lights, etc. These little relays are popular in most German vehicles. >> They are available at most auto parts stores. I used them exclusively >> to turn on halogen type landing and taxi lights on my RV-6. Never had > a >> failure in 675 hours. Switching heavy currents through a toggle > switch >> makes for relatively short life of the switch. The contacts arc each >> time they make and break, and soon they either weld themselves shut, > or >> simply carbon themselves over and won't make next time they are turned >> on. >> Marshall Dues Katy, Texas RV-6 N243MD > > It sounds like a way of ontroducing more failure points if the > available > switches are actually up to snuff. > > How's Dee? Making good progress I hope. > Rob > Rob W M Shipley > RV9A N919RV Fuselage. > > > _- > ====================================================================== > _- > ====================================================================== > _- > ====================================================================== > _- > ====================================================================== > > ________________________________________________________________________________
From: "Dan Checkoway" <dan(at)rvproject.com>
Subject: switch keyway question
Date: Feb 03, 2003
Sorry if the answer to this is obvious... I'm still in the panel planning phase...haven't bought any switches or cut any holes yet. When drilling your panel for toggle switches, is the keyway slot generally ignored? I mean...maybe if you have the panel laser cut you could have the keyway notch integrated into the cutout, but when drilling your own 15/32" holes there doesn't seem to be a good way to do this. Does simply using a lock washer of some sort prevent switch rotation? )_( Dan RV-7 N714D (fuselage/finish) http://www.rvproject.com ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Switches and AC
Date: Feb 02, 2003
Bob, ....per comments about switches versus solid state devices.... I stick with 1,000,000 cycles, thanks. No big deal, but to each his own, and in this case I'll stick with my way. You always want people to tell you why. Well, in this case, my reason is quite simple.....1,000,000+ cycles is better than 1,000. Solid state devices will always win when it becomes a battle of dependability, especially where vibration is a concern. Also, the solid state devices have thermal shutout protection modes that no switch or relay have. The sizes and weight are also much less for the solid state devices. The cube (20A) is about the size of a dice, the powerlink jr (35A) is the size of a domino. In my design I haven't chosen to implement this, as they aren't 100% proven yet, but in the future, you won't even need fuses or circuit breakers with these devices and their protection modes.....if they draw too much current, they trip out until the current reaches a normal level. This would be a highly simplified system without CB's or fuses, and a lot less weight, AND no pilot thought/action required. Until they are proven and I have some hours on them, I chose to go a more traditional route.... http://www.lancaironline.net/pix/shannon-jan03/panel_cbs http://www.lancaironline.net/pix/shannon-jan03/panel_perfect_cube_2 with mounting the cubes DIRECTLY to the circuit breaker, as their tab is a Vin terminal also. ....per questions about avionics busses..... Bob, we've been through all this before on the avionics busses, http://shannon.v8eaters.com/images/lancair/ the spreadsheet with all the loads is there. My devices, Chelton Flight Systems EFIS 2000 system, are not DO-160 on the experimental side (and half the price versus the certified DO-160 version.....the certified version wasn't even available when I purchased mine though, so it wasn't an option), so they require a dedicated buss during starting. I realize this isn't ideal, but it is what I have chosen to work with, and I am quite happen with them. Therefore, I decided to design a system as simple and yet robust as possible within the design limits I chose by using the CFS EFIS. I think I've succeeded. Here's what I've done: The EFIS has to be behind an AV MASTER, no other way about it. I also like the convenience of an AV MASTER to simplify power up and down of my quite complex all electric panel. So, 1) I have to have it to protect my "wimpy" or "pampered" EFIS, and 2) I like the convenience. Also, since the EFIS is one of my essential flight instruments, it needs to be on an ESS buss, so basically I combined an ESS (or endurance as you call it now) buss and a AVIONICS buss together. My design is simple. There is a switch on the panel that controls a Powerlink Jr SSR. The Jr SSR is fed from the main buss through a diode and then on to the ESS AV devices. Now, this alone doesn't make it an ESS buss, so an ALT FEED switch will switch power directly to this ESS buss from the battery in a true emergency, just leaving on what I need, which the EFIS happens to be one of the devices. The only difference between my system and yours is instead of just the diode feeding the ESS buss, I added a interruptible power, so I can shut it off and make it an AV buss too and protect the EFIS during starting. To make this aspect as dependable as possible, I went beyond just a normal relay, and am using a solid state device. In true ESS buss form, this is all backed up by a ALT FEED switch. I think I've come up with the simplest system and the most robust that will fit my needs. I see no drawbacks. As always, I'm open to comments. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Subject: RE: AeroElectric-List: Switches and AC > > >I'm using these for my taxi lights (11A), landing lights (11A), pitot >heat (7A), Navs (5A), and strobes (7A). A 7A "rated" toggle or rocker switch would run for thousands of cycles in any of these applications. > I'm using Eric's larger units >called the Powerlink JR on my gear up and down (35A) and my avionics >busses (15A and 22A). Avionics busses?????? how come? Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: William Shaffer <shafferaviation(at)yahoo.com>
Subject: Switches and AC
Shannon Knoepflein wrote:--> AeroElectric-List message posted by: "Shannon Knoepflein" Eric M. Jones emjones(at)charter.net He's on this list. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Walter Casey Subject: Re: AeroElectric-List: Switches and AC Shannon, How do we contact Eric Jones. On Sunday, February 2, 2003, at 10:04 AM, Shannon Knoepflein wrote: > > > For an application like this, I would suggest the Perfect Cubes, which > are solid state devices that Eric Jones is building. I have been > testing these units the past couple weeks, and have found their > performance to be great. They draw very little current to turn them > on, > so your switches should last for a long time with little degradation. > The cubes themselves, being solid state, will far outlast any relay. > Just something to think about. > > I'm using these for my taxi lights (11A), landing lights (11A), pitot > heat (7A), Navs (5A), and strobes (7A). I'm using Eric's larger units > called the Powerlink JR on my gear up and down (35A) and my avionics > busses (15A and 22A). No relays in my plane :) (well, hopefully > someday) > > Eric is also working on a larger unit, called a Powerlink, that will > hopefully be able to replace the stardard battery contactors and handle > 200A+. I have a prototype, and hope to test it soon. > > Eric has some other cool products too, like the super diodes, a wig wag > flasher, and is working on LED bulbs. All kinds of cool electronic > gadgets that should make our planes safer. > > --- > Shannon Knoepflein <---> kycshann(at)kyol.net > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rob > W > M Shipley > To: AeroElectric-List Digest Server > Subject: AeroElectric-List: Switches and AC > > > > Hey Bob, > I saw this in the RV digest and would like your comments. > > Subject: RV-List: Re: [ExperimentalAvionics] off topic request > Hi.. I agree completely with what Marshall just said about using a > relay > to > handle current, but would add that believing the rating of a switch can > be > VERY hazardous to you health. I rode a "quiet" 2 cycle engine to the > ground > twice before realizing that the Mag switch that was rated at 20Amps AC > is > only good for about 1/10th that in DC. It arched across the contacts > and > shut the magneto off by grounding it. If you do go with a switch and > it > operates on DC, make sure the switch has the current rating you need > for > DC > Hope this helps someone avoid my impromptu soaring lession > Ron DeWees Atlanta, Ga > > ----- Original Message ----- From: "Marshall M. Dues" > >> For switching rather high current (10 to 20 amp) circuits, it is > better >> to use a lesser rated switch to control a small Bosch type relay that >> uses 30 to 40 amp contacts to turn on the heavier loads, like landing >> lights, etc. These little relays are popular in most German vehicles. >> They are available at most auto parts stores. I used them exclusively >> to turn on halogen type landing and taxi lights on my RV-6. Never had > a >> failure in 675 hours. Switching heavy currents through a toggle > switch >> makes for relatively short life of the switch. The contacts arc each >> time they make and break, and soon they either weld themselves shut, > or >> simply carbon themselves over and won't make next time they are turned >> on. >> Marshall Dues Katy, Texas RV-6 N243MD > > It sounds like a way of ontroducing more failure points if the > available > switches are actually up to snuff. > > How's Dee? Making good progress I hope. > Rob > Rob W M Shipley > RV9A N919RV Fuselage. > > > _- > ====================================================================== > _- you san go candhsales.com they have 50 amp DC aircraft relays for $7.95 ea. > ====================================================================== > _- > ====================================================================== > _- > ====================================================================== > > --------------------------------- ________________________________________________________________________________
From: PTACKABURY(at)aol.com
Date: Feb 03, 2003
Subject: Re: Dual Alt, Dual Battery Installation
Thanks Bob: 20A backup alternator it is. Now how do I size the backup battery? paul ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Switches and AC
> > >Bob, > >....per comments about switches versus solid state devices.... >I think I've come up with the simplest system and the most robust that >will fit my needs. I see no drawbacks. As always, I'm open to >comments. Fair 'nuf. ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: switch keyway question
> >Sorry if the answer to this is obvious... > >I'm still in the panel planning phase...haven't bought any switches or cut >any holes yet. > >When drilling your panel for toggle switches, is the keyway slot generally >ignored? I mean...maybe if you have the panel laser cut you could have the >keyway notch integrated into the cutout, but when drilling your own 15/32" >holes there doesn't seem to be a good way to do this. Does simply using a >lock washer of some sort prevent switch rotation? Ignore the keyway for cutting panel and then use anti-rotation washer that comes with switch. Hole layout for using these washers is shown on page 6 of: http://content.honeywell.com/sensing/prodinfo/tr/catalog/tl_series.pdf Note that tab on anti-rotation washer may be on the OPPOSITE side from switch keyway so the anti-rotation hole may need to be BELOW the main clearance hole. Bob . . . ________________________________________________________________________________
Date: Feb 03, 2003
From: Scot Stambaugh <sstambaugh(at)qualcomm.com>
Subject: Re: switch keyway question
My switches came with the washer that fits over the flat on the threaded shaft. The washer has a tab that is bent 90 deg. so I drilled a small hole next to the main switch mounting hole and clocked it properly to align the switch. This keeps the switches properly oriented during installation and keeps them that way during use. Because the switch can't turn during normal use, it also helps to prevent the switch nut from working loose. scot At 11:52 AM 2/3/2003, Dan Checkoway wrote: > >Sorry if the answer to this is obvious... > >I'm still in the panel planning phase...haven't bought any switches or cut >any holes yet. > >When drilling your panel for toggle switches, is the keyway slot generally >ignored? I mean...maybe if you have the panel laser cut you could have the >keyway notch integrated into the cutout, but when drilling your own 15/32" >holes there doesn't seem to be a good way to do this. Does simply using a >lock washer of some sort prevent switch rotation? > >)_( Dan >RV-7 N714D (fuselage/finish) >http://www.rvproject.com > > ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Dual Alt, Dual Battery Installation
Date: Feb 02, 2003
How can you size the altenator without even knowing what loads will be on it? I'd suggest doing a load analysis spreadsheet. There is one on my site, http://shannon.v8eaters.com/images/lancair/ get the spreadsheet, which you can use as a starting point/template. There is a 35A pad mount alternator available from GAMI in both a standard and a 90 degree mount. These are ~6# units. Also, Kelly Aerospace is developing a 70A unit that is pad mount. I imagine you are a little ways out from need the alternator, so I would suggest doing a load analysis, and then deciding what alternator to use. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of PTACKABURY(at)aol.com Subject: Re: AeroElectric-List: Dual Alt, Dual Battery Installation Thanks Bob: 20A backup alternator it is. Now how do I size the backup battery? paul ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Dual Alt, Dual Battery Installation
> > >Thanks Bob: 20A backup alternator it is. Now how do I size the backup >battery? paul I'd run a pair of 17 a.h. batteries. Every year, put a new battery in main alternator slot, move old main to aux battery slot, give old aux battery to grand-kids for their battery powered kiddie-car. This way, you always have a battery less than one year old, no battery more than two years old. This combination of 34 a.h. of demonstrable capacity combined with two engine driven power sources will provide you system integrity not available on the vast majority of aircraft flying in the world today. However, given the the way most light aircraft are used you could probably save a few dollars by running the batteries till they croak . . . with two alternators, your chances of getting caught with a dark panel are on the same order as having your propeller break off. Bob . . . ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Re: switch keyway question
Date: Feb 03, 2003
Hello Dan, if you drill the keyway switch (the 90 deg tab) first, there is no problem to drill the switch hole later, worked on my panel in about 10 cases. Werner (crimping and crimping and crimping.......) ----- Original Message ----- From: "Dan Checkoway" <dan(at)rvproject.com> Subject: AeroElectric-List: switch keyway question > > Sorry if the answer to this is obvious... > > I'm still in the panel planning phase...haven't bought any switches or cut > any holes yet. > > When drilling your panel for toggle switches, is the keyway slot generally > ignored? I mean...maybe if you have the panel laser cut you could have the > keyway notch integrated into the cutout, but when drilling your own 15/32" > holes there doesn't seem to be a good way to do this. Does simply using a > lock washer of some sort prevent switch rotation? > > )_( Dan > RV-7 N714D (fuselage/finish) > http://www.rvproject.com > > ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Re: Wiring headset jacks 2nd try
Date: Feb 04, 2003
Hello Bob, as usual, exactly what I need to confirm my doing! Appreciate very much your help! Kind regards Werner > Here's a wirebook I did for a 430/340 combo > in the AGATE Bonanza a few years ago. > > http://216.55.140.222/temp/gns430.pdf > > > Bob . . . > > ________________________________________________________________________________
Date: Feb 03, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: cycling voltmeter and ammeter
> > have about 16 hours on my RV-4 and have a question.=A0 My voltmeter and >ammeter cycle between 13-14.5 V on the voltmeter and between 5-10 amps every >1/2 second or so.=A0 The volt meter rapidly rises from 13 volts to 14.5 volts >and back almost like the voltage is rising, gets too high, cuts out, drops >below 13 volts, kicks back in, rises to 14.5 volts, cuts out......=A0 It just >rapidly cycles up and down.=A0 I have tried adjusting the voltage regulator >lower but does not seem to help the cycling..... > >I have a 35 amp Van's supplied alternator, a Van's supplied $35ish voltage >regulator, and an Aeroelectric overvoltage protection device.=A0 This issue >does not seem to cause any problems, but it does not seem right.=A0 > >Last night I turned on all my electrical accessories and it seemed to steady >out at about 13 V, but if I turn off just a couple of items, it goes right >back to cycling.=A0 I don't understand what is going on or if it is an issue, >but it just does not seem right. Does anyone have any ideas on what to check? This sounds like a classic voltage stability problem that can jump up when there is too much resistance in the wiring and components between a voltage regulator and where it ties to the bus. Just for grins, try making a temporary connection from the input of your regulator right to the b-lead of the alternator. Use a nice fat 18AWG or 16AWG wire. Disconnect the regulator's input lead that gets power from the bus and splice it to the test wire. Attach the other end of the wire to the alternator b-lead. Turn off ALL electronic gizmos. Start the engine and check the voltmeter. If the voltage looks okay, then try turning things on to vary the load while you watch the voltmeter. There's a good chance that the voltage will be steady. If this is true, then you need to "refurbish" all wiring/components between the bus and the regulator. This is a very common problem on some models of single engine Cessnas where there can be as many as 20 joints in the wiring between bus and regulator. As these age and increase in resistance, the system can become unstable in exactly the manner you have described. Bob . . . ________________________________________________________________________________
From: "Brian & Debi Shannon" <wings(at)theshannons.net>
Subject: DC-DC Converter or AC Inverter w/ Standby ADI????
Date: Feb 03, 2003
Hi Bob/All, I'm looking for a 2" standby ADI as a backup to a dual-EFIS panel for my Glasair with a 14V electric system. Unfortunately it's pretty hard to come by the 2" standby ADIs at all, much less in a 14v version! I've found a few 28V versions and a few 115vac, 400hz, 3 phase versions. So my question is: Would it be better to use a DC-DC converter for the 28v version or an inverter for the AC version. Would there be any problem using the DC-DC converter found here at http://www.majorpower.com/dctodc/majorvtc_120.html#MajorVTC120 (MajorVTC120-12-24)? How about the inverter found here at http://freespace.virgin.net/andy.wright617/inverter.htm ?? The DC-DC converter appears to be much lighter than most inverters at 2.5 lbs but is a bit "pricey" at $279 versus about $160 for an inverter. Are there any issues that would be necessary to consider besides price & weight? Thanks for any input! I'm sure there will be many others curious about this issue as the EFIS units become more economically feasible and people start looking for electric back-up attitude indicators! Regards, Brian --- ________________________________________________________________________________
Date: Feb 03, 2003
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Right Angle BNC
> > >> >>Gang, >> A few months ago somebody asked about crimp-on right angle female BNC >> connectors. Bob mentioned using a right angle adapter. Has anyone yet >> found a source for a decent crimp-on right angle? > > There are a number of sources . . . but none that > I know of that will install with the tool we sell. > AMP 225974-2 is a suitable part that sells for $22.00 > qty of 1. The hand tool that installs it is about $400.00 > > If it were my airplane, I'd install a cable male connector, > mate it with a right angle adapter and shrink a chunk > of double walled tubing over the interface to make it > permanent. . . . the po' boy's right angle connector. > > Bob . . > What about the Amphenol 31-334, available from Newark as PN 39F1443 for $28.92? It needs the Amphenol CTL-1 tool, which Mouser lists for about $50. Is this connector comptiable with the RCT-2 tool that B&C sells? I suddenly developed an interest in 90 deg coax connectors tonight, as I just discovered that my avionics installation leaves a bit less room for the RG-400 coax than I had hoped. So, I spent a little while flipping pages of an old Newark catalog and found: 90 deg BNC 50 ohm jack plug - part number 89F2919 - $18.11 - TYCO ELECTRONICS http://www.newark.com/NewarkWebCommerce/newark/en_US/support/catalog/productDetail.jsp?id=89F2919 90 deg BNC crimp on jack plug (UG-306)- part number 39F071 - $17.39 - AMPHENOL http://www.newark.com/NewarkWebCommerce/newark/en_US/support/catalog/productDetail.jsp?id=39F071 90 deg BNC crimp on jack plug (UG-306A)- part number 39F1071 - $12.62 - AMPHENOL http://www.newark.com/NewarkWebCommerce/newark/en_US/support/catalog/productDetail.jsp?id=39F1071 Questions - should there be enough performance difference between the crimp on connector vs the jack plug to make this a consideration? I've got to connect to COM, NAV, G/S and GPS antennae. I've searched the web, but I can't find what the difference is between a UG-306 and a UG-306A connector (other than about $5). Can anyone shed any light on this? Thanks, -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
Date: Feb 03, 2003
From: Jerzy Krasinski <krasinski(at)direcway.com>
Subject: Re: LEDs
Steve Sampson wrote: > >I am about to order some LEDs. Roughly how many mcd do I need for the >following: > >1. For a red flood for the cabin if all else fails so I can see in dim >light? >2. A white one to provide some light in the baggage compartement to >find something in the dark when the plane is parked? > >Thanks, Steve. > Steve, l000 mcd = 1cd is approximately as much light as from 1 regular candle. Jerzy > > > > ________________________________________________________________________________
From: "Tom Parks" <flightwork2(at)msn.com>
Subject: ABMM
Date: Feb 03, 2003
Bob! If I wire the switch per the terminal number sequence shown in Fig 11-11 of Aeroconnection, it works as advertised regarding closing the contactor in the bat and alt position. Figure 7 of the ABMM schematic shows a (2-10) switch terminals only. The (2-10) switch terminals shown in the notes section of Figure 7 indicates a S700 (2-10) switch, mounted keyway up. I'll use the terminal layout shown in Fig 11-11 for all (2-10) switches (obtained from B&C) for my aircraft wiring. regards, Tom Parks RV-7 N620CF ________________________________________________________________________________
Date: Feb 04, 2003
Subject: Grounding strobe shield on RV's?
From: czechsix(at)juno.com
Bob, I'm interested in getting the strobe wire shield grounding philosophy clarified....understand you recommend for composite aircraft to ground the shielding to the strobe head body, whereas on a metal aircraft to leave the shield at the strobe head end unconnected. Is that correct? Now, on the RV series, of course most of the wing is metal BUT the wingtip is fiberglass so the strobe body is not mounted directly on the metal airframe. So what do you recommend in this case? I think most guys with RV's leave the strobe head end of the shielding unconnected but a friend with an RV-8 using this scheme has some strobe noise coming through the headset. Have no idea if grounding the strobe ends of the shielding would make a difference hence the question (he has the power supply end grounded). Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D firewall forward stuff... ________________________________________________________________________________
From: "James Foerster" <jmfpublic(at)attbi.com>
Subject: Best Brand of 2.25 in Turn & Bank
Date: Feb 04, 2003
I dutifully read the List with search term of 'turn & bank'. After 99 postings, I still don't know what brand of Turn & Bank is best. Aircraft Spruce lists a 2.25in unit for $1187. It has a brushless motor, which should make it more reliable. Another 2.25 in unit is unlighted, and goes for $$810: presumably with a brush motor. The 3.2 in units run less at $662. Anyone know if the smaller units are less reliable? Or more reliable due to newer manufacture? I need to buy one soon, and old Bob convinced me that I'd rather had the T&B instead of the TC. My panel is tight, and the smaller unit would be preferable--and more expensive. Jim Foerster J400 ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Best Brand of 2.25 in Turn & Bank
Date: Feb 03, 2003
The backup unit that Lancair Avionics is putting in my panel is a Mid-Continent 2.25" unit, with a part number of 5550-8340-N5L. Hope that helps, not sure of price, as it is all bunched in with other flight instruments. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of James Foerster Subject: AeroElectric-List: Best Brand of 2.25 in Turn & Bank I dutifully read the List with search term of 'turn & bank'. After 99 postings, I still don't know what brand of Turn & Bank is best. Aircraft Spruce lists a 2.25in unit for $1187. It has a brushless motor, which should make it more reliable. Another 2.25 in unit is unlighted, and goes for $$810: presumably with a brush motor. The 3.2 in units run less at $662. Anyone know if the smaller units are less reliable? Or more reliable due to newer manufacture? I need to buy one soon, and old Bob convinced me that I'd rather had the T&B instead of the TC. My panel is tight, and the smaller unit would be preferable--and more expensive. Jim Foerster J400 ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: DC-DC Converter or AC Inverter w/ Standby ADI????
Date: Feb 03, 2003
If by ADI you mean a backup attitude instrument, I would suggest a refurbished 2" USAF JET Attitude Gyro unit, 501-1131-01. It is 14V, and under $2000 I believe. From the people I've talked to that have it, it performs flawlessly. If that's not what you meant by ADI, ignore. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Brian & Debi Shannon Subject: AeroElectric-List: DC-DC Converter or AC Inverter w/ Standby ADI???? Hi Bob/All, I'm looking for a 2" standby ADI as a backup to a dual-EFIS panel for my Glasair with a 14V electric system. Unfortunately it's pretty hard to come by the 2" standby ADIs at all, much less in a 14v version! I've found a few 28V versions and a few 115vac, 400hz, 3 phase versions. So my question is: Would it be better to use a DC-DC converter for the 28v version or an inverter for the AC version. Would there be any problem using the DC-DC converter found here at http://www.majorpower.com/dctodc/majorvtc_120.html#MajorVTC120 (MajorVTC120-12-24)? How about the inverter found here at http://freespace.virgin.net/andy.wright617/inverter.htm ?? The DC-DC converter appears to be much lighter than most inverters at 2.5 lbs but is a bit "pricey" at $279 versus about $160 for an inverter. Are there any issues that would be necessary to consider besides price & weight? Thanks for any input! I'm sure there will be many others curious about this issue as the EFIS units become more economically feasible and people start looking for electric back-up attitude indicators! Regards, Brian --- ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Feb 04, 2003
Subject: Re: Best Brand of 2.25 in Turn & Bank
In a message dated 2/4/03 4:35:54 AM Central Standard Time, jmfpublic(at)attbi.com writes: > old Bob convinced me > that I'd rather had the T&B instead of the TC. My panel is tight, and the > smaller unit would be preferable--and more expensive. > Good Morning Jim, Welcome to the ranks of believers! Unfortunately, my instrument guru tells me that none of the currently available crop of 2.25 rate instruments, TC or T&B, are much good. They both have comparably high failure rates. My first one lasted about 500 hours and the second one about two thousand hours. I could tell the first one was going bad by the sound it made. The second one sounded nice and quiet right up to the day it died. I intend to take it to my guru to see if we can determine the failure point, but haven't gotten around to doing so as yet. I decided to go back to the full size T&B because I think it helps force me to keep it in my normal scan. After Itzahk Jacoby was killed at Newark, I tried to analyze my technique and realized that I had not been checking the rate instrument as much as I thought I had. If you are not familiar with Itzahk's accident findings, it appears that both his HSI and his TC had failed. If it is a choice between a 2.25 TC or a 2.25 T&B, I would still opt for the T&B, but none of the smaller instruments seem to be as reliable as the ancient sized ones. If you must stick to the little bitty ones, listen to several, if you can, and pick the one that sounds the smoothest. Sure wish Jim Younkin was developing his stuff for certificated machines. It would be nice to be able to get something that was designed after World War One! Happy Skies, Old Bob ________________________________________________________________________________
From: "Shaun Simpkins" <shauns(at)hevanet.com>
Subject: Re: LEDs
Date: Feb 04, 2003
The illuminating power of a light source depends not only on the overall light output but on the solid angle over which it radiates its light. Since an LED is a diffuse light source, it's tricky to constrain the light pattern with an external reflector. There are so many LED fixtures now out on the market that I would go there first before rolling my own. I'd suggest checking into http://www.ledmuseumm.org one of the many LED enthusiast websites, for guidance, or http://www.theledlight.com for LED flashlights, replacement bulbs, fixtures, and raw LEDs. One builder I know was successful in replacing the lamp in the ACS Mini Eyeball Cockpit Light (11-07800) with a high-intensity red LED for use as a cockpit flood. Only works for planes with roofs. Another possibility is to use one of the many LED headlamp fixtures available for campers. These are usually 2-3 bulb affairs that run on tiny batteries but throw a lot of light for around $20. Some have switchable colors. Suitable gooseneck LED fixtures are available, as are LED "brick" fixtures, at automotive customization shops. Shaun > > > > >I am about to order some LEDs. Roughly how many mcd do I need for the > >following: > > > >1. For a red flood for the cabin if all else fails so I can see in dim > >light? > >2. A white one to provide some light in the baggage compartement to > >find something in the dark when the plane is parked? > > > >Thanks, Steve. > > ________________________________________________________________________________
Date: Feb 04, 2003
From: richard(at)riley.net
Subject: Re: DC-DC Converter or AC Inverter w/
Standby ADI???? Brian, I'm using a single panel Bluemountain EFIS, and bought a 115 v 400 hz 3 ph AI. I'm powering it with one of Andy Wright's inverters - haven't installed it yet, so I can't say anything good or bad, but it works nicely on the bench. Can I ask where you found the 28V, and how much they run? > > >Hi Bob/All, > > I'm looking for a 2" standby ADI as a backup to a dual-EFIS panel for my >Glasair with a 14V electric system. Unfortunately it's pretty hard to come >by the 2" standby ADIs at all, much less in a 14v version! I've found a few >28V versions and a few 115vac, 400hz, 3 phase versions. So my question is: >Would it be better to use a DC-DC converter for the 28v version or an >inverter for the AC version. Would there be any problem using the DC-DC >converter found here at >http://www.majorpower.com/dctodc/majorvtc_120.html#MajorVTC120 >(MajorVTC120-12-24)? How about the inverter found here at >http://freespace.virgin.net/andy.wright617/inverter.htm ?? The DC-DC >converter appears to be much lighter than most inverters at 2.5 lbs but is a >bit "pricey" at $279 versus about $160 for an inverter. Are there any >issues that would be necessary to consider besides price & weight? > >Thanks for any input! I'm sure there will be many others curious about this >issue as the EFIS units become more economically feasible and people start >looking for electric back-up attitude indicators! > >Regards, > Brian >--- > > ________________________________________________________________________________
Date: Feb 04, 2003
From: richard(at)riley.net
Subject: Re: Strobes
> >That was it Scott, any suggestions why I would want to >spend $50 more for 90W as opposed to 60W? If your strobe tubes will take the extra power (like, they aren't the Aeroflash wingtip strobes) the 90 w (45 w per side, if you're only running 2) is that much brighter. ________________________________________________________________________________
From: DHPHKH(at)aol.com
Date: Feb 04, 2003
Subject: Deltran On Board Charger
Gang, Ran across something interesting. Deltran has 21 oz automatic battery charger designed for on-board installation, with software tailored for RG batteries. If you have battery dependent ignitions, you could simply plug the airplane into an AC outlet anywhere, and always depart for the next flight with fully charged batteries. http://www.batterytender.com/catalog/product_info.php?cPath=35&products_id=46 Dan Horton ________________________________________________________________________________
From: "Wendell & Jean Durr" <legacy147(at)cableone.net>
Subject: Re: Switches and AC
Date: Feb 04, 2003
go to the list archives how does one do that? (Please forgive my ignorance) ________________________________________________________________________________
From: "Jon Finley" <jon(at)finleyweb.net>
Subject: OT: NAV Radio Squelch
Date: Feb 04, 2003
Hi all, This is a completely off topic question - I apologize. The nav volume on my NAV/COM (King KX-155) will not "disengage". Normally pulling the nav volume knob out turn it "on" and then you turn the knob to increase/decrease the volume. When my nav volume knob is "in" and set to minimum volume I can still hear the nav signal. Anyone know if this is a simple adjustment that I can make, something that a radio shop can fix, or worse??? Thanks! Jon Finley N90MG Q2 - Subaru EJ-22 DD - 440 Hrs. TT - 0 Hrs Engine Apple Valley, Minnesota http://www.FinleyWeb.net/default.asp?id=96 ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Deltran On Board Charger
> >Gang, > Ran across something interesting. Deltran has 21 oz automatic battery >charger designed for on-board installation, with software tailored for RG >batteries. If you have battery dependent ignitions, you could simply plug >the airplane into an AC outlet anywhere, and always depart for the next >flight with fully charged batteries. > >http://www.batterytender.com/catalog/product_info.php?cPath=35&products_id=46 If you store your airplane for extended periods of time (many months), some type of smart, float charger may be beneficial. RG battery self discharge rates are on the order of 2-3% per MONTH. Further, most folks who want the ultimate in battery performance will have a new battery every year. I'll suggest that time and expense to incorporate such a device in a modern airplane will have next to zero return on investment. My father-in-law has a small fork lift in his business that got parked for 90 days and the FLOODED battery ran down and destroyed itself. It was one of those long, skinny, odd-ball 3EE series batteries that cost about $200 each. He put a new battery in and the fork lift is up and running. Given that he is trying to spin this business down, the new battery is at risk of self-destruction too . . . I'm building a 13.0 volt float charger to clip onto the parked fork lift to keep this from happening again. Now, if I could only figure out a way to get an RG battery fitted to the machine . . . Bob . . . ________________________________________________________________________________
Date: Feb 04, 2003
Subject: Re: LEDs
From: "Larry Bowen" <Larry(at)BowenAero.com>
Huh? Roofs? -- Larry Bowen Larry(at)BowenAero.com http://BowenAero.com 2003: The Year of Flight! Shaun Simpkins said: > > [snip] > One builder I know was successful in replacing the lamp in the ACS Mini > Eyeball Cockpit Light > (11-07800) with a high-intensity red LED for use as a cockpit flood. > Only works for planes with > roofs. [snip] ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Grounding strobe shield on RV's?
> >Bob, > >I'm interested in getting the strobe wire shield grounding philosophy >clarified....understand you recommend for composite aircraft to ground >the shielding to the strobe head body, whereas on a metal aircraft to >leave the shield at the strobe head end unconnected. Is that correct? Yes. >Now, on the RV series, of course most of the wing is metal BUT the >wingtip is fiberglass so the strobe body is not mounted directly on the >metal airframe. So what do you recommend in this case? Ground the base of the strobe head to the shield . . . >I think most guys with RV's leave the strobe head end of the shielding >unconnected but a friend with an RV-8 using this scheme has some strobe >noise coming through the headset. Have no idea if grounding the strobe >ends of the shielding would make a difference hence the question (he has >the power supply end grounded). Depending on what conditions he is hearing the strobe noise, grounding the strobe head via shield on wiring may help. Need more details on kind of noise and conditions under which it happens. See chapter on noise . . . Bob . . . ________________________________________________________________________________
Date: Feb 04, 2003
From: "Mark A. Wood" <Mark.Wood(at)uvm.edu>
Subject: Re: LEDs
You need something above your head (a roof) to put the lamp on. > >Huh? Roofs? > >-- >Larry Bowen >Larry(at)BowenAero.com >http://BowenAero.com >2003: The Year of Flight! > >Shaun Simpkins said: >> >> >[snip] >> One builder I know was successful in replacing the lamp in the ACS Mini >> Eyeball Cockpit Light >> (11-07800) with a high-intensity red LED for use as a cockpit flood. >> Only works for planes with >> roofs. >[snip] > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: Switches and AC
Date: Feb 04, 2003
Hi Wendell, Try the following: Go to http://www.matronics.com/ the source of some great products and all the various lists. go to the bottom of the page and click on http://www.matronics.com/ and follow instructions. Go to http://www.matronics.com/searching/search.html and enter various words and word combinations and see what you find. Sometimes it takes a bit of patience to get the info you want. Other times, depending on subject, no amount of trying will seem to work. Jim in Kelowna ----- Original Message ----- From: "Wendell & Jean Durr" <legacy147(at)cableone.net> Subject: Re: AeroElectric-List: Switches and AC > > go to the list archives > > how does one do that? (Please forgive my ignorance) > > ________________________________________________________________________________
Date: Feb 04, 2003
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: BNA seminar
Bob, I got very positive reviews as expected from the Tennessee Valley RV Builders Group members who attended the Nashville seminar this past weekend. I hope the TVRVBG bunch didn't embarrass the rest of the class what with their drooling and other unsociable behavior. ;-) Any members of this list who have an opportunity to attend one of 'Lectric Bob's seminars really need to consider enrollment. He may be too modest to say so, but it will be some of the most valuable time and dollars you can spend while educating yourself about the wiring architecture on our custom-built planes. Sam Buchanan (RV-6) "The RV Journal" http://thervjournal.com ________________________________________________________________________________
Date: Feb 04, 2003
From: "Mark A. Wood" <Mark.Wood(at)uvm.edu>
Subject: inexpensive low output alternator
Bob I am building a light VFR aircraft (Zenith 601) and I am looking for an inexpensive low output alternator to connect to my Continental O-200. I have heard people talk about the alternator from a John Deer lawn tractor and was looking for any input on using this. I have used the drive gear from an old generator which I cut down and I plan to put a pulley on the shaft to drive the alternator. 1 Is using this alternator a reasonable way to go? (in your opinion or feedback from anyone on the list is welcome.) 2. This is a permanent magnet type alternator, do you know how the voltage is regulated, and do I need an external regulator? 3. Do you know what RPM range the alternator would need to turn? I can adjust this by the ratio of the pulleys. Thanks Mark Wood ________________________________________________________________________________
From: "Wendell & Jean Durr" <legacy147(at)cableone.net>
Subject: Re: Switches and AC
Date: Feb 04, 2003
Thanx. My learning curve is almost vertical ________________________________________________________________________________
From: "Francis, David CMDR" <David.Francis(at)defence.gov.au>
Subject: SEC: UNCLASSIFIED - BUS INSTABILITY
Date: Feb 05, 2003
Bob, is this another example of system instability that just needs a cleanup of bus to voltage regulator, or is it more: Aircraft is an elderly Pawnee, amps are stable at all times. There are two voltage cycles, one imposed on the other. Normally the voltage needle oscillates over 0.5 volt about 3-5 times per second. If I turn on the strobe, the voltage drops 1.5 volts in time with firing of the strobe, additonal to the underlying 0.5 cycle. The radios are noisy all the time. Should this be fixed, if so how? Regards, David Francis Email: David.Francis(at)defence.gov.au ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: SEC: UNCLASSIFIED - BUS INSTABILITY
Date: Feb 04, 2003
Do you have the Cessna Flashing Beacon? Our Skyhawk did the same thing until we reversed the connections for the large resistor and the light. Cy Galley - Bellanca Champion Club Newsletter Editor & EAA TC www.bellanca-championclub.com We support Aeroncas ----- Original Message ----- From: "Francis, David CMDR" <David.Francis(at)defence.gov.au> Subject: AeroElectric-List: SEC: UNCLASSIFIED - BUS INSTABILITY > > > Bob, is this another example of system instability that just needs a cleanup > of bus to voltage regulator, or is it more: > > Aircraft is an elderly Pawnee, amps are stable at all times. There are two > voltage cycles, one imposed on the other. > > Normally the voltage needle oscillates over 0.5 volt about 3-5 times per > second. If I turn on the strobe, the voltage drops 1.5 volts in time with > firing of the strobe, additonal to the underlying 0.5 cycle. The radios are > noisy all the time. Should this be fixed, if so how? > > Regards, David Francis > > Email: David.Francis(at)defence.gov.au > > ________________________________________________________________________________
Date: Feb 04, 2003
From: DHPHKH(at)aol.com
Subject: Re: Deltran On Board Charger
Bob writes: <> You may be right, but it's still fun to explore the "why". Subject is an RV8A with dual Lightspeeds. I've declined to install an APU plug, as it seems kinda dumb to help crank and launch a battery dependent airplane with low batteries. At 21 oz and less than $100, the charger doesn't weigh much more than an APU plug, or cost much more either. You always have it with you. You know it has the right charge cycle and rates, unlike the relic in the back of the hanger. The little green light tells you when you've reached full charge, and it won't overcharge. It would allow recharging without removing the rear of the RV baggage compartment. Return on investment? Fail an alternator on the outbound trip, and after a full recharge you could fly your battery ignition airplane some reasonable distance back to home base. I'll bet you would save more than $100 compared to repairs in a foreign port No, I haven't thought it all through yet, but it is an interesting idea. Dan ________________________________________________________________________________
Date: Feb 04, 2003
aeroelectric-list(at)matronics.com
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Wiring harness heads up
I've just had a bad wiring harness experience that I want to share with you, as it highlights a potential safety problem. I bought my avionics from a popular avionics vendor, and I had him make up the wiring harness. Well, this wiring harness has been a nightmare. Two pins were swapped on the transponder, which meant the transponder and altitude encode wouldn't talk to each other. I swapped the pins and everything is OK there now. On the intercom, the PTT and mic wires were swapped between the Com 1 and Com 2 spots. If I had selected Com 1 to transmit, I would have been transmitting on Com 2, but listening on Com 1. OK, I can fix that. I found it on the bench when I decided to check every wire with an ohmmeter. It would have been a royal PITA to find and fix if I hadn't found the problem until I was doing post-installation functional checks. Well tonight I found the problem that has stopped me in my tracks. The Com 1 power line is supposed to get a 10a fuse, but the wire is only 20 AWG. It needs to be 18 AWG if it is going to get a 10a fuse. If I had simply followed the notes the vendor sent me, and I ever had a short, I could have a smoking wire before the fuse blew. If I use a 7a fuse to match the wire I could be looking at nuisance fuse blowing. So, please pay close attention to the details of any vendor supplied wiring harness. Don't simply assume that it must be OK just because it comes from a reputable vendor. -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
From: Benford2(at)aol.com
Date: Feb 04, 2003
Subject: Re: Wiring harness heads up
In a message dated 2/4/2003 7:37:58 PM Mountain Standard Time, khorto1537(at)rogers.com writes: > > I've just had a bad wiring harness experience that I want to share > with you, as it highlights a potential safety problem. > > I bought my avionics from a popular avionics vendor, and I had him > make up the wiring harness. Well, this wiring harness has been a > nightmare. Two pins were swapped on the transponder, which meant the > transponder and altitude encode wouldn't talk to each other. I > swapped the pins and everything is OK there now. On the intercom, > the PTT and mic wires were swapped between the Com 1 and Com 2 spots. > If I had selected Com 1 to transmit, I would have been transmitting > on Com 2, but listening on Com 1. OK, I can fix that. I found it on > the bench when I decided to check every wire with an ohmmeter. It > would have been a royal PITA to find and fix if I hadn't found the > problem until I was doing post-installation functional checks. > > Well tonight I found the problem that has stopped me in my tracks. > The Com 1 power line is supposed to get a 10a fuse, but the wire is > only 20 AWG. It needs to be 18 AWG if it is going to get a 10a fuse. > If I had simply followed the notes the vendor sent me, and I ever had > a short, I could have a smoking wire before the fuse blew. If I use > a 7a fuse to match the wire I could be looking at nuisance fuse > blowing. > > So, please pay close attention to the details of any vendor supplied > wiring harness. Don't simply assume that it must be OK just because > it comes from a reputable vendor. > -- > Kevin Horton RV-8 (finishing kit) > Ottawa, Canada > http://go.phpwebhosting.com/~khorton/rv8/ > Do tell all of us the name of this vendor so we can steer real clear of them. I just finished my panel and it was ALOT of work. I am sure everything is connected correctly. You were smart by checking your harness while it was still on the bench. You can probably run another 18 ga wire on the outside of your bundle and disable the smaller wire. I would bet a 7 amp fuse will work without blowing out though. ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: switch keyway question
> > >I have several toggle switches that came without anti-rotation washers. >Does anyone know where the washers can be purchased seperately? > >Vince Welch >N327W Send me your address and how many you need . . . I'll mail them to you. Bob . . . ________________________________________________________________________________
Date: Feb 04, 2003
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Wiring harness heads up
> >In a message dated 2/4/2003 7:37:58 PM Mountain Standard Time, >khorto1537(at)rogers.com writes: > > >Do tell all of us the name of this vendor so we can steer real clear of them. >I just finished my panel and it was ALOT of work. I am sure everything is >connected correctly. You were smart by checking your harness while it was >still on the bench. You can probably run another 18 ga wire on the outside of >your bundle and disable the smaller wire. I would bet a 7 amp fuse will work >without blowing out though. > I'd rather not name names. This vendor has lots of satisfied customers, and I have never heard anyone else complain about a problem. Any vendor can screw up a wiring harness. So no matter who you buy from you should give the harness a good check out on the bench. That was really the point of my message, rather than to skewer a vendor whose employee had a bad day. Kevin ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Deltran On Board Charger
> >Bob writes: ><modern airplane will have next to zero return on investment.>> > > You may be right, but it's still fun to explore the "why". > > Subject is an RV8A with dual Lightspeeds. I've declined to install an > APU plug, as it seems kinda dumb to help crank and launch a battery > dependent airplane with low batteries. > > At 21 oz and less than $100, the charger doesn't weigh much more than > an APU plug, or cost much more either. You always have it with you. You > know it has the right charge cycle and rates, unlike the relic in the > back of the hanger. The little green light tells you when you've reached > full charge, and it won't overcharge. It would allow recharging without > removing the rear of the RV baggage compartment. > > Return on investment? Fail an alternator on the outbound trip, and > after a full recharge you could fly your battery ignition airplane some > reasonable distance back to home base. I'll bet you would save more than > $100 compared to repairs in a foreign port > > No, I haven't thought it all through yet, but it is an interesting idea. If you were flying a Ford gear driven alternator on a C-172 fitted with a flooded battery that was 3-4 years old, then I would agree, you need everything going for you that you can get. That same $100 will by two years worth of batteries for a yearly change-out cycle that would (if the airplane is flown every two months or so) guarantee a level of reliability that all the chargers in the world cannot bestow on a Cessna. Bob . . . ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Gotta pack up again . . .
RAC is sending me out to Whippany, NJ for the rest of the week. See you all Saturday morning. . . Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: inexpensive low output alternator
> >Bob >I am building a light VFR aircraft (Zenith 601) and I am looking for >an inexpensive low output alternator to connect to my Continental >O-200. I have heard people talk about the alternator from a John Deer >lawn tractor and was looking for any input on using this. > >I have used the drive gear from an old generator which I cut down and >I plan to put a pulley on the shaft to drive the alternator. > >1 Is using this alternator a reasonable way to go? (in your opinion >or feedback from anyone on the list is welcome.) > >2. This is a permanent magnet type alternator, do you know how the >voltage is regulated, and do I need an external regulator? > >3. Do you know what RPM range the alternator would need to turn? I >can adjust this by the ratio of the pulleys. If you're proposing a belt-drive adapter, then the Nipon-Denso 40A machine would be my choice (B&C L-40). Unless you are experienced at modifying modern alternator to accept external regulators, consider using the built in regulator with external OV protection as shown in http://www.aeroelectric.com/articles/crowbar.pdf Bob . . . ________________________________________________________________________________
Date: Feb 04, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Wiring harness heads up
> >I've just had a bad wiring harness experience that I want to share >with you, as it highlights a potential safety problem. > >I bought my avionics from a popular avionics vendor, and I had him >make up the wiring harness. Well, this wiring harness has been a >nightmare. Two pins were swapped on the transponder, which meant the >transponder and altitude encode wouldn't talk to each other. I >swapped the pins and everything is OK there now. On the intercom, >the PTT and mic wires were swapped between the Com 1 and Com 2 spots. >If I had selected Com 1 to transmit, I would have been transmitting >on Com 2, but listening on Com 1. OK, I can fix that. I found it on >the bench when I decided to check every wire with an ohmmeter. It >would have been a royal PITA to find and fix if I hadn't found the >problem until I was doing post-installation functional checks. > >Well tonight I found the problem that has stopped me in my tracks. >The Com 1 power line is supposed to get a 10a fuse, but the wire is >only 20 AWG. It needs to be 18 AWG if it is going to get a 10a fuse. >If I had simply followed the notes the vendor sent me, and I ever had >a short, I could have a smoking wire before the fuse blew. If I use >a 7a fuse to match the wire I could be looking at nuisance fuse >blowing. An 20AWG wire would rise 10 degrees C at 7A continuous . . which never happens in a transceiver. The 10A protection recommended is a bit hefty, a 7A fuse (80+ watts into the radio during transmit) would probably be fine too. There was no danger imposed by running a 10A fuse in this case, it just means that the wire gets a bit hotter before the fuse opens but in no way represents a threat to the wire bundle. >So, please pay close attention to the details of any vendor supplied >wiring harness. Don't simply assume that it must be OK just because >it comes from a reputable vendor. Sounds like a case of multiple dyslexic pin insertions. Pretty easy to do. Disappointing tho that they didn't do their own pin-to-pin ringout of the harness. Bob . . . ________________________________________________________________________________
From: "James Foerster" <jmfpublic(at)attbi.com>
Subject: Best LED color for preserving night vision
Date: Feb 05, 2003
I'm designing a ceiling mounted headphone jack with integral LEDs for cabin light. It will have both a white LED and another color. Initially, I was thinking I would use red, but I vaguely recall that the military has determined that another color, perhaps green, was better as long as this was kept at a low level. A brief Google search found at least one reference confirming this vague notion. http://www.corvus.com/kniffen.htm is an astronomy reference. I intend to have the LEDs on Bob's dimmer, fed through a 4 volt Zener and series resistor, as was mentioned recently on this list. Each LED will have a double throw switch, for full brightness, or for dimmer level power. The green LED is wired for full voltage as well as dimmer power for those times when the master is off, and the plane is parked, needing some amount of cabin light. I will make up a pc board with the connector for the wire harness. I can find pc mount 1/4 in jacks, but not the slightly smaller microphone jack. I have not decided whether to use DB9 or DB15 connectors, or just use FASTON tabs on the pc board. Anyone have any thoughts on color choice? Jim Foerster ________________________________________________________________________________
Date: Feb 05, 2003
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Re: Wiring harness heads up
> > >> >>I've just had a bad wiring harness experience that I want to share >>with you, as it highlights a potential safety problem. >> >>I bought my avionics from a popular avionics vendor, and I had him >>make up the wiring harness. Well, this wiring harness has been a >>nightmare. Two pins were swapped on the transponder, which meant the >>transponder and altitude encode wouldn't talk to each other. I >>swapped the pins and everything is OK there now. On the intercom, >>the PTT and mic wires were swapped between the Com 1 and Com 2 spots. >>If I had selected Com 1 to transmit, I would have been transmitting >>on Com 2, but listening on Com 1. OK, I can fix that. I found it on >>the bench when I decided to check every wire with an ohmmeter. It >>would have been a royal PITA to find and fix if I hadn't found the >>problem until I was doing post-installation functional checks. >> >>Well tonight I found the problem that has stopped me in my tracks. >>The Com 1 power line is supposed to get a 10a fuse, but the wire is >>only 20 AWG. It needs to be 18 AWG if it is going to get a 10a fuse. >>If I had simply followed the notes the vendor sent me, and I ever had >>a short, I could have a smoking wire before the fuse blew. If I use >>a 7a fuse to match the wire I could be looking at nuisance fuse >>blowing. > > An 20AWG wire would rise 10 degrees C at 7A continuous . . > which never happens in a transceiver. The 10A protection > recommended is a bit hefty, a 7A fuse (80+ watts into the radio > during transmit) would probably be fine too. There was no > danger imposed by running a 10A fuse in this case, it just > means that the wire gets a bit hotter before the fuse opens > but in no way represents a threat to the wire bundle. > I appreciate your input Bob. This is a GNS-430, and that "Com" power wire seems to do more than just power the com transceiver. I didn't hook it up when I first tried to check the unit out on the bench, as I didn't have a com antenna, and the complete display remained blank. Once I hooked the "Com" power line up I was able to bring the whole unit to life. It drew about 3a just sitting there doing nothing. Garmin recommends a 10a fuse. I'm hesitant to drop down to a 7a fuse, as I certainly don't want to set myself up for a nuisance trip issue. I'm also hesitant to bust the wire size recommendations in AC43.13-1B - I studied them last night and I can't see a way to justify a 10a fuse, unless I run this power line outside the bundle, all by itself. I'll probably get a local avionics shop to replace the 20 AWG wire with 18 AWG. Kevin ________________________________________________________________________________
Date: Feb 05, 2003
From: Ed Holyoke <bicyclop(at)pacbell.net>
Subject: Best LED color for preserving night vision
> I'm designing a ceiling mounted headphone jack with integral LEDs for > cabin > light. It will have both a white LED and another color. Initially, I was > thinking I would use red, but I vaguely recall that the military has > determined that another color, perhaps green, was better as long as this > was > kept at a low level. A brief Google search found at least one reference > confirming this vague notion. http://www.corvus.com/kniffen.htm is an > astronomy reference. > > Anyone have any thoughts on color choice? > > Jim Foerster I think that the military prefers green for use with night vision goggles. See: http://www.seitzinc.com/cat_1.htm http://www.seitzinc.com/cat_2.htm I'm not sure which color would be better for reading charts. My guess is red. Good luck, Ed Holyoke ________________________________________________________________________________
From: Benford2(at)aol.com
Date: Feb 05, 2003
Subject: Re: Wiring harness heads up
In a message dated 2/5/2003 5:16:34 AM Mountain Standard Time, khorto1537(at)rogers.com writes: > > I appreciate your input Bob. This is a GNS-430, and that "Com" power > wire seems to do more than just power the com transceiver. I didn't > hook it up when I first tried to check the unit out on the bench, as > I didn't have a com antenna, and the complete display remained blank. > Once I hooked the "Com" power line up I was able to bring the whole > unit to life. It drew about 3a just sitting there doing nothing. > > Garmin recommends a 10a fuse. I'm hesitant to drop down to a 7a > fuse, as I certainly don't want to set myself up for a nuisance trip > issue. I'm also hesitant to bust the wire size recommendations in > AC43.13-1B - I studied them last night and I can't see a way to > justify a 10a fuse, unless I run this power line outside the bundle, > all by itself. I'll probably get a local avionics shop to replace > the 20 AWG wire with 18 AWG. > > Kevin > > > If you have a 430 then you spent a fair amount of money at that unnamed avionics shop. I am curious ?????? Why not just have them fix this big mess you have on your bench? Ben Haas. N801BH. ________________________________________________________________________________
From: "Rob Housman" <RobH@hyperion-ef.com>
Subject: Best LED color for preserving night vision
Date: Feb 05, 2003
It is almost impossible to see everything on a chart (especially all that stuff printed in the FAA's favorite color: magenta) when using a red light. Green, however, makes it easy to read the charts. Best regards, Rob Housman Europa XS Tri-Gear A070 Airfarame complete Irvine, CA -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Ed Holyoke Subject: RE: AeroElectric-List: Best LED color for preserving night vision > I'm designing a ceiling mounted headphone jack with integral LEDs for > cabin > light. It will have both a white LED and another color. Initially, I was > thinking I would use red, but I vaguely recall that the military has > determined that another color, perhaps green, was better as long as this > was > kept at a low level. A brief Google search found at least one reference > confirming this vague notion. http://www.corvus.com/kniffen.htm is an > astronomy reference. > > Anyone have any thoughts on color choice? > > Jim Foerster I think that the military prefers green for use with night vision goggles. See: http://www.seitzinc.com/cat_1.htm http://www.seitzinc.com/cat_2.htm I'm not sure which color would be better for reading charts. My guess is red. Good luck, Ed Holyoke ________________________________________________________________________________
Date: Feb 05, 2003
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: Wiring harness heads up
Kevin; I am sure you have checked the wiring schematic carefully but may I suggest you look for a duplicated or two line power feed ? Some avionics (the King KY-97 comm, for one) use two wire power feeds to spread the power going into the unit over two connector pins for reasons of conductor sizing, etc. The two leads go back to a single breaker in my case but could go to individual ones to ensure both wires are protected by a suitably sized breaker. (As Bob says often enough, the breaker protects the wire not the radio, etc.) Just a thought. If its a single wire feed, you may be looking at going to a larger gauge wire as you say. Jim Oke Wpg., MB ----- Original Message ----- From: "Kevin Horton" <khorto1537(at)rogers.com> Subject: Re: AeroElectric-List: Wiring harness heads up > > > > > > >> > >>I've just had a bad wiring harness experience that I want to share > >>with you, as it highlights a potential safety problem. > >> > >>I bought my avionics from a popular avionics vendor, and I had him > >>make up the wiring harness. Well, this wiring harness has been a > >>nightmare. Two pins were swapped on the transponder, which meant the > >>transponder and altitude encode wouldn't talk to each other. I > >>swapped the pins and everything is OK there now. On the intercom, > >>the PTT and mic wires were swapped between the Com 1 and Com 2 spots. > >>If I had selected Com 1 to transmit, I would have been transmitting > >>on Com 2, but listening on Com 1. OK, I can fix that. I found it on > >>the bench when I decided to check every wire with an ohmmeter. It > >>would have been a royal PITA to find and fix if I hadn't found the > >>problem until I was doing post-installation functional checks. > >> > >>Well tonight I found the problem that has stopped me in my tracks. > >>The Com 1 power line is supposed to get a 10a fuse, but the wire is > >>only 20 AWG. It needs to be 18 AWG if it is going to get a 10a fuse. > >>If I had simply followed the notes the vendor sent me, and I ever had > >>a short, I could have a smoking wire before the fuse blew. If I use > >>a 7a fuse to match the wire I could be looking at nuisance fuse > >>blowing. > > > > An 20AWG wire would rise 10 degrees C at 7A continuous . . > > which never happens in a transceiver. The 10A protection > > recommended is a bit hefty, a 7A fuse (80+ watts into the radio > > during transmit) would probably be fine too. There was no > > danger imposed by running a 10A fuse in this case, it just > > means that the wire gets a bit hotter before the fuse opens > > but in no way represents a threat to the wire bundle. > > > > I appreciate your input Bob. This is a GNS-430, and that "Com" power > wire seems to do more than just power the com transceiver. I didn't > hook it up when I first tried to check the unit out on the bench, as > I didn't have a com antenna, and the complete display remained blank. > Once I hooked the "Com" power line up I was able to bring the whole > unit to life. It drew about 3a just sitting there doing nothing. > > Garmin recommends a 10a fuse. I'm hesitant to drop down to a 7a > fuse, as I certainly don't want to set myself up for a nuisance trip > issue. I'm also hesitant to bust the wire size recommendations in > AC43.13-1B - I studied them last night and I can't see a way to > justify a 10a fuse, unless I run this power line outside the bundle, > all by itself. I'll probably get a local avionics shop to replace > the 20 AWG wire with 18 AWG. > > Kevin > > ________________________________________________________________________________
From: KahnSG(at)aol.com
Date: Feb 05, 2003
Subject: solid state gyro & avionics master relay
Has anyone seen the solid state gyro from Crossbow? Here is a link to them. http://www.xbow.com/General_info/gyro_guide.htm Does anyone know anything about Tiger Avionics? I installed one of their avionics master relays in my plane about 16 years ago. I would like to have some documentation on it. I'm considering taking it out and/or installing an E-buss now. I believe they were located in Phoenix. Steve ________________________________________________________________________________
Date: Feb 05, 2003
Subject: Re: Grounding strobe shield on RV's?
From: czechsix(at)juno.com
Hmmm...interesting...a quick survey of the RV List shows pretty much everybody is grounding the shield only at the power supply end. Funny thing is that some folks get no noise at all, and others have problems. But the fact that there are some who do NOT have noise even with the shields connected only at the power supply end implies that the connection at the strobe head is not critical for the RV series, and there's something else happening to cause the noise that some people are experiencing. Given the variety of routing and wiring techniques used in each individual aircraft it may be difficult to trace the source of strobe noise... --Mark Navratil Cedar Rapids, Iowa RV-8A N2D firewall forward... From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: Grounding strobe shield on RV's? > >Bob, > >I'm interested in getting the strobe wire shield grounding philosophy >clarified....understand you recommend for composite aircraft to ground >the shielding to the strobe head body, whereas on a metal aircraft to >leave the shield at the strobe head end unconnected. Is that correct? Yes. >Now, on the RV series, of course most of the wing is metal BUT the >wingtip is fiberglass so the strobe body is not mounted directly on the >metal airframe. So what do you recommend in this case? Ground the base of the strobe head to the shield . . . >I think most guys with RV's leave the strobe head end of the shielding >unconnected but a friend with an RV-8 using this scheme has some strobe >noise coming through the headset. Have no idea if grounding the strobe >ends of the shielding would make a difference hence the question (he has >the power supply end grounded). Depending on what conditions he is hearing the strobe noise, grounding the strobe head via shield on wiring may help. Need more details on kind of noise and conditions under which it happens. See chapter on noise . . . Bob . . . ________________________________________________________________________________
Date: Feb 05, 2003
Subject: Re: Best LED color for preserving night vision
From: James Freeman <flyeyes(at)bellsouth.net>
On Wednesday, February 5, 2003, at 03:24 AM, James Foerster wrote: > Anyone have any thoughts on color choice? > > Jim Foerster > > HI Jim. You'd think this choice would be fairly obvious, but then you' d wrong.... ;-) I have looked into this a few times and found conflicting recommendations. Older literature (and the AIM, last time I looked this up there) suggest red, and one reason for the sometimes odd color choices on FAA charts is to make everything at least legible under red light. It turns out that, although theoretically sound, the color of light probably doesn't have any significant impact on the eye's dark adaptation. A (minor) disadvantage of red light or gauges is that as we age, it is harder to see red objects up close. This is because red light is a longer wavelength, and is therefore refracted less strongly than shorter wavelengths. If you have a need reading glasses and have a high quality inkjet, try printing some words in the smallest font possible in red and then adjacent in blue or green. You'll notice that the green/blue objects can be a little closer and still be sharp. Blues/greens (shorter wavelengths) will scatter more easily and cause more glare if you have any opacity or irregularity in your eyes or correction (e.g. cataracts, astigmatism, dirty lenses, etc.) The dark adapted eye has its peak sensitivity at a blue-green wavelength (one of the reasons we are all slightly more nearsighted at night than during the day) AFAIK current military fashion is blue-green, but this is for compatibility with the current technology night vision goggles. The most important consideration, really, is what you like. I have owned cars with blue/green electroluminescent gauges and didn't particularly like them, although they were very easy to read. I currently have a car with white dash lights, and one with reddish-orange lights. Both are perfectly functional, but I like the reddish-orange much better. Bottom line is, pick what you like, make sure it's pointed at what you want to be able to read, and make sure the dimmer is effective.... JFF ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: solid state gyro & avionics master relay
Date: Feb 04, 2003
The crossbow unit, the 500, is what is supplied with the Chelton/Sierra EFIS. Despite a few early troubles, I have heard great things about their latest version. When properly calibrated, accordingly to all the test pilots at Lancair, it hangs right in there with the laser ring gyro control unit. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of KahnSG(at)aol.com Subject: AeroElectric-List: solid state gyro & avionics master relay Has anyone seen the solid state gyro from Crossbow? Here is a link to them. http://www.xbow.com/General_info/gyro_guide.htm Does anyone know anything about Tiger Avionics? I installed one of their avionics master relays in my plane about 16 years ago. I would like to have some documentation on it. I'm considering taking it out and/or installing an E-buss now. I believe they were located in Phoenix. Steve ________________________________________________________________________________
Date: Feb 05, 2003
From: John Mireley <mireley(at)pilot.msu.edu>
Subject: Re: solid state gyro & avionics master relay
Shannon Knoepflein wrote: > >The crossbow unit, the 500, is what is supplied with the Chelton/Sierra >EFIS. Despite a few early troubles, I have heard great things about >their latest version. When properly calibrated, accordingly to all the >test pilots at Lancair, it hangs right in there with the laser ring gyro >control unit. > > > And costs $7,000 without a display. You can get software to drive your PDA with it.. John Mireley ________________________________________________________________________________
From: owner-aeroelectric-list-server(at)matronics.com
Subject: EXPBUS
Date: Feb 05, 2003
Hi all. I'll soon start on the electric system for my Europa. I'm considering the EXPBUS from Control Vision to be the "heart" of my system. One of the local veterans in the field adviced against it however (he has no personal experience with the EXPBUS though). He said that it looked vulnerable - and, if something would go wrong with it, it would take a lot of work to trouble-shoot - and most likely have it sent across the pond for repairs.... With of course a longtime grounding of the A/C as a result. Still, I'm leaning towards the EXPBUS - as it must be the simplest and most well arranged system for the homebuilder. So - to all who has been there, done that: what's your experience/advice?? Hans ________________________________________________________________________________
From: John Loram <johnl(at)loram.org>
Subject: solid state gyro & avionics master relay
Date: Feb 05, 2003
Crossbow is quoting single unit quantities of the AHRS500 at $12,000, and the less precise AHRS4000 at $7,000. They are working on less spendy two axis units (without the magnetometer) for around $2000. Whether they'll ever see the light of day, remains to be determined. They are aware of the GA/Experimental market and are interested. -john- john(at)loram.org www.loram.org -----Original Message----- From: John Mireley [mailto:mireley(at)pilot.msu.edu] Subject: Re: AeroElectric-List: solid state gyro & avionics master relay Shannon Knoepflein wrote: > >The crossbow unit, the 500, is what is supplied with the Chelton/Sierra >EFIS. Despite a few early troubles, I have heard great things about >their latest version. When properly calibrated, accordingly to all the >test pilots at Lancair, it hangs right in there with the laser ring gyro >control unit. > > > And costs $7,000 without a display. You can get software to drive your PDA with it.. John Mireley ________________________________________________________________________________
From: BillRVSIX(at)aol.com
Date: Feb 05, 2003
Subject: Facet Electric fuel pump ?
Hello dose any have any idea how many amps the Facet fuel pump from vans draws. Working on bus load analysis and need to figure out circuit breaker size. Thanks Bill Higgins Pembroke Ma. ________________________________________________________________________________
Date: Feb 05, 2003
aeroelectric-list(at)matronics.com
From: Kevin Horton <khorto1537(at)rogers.com>
Subject: Wiring harness follow up
I reported yesterday about some problems I had with the vendor supplied wiring harnesses that I purchased with my avionics. There were several pairs of wires that were on the wrong pins, and one power line was only 20 AWG even though it was supposed to get a 10a fuse. I received many e-mails, on and off the lists, so please understand if I don't respond to each one individually. Today I called the vendor to talk to him. He was very cooperative and easy to deal with. He said that his employees are supposed to "ohm out" each harness, but that something obviously went wrong with my harness. He offered to take the harness back, personally fix all the problems, and to give it a complete inspection - no charge. Power line - I originally was concerned that I could be looking at a possible smoke event if the 20 AWG power line ever shorted. However, Bob Nuckolls responded that although a 10a fuse was a bit much for a 20 AWG wire, and the wire would get hotter than desired if it ever shorted, it should not lead to a smoke event. I discussed this issue with the vendor. He explained that the Garmin specified 18 AWG wire requires an extra long pin to make room for a larger crimp area. In his opinion, this long pin has a real risk of later shorting out against other wires in the connector. He discussed the issue with his local FAA folks, and convinced them to allow him to use 20 AWG wire. Note - this power line "Y's" to go to two pins, so it should be possible to use 20 AWG wire from the pins to the Y, and 18 AWG wire the rest of the way. I didn't think to bring this up with the vendor while I had him on the phone, but I requested he do this in the letter I sent with the harnesses. Many people wanted me to name the vendor, as they seemed to want to stay away from him. That was not the point of my messages. Even with the issues I had with my wiring harness I am still glad I chose the vendor I did. Any vendor can make a mistake. The important thing is how they deal with the mistake. My story was intended to advise that wiring harnesses should be completely checked out on the bench before installing them in the aircraft. Several of my problems would not have been noticed until I was doing the functional checks after installation, and it would have been very difficult to find and correct the problems with harness embedded in the aircraft. Don't just assume that any vendor supplied part is good without inspecting it. -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ ________________________________________________________________________________
From: Benford2(at)aol.com
Date: Feb 06, 2003
Subject: Fuel Pump
If I remember correctly the Facet pump needs 1.2 Amps. ________________________________________________________________________________
From: John Loram <johnl(at)loram.org>
Subject: Facet Electric fuel pump ?
Date: Feb 05, 2003
The A/C Spruce catalog says 1amp max. But I don't know if that's peak or RMS. I'd call Facet. regards, -john- john(at)loram.org www.loram.org -----Original Message----- From: BillRVSIX(at)aol.com [mailto:BillRVSIX(at)aol.com] Subject: AeroElectric-List: Facet Electric fuel pump ? Hello dose any have any idea how many amps the Facet fuel pump from vans draws. Working on bus load analysis and need to figure out circuit breaker size. Thanks Bill Higgins Pembroke Ma. ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Re: Facet Electric fuel pump ?
Date: Feb 06, 2003
Bill, I have a Facet , the inrush current on switch-on is 1.2 Amps, it stabilises on 0.9 Amps during continouse run (wet), this on the Batterie only, so with 13.8 it might draw 10% more (if I remember Bobs advice correctly). I do not know, what your pumps type is, mine is a Facet 40108. Hope it helpes Werner ----- Original Message ----- From: "John Loram" <johnl(at)loram.org> Subject: RE: AeroElectric-List: Facet Electric fuel pump ? > > The A/C Spruce catalog says 1amp max. But I don't know if that's peak or > RMS. I'd call Facet. > > regards, -john- > > john(at)loram.org > www.loram.org > > -----Original Message----- > From: BillRVSIX(at)aol.com [mailto:BillRVSIX(at)aol.com] > To: rv-list(at)matronics.com; aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: Facet Electric fuel pump ? > > > Hello dose any have any idea how many amps the Facet fuel pump from vans > draws. Working on bus load analysis and need to figure out circuit breaker > size. Thanks > > Bill Higgins > Pembroke Ma. > > ________________________________________________________________________________
From: "Shannon Knoepflein" <kycshann(at)kyol.net>
Subject: Facet Electric fuel pump ?
Date: Feb 05, 2003
If it's the same little 14V facet pump I'm using, it draws .98 amps while pumping, .76 when empty. Hope that helps. --- Shannon Knoepflein <---> kycshann(at)kyol.net -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of BillRVSIX(at)aol.com Subject: AeroElectric-List: Facet Electric fuel pump ? Hello dose any have any idea how many amps the Facet fuel pump from vans draws. Working on bus load analysis and need to figure out circuit breaker size. Thanks Bill Higgins Pembroke Ma. ________________________________________________________________________________
From: "Avionics Systems" <hk53(at)his.com>
Subject: Re: Wiring harness follow up
Date: Feb 06, 2003
Just a little additional info here. The longer pins that work with the 18 gauge wire could potentially short against each other, but nothing would happen since it would be ground touching ground or power touching power. All the other pins are inside the connector and could not be affected. Also Garmin supplies insulating tubing with each GNS-430 kit to insulate those longer pins from touching each other. We use the longer pins and have never had a problem. David Buckwalter Avionics Systems, LLC. ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Feb 06, 2003
Subject: Re: EXPBUS
In a message dated 2/5/2003 4:20:50 PM Eastern Standard Time, owner-aeroelectric-list-server(at)matronics.com writes: > Still, I'm leaning towards the EXPBUS - as it must be the simplest and most > well arranged system for the homebuilder. So - to all who has been there, > done that: what's your experience/advice?? > > Hans > Hans, I don't know how much you personally respect AeroElectric Bob but see http://www.aeroelectric.com/articles/expbusad.html for his in depth critical review of the EXPBUS.=A0=A0=A0 =A0=A0=A0 And=A0 http://www.aeroelectric.com/articles/expbusthd.html for more follow thru discussions to this review online. =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 Chris ________________________________________________________________________________
From: "Cliff Shaw" <flyinggpa(at)attbi.com>
Subject: Re: Best Brand of 2.25 in Turn & Bank
Date: Feb 06, 2003
Shannon I found the list price of your TnB off there web page. $1776.00 I about fell off my chare. It is made by a instrument company , General Design, but I can't make Google find it. It does find a list of aviation company with General Design listed, so I am sure they are for real. Just NO web sight. ( just a little follow-up) Cliff Shaw 1041 Euclid ave. Edmonds WA 98020 (425) 776-5555 N229WC "Wile E Coyote" ----- Original Message ----- From: "Shannon Knoepflein" <kycshann(at)kyol.net> Subject: RE: AeroElectric-List: Best Brand of 2.25 in Turn & Bank > > The backup unit that Lancair Avionics is putting in my panel is a > Mid-Continent 2.25" unit, with a part number of 5550-8340-N5L. Hope > that helps, not sure of price, as it is all bunched in with other flight > instruments. > > --- > Shannon Knoepflein <---> kycshann(at)kyol.net > ________________________________________________________________________________
From: "Huw & Rachel" <huwrachel(at)earthlink.net>
Subject: EXPBUS
Date: Feb 06, 2003
Hans wrote on 02/05/03 >>>> >>I'll soon start on the electric system for my Europa. I'm considering the EXPBUS >>from Control Vision to be the "heart" of my system. One of the local veterans >>in the field adviced against it however (he has no personal experience with >>the EXPBUS though). He said that it looked vulnerable - and, if something would >>go wrong with it, it would take a lot of work to trouble-shoot - and most likely >>have it sent across the pond for repairs.... With of course a longtime >>grounding of the A/C as a result. Hans There is a lot of discussion in the archives of this list about the EXPBUS, but I doubt that anyone has enough airtime with the device to give you advice. I am planning to install an Eggenfellner Subaru in my Glastar and the recommended electrical system for that installation is based around the EXPBUS. This is mainly because it supports automatic switching between batteries in a dual battery setup. I strongly disagree with the choice of the EXPBUS not on grounds of its technical capabilities, because I don't have the knowledge to argue, but on its repairability. I keep hoping that Bob or someone else will produce a wiring diagram that we can pick up and use for building. That diagram would of course be based on standard components available from a number of sources. Meanwhile I read Bob's book and watch here in the hope that I can find an alternate way forward. from Huw Williams huwrachel(at)earthlink.net ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: EXPBUS
Date: Feb 06, 2003
There has been a lot of dialog on this list about the unit. First some upfront comments. 1. I am using (planning to use) both this approach (EXPBUS) in a plane and Bob's dual/dual approach in another. 2. I like BOTH approaches. For me they solve different problems. 3. I am *happy* with the EXPBUS installation. So far there have been no problems with it (~75hrs) I installed one in the RV6 my partner and I are currently flying and plan a different route for another RV I have under construction. I think both approaches are just fine, you need to decide what is important to you. Some of *my* logic follows. It may not apply to anyone else's way of thinking (for either case). RV with EXPBUS 1. Wanted a contained system that allowed the "connections to be made" to a reserved space already. 2. Works well for straightforward systems 3. If anything goes wrong, the unit can be replaced (Some may think the plane has to be down if *anything* fails but I didn't see it that way. If it was a major failure, then I would try to get them to send me a loaner while it was being repaired. RV without EXPBUS 1. I plan for a more "complex" (please note the quotes) system. Basically Bob's Z14 I think. All electric. Dual alternator. Dual battery. I think the Eggenfellner (sp?) Subaru systems use the EXPBUS for this but I will be going the Aeroelectric way. 2. Z14 handles the issues I have for the second RV that I did not have for the first. There is a lot of solid logic and thinking behind the designs that Bob has made available to us over the years. It is also a matter of what you really feel comfortable working with and then flying behind. On the other hand some people feel more comfortable with a "box" they feel is straightforward, pre-tested and built by someone else. To each his own. I have seen many planes with the EXPBUS but you don't hear that much about it hear because we (me included) on this list tend to more so disciples of the "Aeroelectric Way" (for good reason). All I am saying is that there is room for both approaches and if you want to dicuss a **specific** question about your potential installation, feel free to contact me off list. James p.s. Another couple of comments I forgot to add. 1. You will need to take a minute and walk through the EXPBUS design philosophy just like you need to do with Bob's. 2. Control Vision would do themselves and us all a big favor if they included a few more "application notes" ... a kinda "here's how you would hook it up for A, here's how for B and here's how for C. The system has a lot more flexibility than meets the eye, but you have tostudy it to realize that. > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] > Sent: Wednesday, February 05, 2003 4:20 PM > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: EXPBUS > > > Hi all. > > I'll soon start on the electric system for my Europa. I'm > considering the EXPBUS from Control Vision to be the "heart" of > my system. One of the local veterans in the field adviced against > it however (he has no personal experience with the EXPBUS > though). He said that it looked vulnerable - and, if something > would go wrong with it, it would take a lot of work to > trouble-shoot - and most likely have it sent across the pond for > repairs.... With of course a longtime grounding of the A/C as a result. > > Still, I'm leaning towards the EXPBUS - as it must be the > simplest and most well arranged system for the homebuilder. So - > to all who has been there, done that: what's your experience/advice?? > > Hans > > ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: EXPBUS
Date: Feb 06, 2003
Huw raises an important point ... repairability. And personally I think this might be the most relevant point. What one needs to do though is a failure mode analysis ... what is likely to fail when and how and what will its impact be on my flight. (We have all heard that here before). Basic things that could fail .. Mechanical Switches "Connections" "Polyfuse Switch" (name??) Capacitors, diodes in circuit Mechanical Switches ... Changing the switch is straightforward. Also, it is possible to use the SAME switches that you would otherwise use if that was a concern. Connections ... The same Fast-on (name??) tabs used here. Polyfuse Switch ... If one of these fails, you have the ability (on some later models I believe) to insert a standard fuse and simply loose the "reset" capability. Caps, diodes etc .... This would be more problematic. Now you need to ask what components of you panel would be taken out. THere are some specific things that I did to try to minimize the downside here. Don't have it all before me but I would be willing to **TRY** to answer a specific question about the installation. James By the way .... I have **NO** conection to CV other than being a customer. I believe their system "works" for some people and not for others Your mileage may vary > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Huw & > Rachel > Sent: Thursday, February 06, 2003 11:54 AM > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: EXPBUS > > > > > Hans wrote on 02/05/03 >>>> > > >>I'll soon start on the electric system for my Europa. I'm > considering the > EXPBUS > >>from Control Vision to be the "heart" of my system. One of the local > veterans > >>in the field adviced against it however (he has no personal experience > with > >>the EXPBUS though). He said that it looked vulnerable - and, if > something > would > >>go wrong with it, it would take a lot of work to trouble-shoot > - and most > likely > >>have it sent across the pond for repairs.... With of course a longtime > >>grounding of the A/C as a result. > > Hans > > There is a lot of discussion in the archives of this list about > the EXPBUS, > but I doubt that anyone has enough airtime with the device to give you > advice. I am planning to install an Eggenfellner Subaru in my > Glastar and > the recommended electrical system for that installation is based > around the > EXPBUS. This is mainly because it supports automatic switching between > batteries in a dual battery setup. I strongly disagree with the choice of > the EXPBUS not on grounds of its technical capabilities, because I don't > have the knowledge to argue, but on its repairability. I keep hoping that > Bob or someone else will produce a wiring diagram that we can pick up and > use for building. That diagram would of course be based on standard > components available from a number of sources. > > Meanwhile I read Bob's book and watch here in the hope that I can find an > alternate way forward. > > from > Huw Williams > huwrachel(at)earthlink.net > > ________________________________________________________________________________
Date: Feb 06, 2003
From: "William Yamokoski" <yamokosk(at)lmc.cc.mi.us>
Subject: Re: EXPBUS
Just a minor point of clarification....the Eggenfellner EXPBUS design is for dual batteries, one alternator. I didn't use it...went with a basic Bob design, mainly because I already had most of the parts before deciding on the Eggenfellner engine. Wonder if using EXPBUS would have toned down my miserable radio noise....NAH! Bill Yamokoski ________________________________________________________________________________
From: brucem(at)olypen.com
Subject: EXPBUS
Date: Feb 06, 2003
Hans, The EXPBUS uses poly fuses (solid state, self-resetting devices). See the AeroElectric book and website for some strong negative opinions on these. Regards, Bruce McGregor --------------------------------------------- This message was sent using OlyPen's WebMail.
http://www.olypen.com ________________________________________________________________________________
Date: Feb 06, 2003
Subject: Re: Facet Electric fuel pump ?
From: czechsix(at)juno.com
Bill, I asked this question to Craig Weber, Facet's engineering rep, a while back and the answer for the pump Vans sells (model # 40108) is 1.4 amps. I went with the "beer can" style pump instead on my RV, not because it draws less current (1 A) but because I like the inlet filter screen and it also fit in the wingroot where I wanted to mount it. --Mark Navratil Cedar Rapids, Iowa RV-8A N2D firewall forward.... ------------------------------------------------------ Mark, The 478360 draws 1 amp max. The 40108 draws 1.4 amps max. Regards Craig > ---------- > From: > menavrat(at)rockwellcollins.com[SMTP:menavrat(at)rockwellcollins.com] > Sent: Monday, July 23, 2001 1:40 PM > To: Weber, Craig > Subject: RE: Interrupter Fuel Pump Question > > > Hi Craig, > > Can you tell me the max current or power requirements for the 478360 > interrupter fuel pump (@12 VDC)? > Also for comparison sake, what is the power req'ts for the solid state > 40108 pump (also 12 VDC)? > > Thanks, > > --Mark Navratil From: BillRVSIX(at)aol.com Subject: AeroElectric-List: Facet Electric fuel pump ? Hello dose any have any idea how many amps the Facet fuel pump from vans draws. Working on bus load analysis and need to figure out circuit breaker size. Thanks Bill Higgins Pembroke Ma. ________________________________________________________________________________
From: "Stucklen, Frederic IFC" <Fred.Stucklen(at)UTCFuelCells.com>
Subject: CarlingTech PWM Dimmer (long)
Date: Feb 06, 2003
Listers, Yesterday I received an electronic dimmer from Carling Technologies that was previously talked about on the Aeroelectric List. (see http://www.carlingtech.com/products/switches/ld_series.asp ). This is a digital PWM circuit that is capable of 10A of current, with an output that is adjustable from 0-100% duty cycle. (i.e., full OFF to full ON. 50% duty cycle would essentially be a square wave..). It has a three wire interface: +12VDC, Output, and Ground, with 1/4" fast-on tabs, so it's real simple to hook up. In my case, the dimmer power and all lights are brought to a terminal strip, so running a twisted pair of #18 wire to the dimmer, and another #18 wire from the dimmer to the avionics common ground, only took a few minutes to complete. (I did not mount it into the panel yet..) The part I evaluated is a LD3A1CC1-3AAFE-1FC. (12v, 10A, 11 step, Red led labeling, black case, rocker switch, "Bright/DIM" labeling. See the Carling web site for other versions). When I first heard of this device, my main concern centered about the interference it might cause to the IFR panel I'm installing in my new RV-6A. In a previous IFR RV-6A, I had designed and installed a PWM style dimmer, and had to take special care to avoid EMI that would negate it's usefulness in an avionics panel. Among other design issues, I found that by using relatively low switching frequencies, controlling the rising and falling edges of the switching waveform, using proper bypass and grounding techniques, and using twisted pairs for power leads, the EMI was issues were eliminated. I was pleasantly surprised to find that these issues have been properly addressed in the Carling LD-Series dimmer circuit. Even with the dimmer next to the antenna of a COMM radio, I was not able to detect any significant EMI on either the COMM or VOR/ILS frequency ranges. I was also not able to detect any perceptible additional noise in an adjacent AM radio over the entire AM band, so it shouldn't effect ADF's. With the dimmer near it's intended mounting location, I couldn't detect any interference on any of the radios. (see http://www.matronics.com/photoshare/Fred.Stucklen@UTCFuelCells.com.01.19.200 3/ for an earlier picture of my panel..) Any noise I was able to detect, at any test condition, was only with the radio squelch open and the audio turned up. Even this was barely perceptible. While this test was done in the shop, and not out in the quiet electrical domain of an open field, I'm relatively confident that the device will not cause any electrical interference to the avionics. Putting an oscilloscope on the dimmers output revealed a 200 Hz PWM waveform with smooth rise/fall time transitions and no spikes or overshoots when driving a load of standard incandescent bulbs and some LED's (i.e., no additional inductive loads...). Switch turn off times were about 60 uSec (0V - 12 Vdc) with a max Dv/Dt of 9V/50 uSec. Switch turn on times were a bit faster at 20 uSec (12 Vdc - 0V) with a max Dv/Dt of -9V/15uSec. The PWM duty cycle was adjustable from 0-100% in .5mS steps. With a 5 mS period for the frequency, that results in 11 steps over the full range of control (including OFF). For some, this might not be fine enough control. But turning out the lights in the shop, and playing around with the dimmer while sitting in the cockpit, convinced me that it should do the job for me. According to Carling Technologies, the dimmer retail cost is about $35.00. I'm trying to get a quote from a local distributor for cost and delivery times...... Fred Stucklen RV-6A N926RV (Reserved) ________________________________________________________________________________
Date: Feb 07, 2003
From: John Mireley <mireley(at)pilot.msu.edu>
Subject: OT: Cockpit floors could become 'invisible' to assist
pilots in landing. I can't imagine trying a landing while looking straight down at the runway. http://story.news.yahoo.com/news?tmpl=story&u=/ap/20030207/ap_on_fe_st/japan_invisible_2 ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Re: AeroElectric-List Digest: 34 Msgs - 01/07/03
Date: Feb 07, 2003
If I separate the Firewall Ground Block and the Panel Ground Block on an Aluminum airplane (RV-9A), do I need to connect the two of them with a 2AWG wire or is the firewall that they are rivetted to sufficent ground connection between them? - Jim ________________________________________________________________________________
From: "Tom Schiff" <tomschiff(at)attbi.com>
Subject: OT: Cockpit floors could become 'invisible' to
assist pilots in landing.
Date: Feb 07, 2003
I remember talking to a WW II ace his squadron lost a number of planes because it was possible to look down and see the runway through the open gear doors. In doing so the pilots lost the perspective of where they were. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of John Mireley Subject: AeroElectric-List: OT: Cockpit floors could become 'invisible' to assist pilots in landing. I can't imagine trying a landing while looking straight down at the runway. http://story.news.yahoo.com/news?tmpl=story&u=/ap/20030207/ap_on_fe_st/j apan_invisible_2 ________________________________________________________________________________
From: John Schroeder <jschroeder(at)perigee.net>
Date: Feb 07, 2003
Subject: Re: AeroElectric-List Digest: 34 Msgs - 01/07/03
Jim - Buy the combo ground block from B&C and the hardware comes with it to join them together. You drill holes thru the firewall and mount them back-to-back with the studs, washers and nuts. The studs act like a wire/busbar. John 2/7/2003 2:54:41 PM, "Jim Pack" wrote: > >If I separate the Firewall Ground Block and the Panel Ground Block on an >Aluminum airplane (RV-9A), do I need to connect the two of them with a 2AWG >wire or is the firewall that they are rivetted to sufficent ground >connection between them? > >- Jim ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Ground Block
Date: Feb 07, 2003
I am using the B&C Ground Block, however, the space on the engine site where it is best placed, does not correspond to the space on the cabin side. They need to be offset by a foot. So, I have riveted the two sides into the most appropriate place for the application on the respective sides of the firewall. Is that OK or do I need to wire them together with 2AWG? - Jim > > Jim - > > Buy the combo ground block from B&C and the hardware comes with it to join them > together. You drill holes thru the firewall and mount them back-to-back with the > studs, washers and nuts. The studs act like a wire/busbar. > > John > > >If I separate the Firewall Ground Block and the Panel Ground Block on an > >Aluminum airplane (RV-9A), do I need to connect the two of them with a 2AWG > >wire or is the firewall that they are rivetted to sufficent ground > >connection between them? > > > >- Jim > ________________________________________________________________________________
From: "John Karnes" <jpkarnes(at)charter.net>
Subject: OV circuit breaker tripping
Date: Feb 07, 2003
Bob- I have an auto conversion engine with nippodenso alternator. It has an internal voltage regulator. After a really bad overheating condition, the OV circuit breaker is tripping every time the engine starts running. Changing to the new "yellow lead" module didn't help. Can I assume the regulator is faulty. If so, can I run the wire from the alternator into an aftermarket regulator to fix this problem or do I need to purchase a whole new alternator? Thanks. John Karnes Port Orchard, WA Zenith 601HDS w/Stratus Subaru engine ________________________________________________________________________________
From: TimRhod(at)aol.com
Date: Feb 08, 2003
Subject: voltage regulators
Can any one tell me where they usually mount voltage regulators in a canard pusher? I seems with three or four wires needing to go to the panel, warning light, panel ground, and only one going to the alternator that it would be best to put it in the nose. Tim Rhodenbaugh, Velocity XL, timrhod(at)aol.com Thanks ________________________________________________________________________________
Date: Feb 08, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: voltage regulators
> >Can any one tell me where they usually mount voltage regulators in a canard >pusher? I seems with three or four wires needing to go to the panel, warning >light, panel ground, and only one going to the alternator that it would be >best to put it in the nose. Tim Rhodenbaugh, Velocity XL, timrhod(at)aol.com >Thanks That would be my choice. Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
Date: Feb 08, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: OV circuit breaker tripping
> >Bob- > I have an auto conversion engine with nippodenso alternator. It has an >internal voltage regulator. After a really bad overheating condition, the >OV circuit breaker is tripping every time the engine starts running. >Changing to the new "yellow lead" module didn't help. Can I assume the >regulator is faulty. If so, can I run the wire from the alternator into an >aftermarket regulator to fix this problem or do I need to purchase a whole >new alternator? Thanks. You can have the alternator repaired at an automotive shop . . . if the regulator is bad, they'll replace it. Did you notice the voltmeter in your airplane before the trip? Was it indeed running 16 volts or more? Bob . . . ________________________________________________________________________________
Date: Feb 08, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Ground Block
> >I am using the B&C Ground Block, however, the space on the engine site where >it is best placed, does not correspond to the space on the cabin side. They >need to be offset by a foot. So, I have riveted the two sides into the most >appropriate place for the application on the respective sides of the >firewall. Is that OK or do I need to wire them together with 2AWG? The idea was that all cranking currents would be carried by no part of the airframe or any components that held it together. Hence, the 5/16" brass bolt intended to connect cockpit side grounds with engine compartment grounds. It wouldn't hurt anything to run a fatwire jumper between them . . . Bob . . . ________________________________________________________________________________
Date: Feb 08, 2003
From: richard(at)riley.net
Subject: Re: voltage regulators
> > > > > >Can any one tell me where they usually mount voltage regulators in a canard > >pusher? I seems with three or four wires needing to go to the panel, warning > >light, panel ground, and only one going to the alternator that it would be > >best to put it in the nose. Tim Rhodenbaugh, Velocity XL, timrhod(at)aol.com > >Thanks > > > That would be my choice. We always mount them to the canard bulkhead, between the lift tabs. ________________________________________________________________________________
Date: Feb 08, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Best LED color for preserving night
vision > > >I'm designing a ceiling mounted headphone jack with integral LEDs for cabin >light. It will have both a white LED and another color. Initially, I was >thinking I would use red, but I vaguely recall that the military has >determined that another color, perhaps green, was better as long as this was >kept at a low level. A brief Google search found at least one reference >confirming this vague notion. http://www.corvus.com/kniffen.htm is an >astronomy reference. . . . it is indeed a vague notion. About 35 years ago, red flood lighting was standard in the small Cessnas . . . for lots of dollars extra, one could install the optional red or blue/white post lights. One can find about as many opinion/reason combinations as there are pilots . . . some of whom will have never flown at night. EVERY color of light, if kept at a level just bright enough to see that all is well, will probably do just fine. Individuals may find that they favor or have problems with one color over another but I'll bet that has more to do with individual physiology than for any standard rules-of-thumb for cockpit lighting. Besides, if you're using flood lighting, changing colors later to suit your personal preferences is easy . . . Bob . . . ________________________________________________________________________________
Date: Feb 08, 2003
From: John Rourke <jrourke@allied-computer.com>
Subject: Re: Best LED color for preserving night vision
I bought one of those LED gooseneck lights with 6 LEDs in it - but I'm replacing them with two red, 2 green and 2 blue LEDs, and a 6-position DIP switch to program whatever color I want. It will be interesting to discover what color I find to be most effective, and what others prefer. -John R. (Actually, maybe I'll put in TWO 6p dipswitches, and a on-off-on DPST so I can compare two different colors in flight) > > >> >> >>I'm designing a ceiling mounted headphone jack with integral LEDs for cabin >>light. It will have both a white LED and another color. Initially, I was >>thinking I would use red, but I vaguely recall that the military has >>determined that another color, perhaps green, was better as long as this was >>kept at a low level. A brief Google search found at least one reference >>confirming this vague notion. http://www.corvus.com/kniffen.htm is an >>astronomy reference. > > > > . . . it is indeed a vague notion. About 35 years ago, red > flood lighting was standard in the small Cessnas . . . for lots > of dollars extra, one could install the optional red or blue/white > post lights. One can find about as many opinion/reason combinations > as there are pilots . . . some of whom will have never flown at > night. > > EVERY color of light, if kept at a level just bright enough > to see that all is well, will probably do just fine. Individuals > may find that they favor or have problems with one color over > another but I'll bet that has more to do with individual > physiology than for any standard rules-of-thumb for cockpit > lighting. Besides, if you're using flood lighting, changing > colors later to suit your personal preferences is easy . . . > > Bob . . . > > > > > > > > ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Re: Ground Block
Date: Feb 08, 2003
So, you feel it is worth a hole in the firewall to connect the two grounds? - Jim > >I am using the B&C Ground Block, however, the space on the engine site where > >it is best placed, does not correspond to the space on the cabin side. They > >need to be offset by a foot. So, I have riveted the two sides into the most > >appropriate place for the application on the respective sides of the > >firewall. Is that OK or do I need to wire them together with 2AWG? > > The idea was that all cranking currents would be carried by > no part of the airframe or any components that held it together. > Hence, the 5/16" brass bolt intended to connect cockpit side > grounds with engine compartment grounds. It wouldn't hurt anything > to run a fatwire jumper between them . . . > > Bob . . . > ________________________________________________________________________________
From: "Jim Pack" <jpack(at)igs3.com>
Subject: Ground Block
Date: Feb 08, 2003
What benefit does this offer? Is it corrosion, or is it interference with other electrical stuff, or what? - Jim > The idea was that all cranking currents would be carried by > no part of the airframe or any components that held it together. ________________________________________________________________________________
Date: Feb 08, 2003
From: Rico Voss <vozzen(at)yahoo.com>
Subject: Re: Best LED color for preserving night vision
After 20+ years in the merchant marine, on the darkened bridge of a ship, I've learned that there is good reason for the traditional red lighting. I feel that the red lighting can be cranked up enough to be useful, yet still allows the eye to recover instantly when vision is taken back into the darkness outside the window. Other colors, turned up to a useful intensity, are harder to recover from. Of course, the option is to run any color at a lower level. But in general, my vote would be RED. --Richard ________________________________________________________________________________
From: John Schroeder <jschroeder(at)perigee.net>
Date: Feb 08, 2003
Subject: Re: Best LED color for preserving night vision
John R. Where did you get the 6 LED gooseneck light? Thanks, John >I bought one of those LED gooseneck lights with 6 LEDs in it ________________________________________________________________________________
From: "Eric M. Jones" <emjones(at)charter.net>
Subject: My Web Site Finally
Date: Feb 08, 2003
Please check out and save the link for: www.PerihelionDesign.com All sorts of aero-related stuff for sale and in development. This site is best viewed with IE and a PC. Macs and Netscape seem to be a problem. I'm working on it. I made this wesite with a bunch of Webwizards from Excel and MSWord, so who knows? Regards, Eric M. Jones ________________________________________________________________________________
Date: Feb 09, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Ground Block
> >What benefit does this offer? Is it corrosion, or is it interference with >other electrical stuff, or what? > >- Jim > > > The idea was that all cranking currents would be carried by > > no part of the airframe or any components that held it together. This is but one of many building blocks that make up the design goal for a quiet, maximum performance electrical system. When airplanes first got batteries and starters, few, if any, of these building blocks were perceived or even necessary. Nowadays, most are understood but application on certified iron is sporadic . . . oft shoved aside by traditional, political or regulatory decision making processes. The quietest airplanes minimize use of airframe to carry power or signal currents on the airframe for either potential victims or potential antagonists but particularly potential victims. The single-point ground system was a no-brainer feature of the composite airplane . . . and many have been constructed over the years with noise free systems. Metal airplanes can derive equal benefit by adopting similar philosophies. Ground loop coupling of effects between systems simply cannot occur when there are no loops (multiple grounds on airframes that carry currents for multiple systems). Will your airplane suffer the indignities of a trashy system for having pushed one design goal aside? Probably not. Will you suffer some drop in performance? Probably none that you will perceive . . . many airplanes we've grown up with over the years have electrical performance issues that can only be calculated and/or measured. As humans pushing buttons and twisting knobs, our ability to resolve variability in system performance is extremely limited. Just try to be sensitive to the fact that brushing COMBINATIONS of building blocks aside can digress your system back toward what we've been told (by both manufacturers and regulators) are "the best airplanes we know how to build." I hope our associations here and elsewhere in the OBAM aircraft community have exposed what a sad joke that is. Bob . . . ________________________________________________________________________________
Date: Feb 09, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Ground Block
> >So, you feel it is worth a hole in the firewall to connect the two grounds? > >- Jim That's the way it was designed . . . ________________________________________________________________________________
From: "Sam Hoskins" <shoskins(at)Globaleyes.net>
Subject: Fuse reccomendation
Date: Feb 09, 2003
I am retrofitting my Q-200 with a B&C 200G alternator. Their drawing calls for a 15a fuse on the engine side of the firewall. What would be a recommended fuse and holder for this application? I didn't find anything in the AEC catalog, maybe I'm just not looking in the right place. The catalog said the ATC fuseblock was not reccomended for continous loads more than 7a. Sam Hoskins Murphysboro, IL Quickie Q-200 Flying since '86 with over 1,200 hours. http://home.globaleyes.net/shoskins/page1.htm ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Feb 09, 2003
Subject: Re: My Web Site Finally
In a message dated 2/8/03 2:24:24 PM Pacific Standard Time, emjones(at)charter.net writes: << www.PerihelionDesign.com >> Hi Eric, I tried the website this morning and for some reason none of the links respond, plus there are no illustrations except for the picture of the Glastar at the top but it looks as if you intended there to be some. I am using a PC with Microsoft Office 97 on an old IBM notebook so it may be my equipment. Harry Crosby Pleasanton, California RV-6, starting firewall forward ________________________________________________________________________________
From: "Ageless Wings" <harley(at)AgelessWings.com>
Subject: My Web Site Finally
Date: Feb 09, 2003
Harry.... The pictures are quite large...he didn't reduce them to a manageable size. So, if you are trying to load it with a dialup modem, they may take quite awhile. I have a DSL line, and I thought there was a mistake at first, too...but eventually they all loaded....the links followed. Harley >> -----Original Message----- >> From: owner-aeroelectric-list-server(at)matronics.com >> [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of >> HCRV6(at)aol.com >> Sent: Sunday, February 09, 2003 1:09 PM >> To: aeroelectric-list(at)matronics.com >> Subject: Re: AeroElectric-List: My Web Site Finally >> >> >> >> In a message dated 2/8/03 2:24:24 PM Pacific Standard Time, >> emjones(at)charter.net writes: >> >> << www.PerihelionDesign.com >> >> >> Hi Eric, I tried the website this morning and for some reason >> none of the >> links respond, plus there are no illustrations except for the >> picture of the >> Glastar at the top but it looks as if you intended there to be >> some. I am >> using a PC with Microsoft Office 97 on an old IBM notebook so it >> may be my >> equipment. >> >> Harry Crosby >> Pleasanton, California >> RV-6, starting firewall forward >> >> >> >> >> >> >> ________________________________________________________________________________
Date: Feb 09, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Fuse reccomendation
> > >I am retrofitting my Q-200 with a B&C 200G alternator. Their drawing >calls for a 15a fuse on the engine side of the firewall. > >What would be a recommended fuse and holder for this application? I >didn't find anything in the AEC catalog, maybe I'm just not looking in the >right place. The catalog said the ATC fuseblock was not reccomended for >continous loads more than 7a. The fuse blocks are rated by the manufacturer at up to 30A per slot. For aircraft use we've recommended de-rating to 15A per slot . . . and then only for loads like pitot heat and klieg-lights you may have bolted on for night landings. The single ATC fuse holder at http://www.aeroelectric.com/Catalog/ckrtprot/ckrtprot.html#ifh-2 is also RATED for much more . . . about 20A as I recall. You could use this with a 15A fuse in it for the 200G alternator. If it were my airplane, I'd wire per figure Z-16 of Appendix Z and use a 20AWG fusible link on the end of a 16AWG or 14AWG feeder . . . the feeder/link combination shown on Figure Z-16 is appropriate for the larger, Rotax alternator. Bob . . . ________________________________________________________________________________
Date: Feb 09, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: MicroSwitch vs. Carling Differences
Over the years, AeroElectric Connection drawings have depicted a mixture of progressive transfer switches by Honeywell-MicroSwitch and Carling (who makes the S700-Series switches stocked at B&C. Until all the documentation can be updated to resolve differences between the two brands see the benchmark document at: http://www.aeroelectric.com/articles/Carling_Micro/Carling_Micro.pdf These differences have left a few pitfalls for generating new drawings from the archives of old drawings. One has to be careful lest artifacts of both switch brands get intermixed. Just such a snafu occurred when instructions for the LV_Warn/ABMM modules were crafted. For those of you who have received LV_Warn Modules from the first production batch, B-revision instructions have been posted at: http://www.aeroelectric.com/Catalog/AEC/9005/9005-701B.pdf The second production batch is being finished now and will be shipped tomorrow with Revision B instructions. Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
From: "Sam Hoskins" <shoskins(at)Globaleyes.net>
Subject: Re: Fuse reccomendation
Date: Feb 09, 2003
Ok, I see that. I was already considering a fuselink, but some or your writings (page 10-4)seemed to discourage them in the current ranges we are talking about here. Re-reading it, I see you addressed PM alternators. While I'm looking at Z-16 - what is the purpose of the 22AWG fuselink in series with the 5a breaker? Isn't that redundent redundent? Sam ----- Original Message ----- From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: Fuse reccomendation > > > > > > >I am retrofitting my Q-200 with a B&C 200G alternator. Their drawing > >calls for a 15a fuse on the engine side of the firewall. > > > >What would be a recommended fuse and holder for this application? I > >didn't find anything in the AEC catalog, maybe I'm just not looking in the > >right place. The catalog said the ATC fuseblock was not reccomended for > >continous loads more than 7a. > > The fuse blocks are rated by the manufacturer at up to 30A > per slot. For aircraft use we've recommended de-rating to 15A > per slot . . . and then only for loads like pitot heat and > klieg-lights you may have bolted on for night landings. > > The single ATC fuse holder at > > http://www.aeroelectric.com/Catalog/ckrtprot/ckrtprot.html#ifh-2 > > is also RATED for much more . . . about 20A as I recall. > You could use this with a 15A fuse in it for the 200G > alternator. > > If it were my airplane, I'd wire per figure Z-16 of Appendix > Z and use a 20AWG fusible link on the end of a 16AWG or > 14AWG feeder . . . the feeder/link combination shown on > Figure Z-16 is appropriate for the larger, Rotax alternator. > > Bob . . . > > ________________________________________________________________________________
Date: Feb 10, 2003
From: John Rourke <jrourke@allied-computer.com>
Subject: Re: Best LED color for preserving night vision
I'm checking... I can't find my receipt, and this link isn't where I bought it from, but it looks like the same thing and I think has the same part number - but I didn't pay as much for it (and I know there were several models with various combinations of color/quantity of LEDs): http://www.cetsolar.com/3ledcabin.htm I'll look for the receipt when I get back to the hangar next week - but in any event, I think I'll end up modifying it so much (or destroying it in the process) that I should probably just make my own - all I really need is the swivel mount (gooseneck was the wrong word) -John R. John Schroeder wrote: > > John R. > > Where did you get the 6 LED gooseneck light? > > Thanks, > > John > > >>I bought one of those LED gooseneck lights with 6 LEDs in it > > > > > > > > > ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Fuse reccomendation
> > >Ok, I see that. I was already considering a fuselink, but some or your >writings (page 10-4)seemed to discourage them in the current ranges we are >talking about here. Re-reading it, I see you addressed PM alternators. > >While I'm looking at Z-16 - what is the purpose of the 22AWG fuselink in >series with the 5a breaker? Isn't that redundent redundent? Fuseblock (and bus) may be mounted somewhat remotely from the panel and the 5A field breaker. If you EXTEND the bus with a wire up to the breaker, it should be protected. If you use a FUSE in the fuse block, then because of the much faster response time of a fuse, a 15A fuse might open faster than a 5A breaker . . . so we use a fusible link with a time constant that is greater than a breaker to protect that wire segment. Bob . . . ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Order processing system on the fritz
The website's order-form program was down from February 1 through February 9. If you placed an order within this interval and received a copy of it via your e-mail, check the serial number of the order in the subject line of the echo. We've lost serials 870 through 921. If your order fell within this group -OR- if you placed and order and did NOT receive an e-mail copy, please do us the kindness of re-entering your order now. If you have any questions, please call Bob at 316.685.8617 for AEC orders or Todd at 316.283.8000 for B&C orders. Ya gotta love these computers . . . otherwise we couldn't put up with them! Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
From: N823ms(at)aol.com
Date: Feb 10, 2003
Subject: Autocad LT
Bob: Asked my son about the Autocad LT at the bookstore of Ole Miss. If you go to JourneyED.Com, you will see a list of AutoCAD's. Which one are you talking about? There are a few around 150.00. Thanks, Ed Silvanic N823MS(at)aol.com ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Autocad LT
> >Bob: > > Asked my son about the Autocad LT at the bookstore of Ole Miss. If >you go to JourneyED.Com, you will see a list of AutoCAD's. Which one are you >talking about? There are a few around 150.00. > >Thanks, > >Ed Silvanic >N823MS(at)aol.com Autocad LT 2002 for $149.98 would be my suggestion. It is "light" in name only . . . VERY powerful program. Bob . . . ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Facet Electric fuel pump ?
> >Bill, I asked this question to Craig Weber, Facet's engineering rep, a >while back and the answer for the pump Vans sells (model # 40108) is 1.4 >amps. I went with the "beer can" style pump instead on my RV, not because >it draws less current (1 A) but because I like the inlet filter screen and >it also fit in the wingroot where I wanted to mount it. > >--Mark Navratil >Cedar Rapids, Iowa >RV-8A N2D firewall forward.... Does anyone have a Facet pump they could send me for some REAL energy measurements? I'd like to set one up to pump a fix pressure head and put a data acquisition system on it to plot the current curve (ya can't put a simple ammeter in series with a critter that pulses) . . . I'd really like to get some good data on one. Bob . . . ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: EXPBUS
> >In a message dated 2/5/2003 4:20:50 PM Eastern Standard Time, >owner-aeroelectric-list-server(at)matronics.com writes: > > > Still, I'm leaning towards the EXPBUS - as it must be the simplest and most > > well arranged system for the homebuilder. So - to all who has been there, > > done that: what's your experience/advice?? If for no other reasons: (1) The EXPbus may or may not have all the circuit features you need. What you see is what you get for now and in the future. (2) The EXPbus is warmed-over 1960's certifie-iron architecture. (3) For what the EXPbus costs, we can buy all the circuit protection, switches, terminals, wire, contactors and installation supplies to do any of the Z-figures or a variation thereof) and have money left over. Bob . . . ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: ABMM
> >Bob! > >If I wire the switch per the terminal number sequence shown in Fig 11-11 >of Aeroconnection, it works as advertised regarding closing the contactor >in the bat and alt position. Figure 7 of the ABMM schematic shows >a (2-10) switch terminals only. The (2-10) switch terminals shown in the >notes section of Figure 7 indicates a S700 (2-10) switch, mounted keyway >up. I'll use the terminal layout shown in Fig 11-11 for all (2-10) >switches (obtained from B&C) for my aircraft wiring. See http://www.aeroelectric.com/articles/Carling_Micro/Carling_Micro.pdf Thanks for bringing this to my attention . . . ________________________________________________________________________________
Date: Feb 10, 2003
Subject: parallel resistor for LED used with LR-3?
From: czechsix(at)juno.com
Bob, I found in the archives a reference where you recommended a 220 ohm resistor to be used in parallel with an LED when used to replace the incandescent bulb in the LR-3 Low voltage warning circuit. Then I also have a sketch you posted for someone not too long ago showing the same thing only in this case you recommend a 470 ohm resistor for the parallel resistor. Is it 220, 470, or does it matter? I don't know how much current the LR-3 sinks in the OFF state so I'm not sure how to calculate what it should be. For what it's worth, Greg Toman suggests a 1K resistor to be used with his engine monitor warning light if replaced with an LED, but his circuit may not sink the same amount of current as the LR-3....so maybe that's a moot point. Thanks, --Mark Navratil Cedar Rapids, Iowa RV-8A N2D firewall forward.... ________________________________________________________________________________
Date: Feb 10, 2003
Subject: Lonestar Mag Filter - Success
From: "Matt Prather" <mprather(at)spro.net>
After some struggle to quiet the original magneto ignition system on my VariEze, I have some sucess to report. I replaced one of the mags with an old-style LSE CDI ignition, and I had the remaining mag rebuilt (new coil, points, condensor, timing adjusted, etc). There was still quite a bit of crackle showing up on my comm radio. The LSE ignition is very quiet, but it bothered me that the mag was only slightly better after the rebuild than before, and 10x worse than the LSE. Out of a small amount of desperation, I ordered one of the Lonestar Mag Filters from 'Spruce, and installed it over the weekend. I am happy to report that it made a huge difference in the system. While the mag is still noisier than the LSE, it only takes about 1/2 available squelch to cover it up. Interestingly, (to me) even when I turn the squelch down, the amplitude of the noise is much less than before. Lonestar touts the effectiveness of the coaxial design of their filter, and from my recent experience I can't argue. I didn't try any other style of cap, however. I suspect that part of my difficulties came from the VE not providing any shielding that an Al airplane might enjoy. Matt (Quiet and Happy) Prather N34RD ________________________________________________________________________________
Date: Feb 10, 2003
From: Mark Steitle <msteitle(at)mail.utexas.edu>
Subject: Re: Best LED color for preserving night
vision The LED Light.com has a variety of led fixtures. One looks like the one referenced by John R. See http://www.theledlight.com/interior.html Mark S. ><jrourke@allied-computer.com> > >I'm checking... I can't find my receipt, and this link isn't where I >bought it from, but it looks like the same thing and I think has the >same part number - >-John R. > > >John Schroeder wrote: > > > > > John R. > > > > Where did you get the 6 LED gooseneck light? > > > > Thanks, > > > > John > > > > > >>I bought one of those LED gooseneck lights with 6 LEDs in it > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Subject: Garmin 196
Date: Feb 10, 2003
From: "David.vonLinsowe" <David.vonLinsowe(at)delphi.com>
I'm toying with the idea of panel mounting a Garmin 196. Has anyone used one at night? How good is the visibility/readability of the display at night? Thanks, Dave RV-6 ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: parallel resistor for LED used with
LR-3? > >Bob, > >I found in the archives a reference where you recommended a 220 ohm >resistor to be used in parallel with an LED when used to replace the >incandescent bulb in the LR-3 Low voltage warning circuit. Then I also >have a sketch you posted for someone not too long ago showing the same >thing only in this case you recommend a 470 ohm resistor for the parallel >resistor. 470 ohm series resistance will give you about 21 mA of lamp current. 220 raises it to 45 mA. The high intensity red lamps I use really get your attention at 45 mA! >Is it 220, 470, or does it matter? I don't know how much current the LR-3 >sinks in the OFF state so I'm not sure how to calculate what it should be. The LR-3 pulls down at about 2 mA in the off state. Putting a 220 ohm resistor across the LED and then a 220-470 ohm resistor in series with the lamp/led combo will get it lit up in good shape. You need the 220 across the lamp to keep it dark while off-state leakage is present. >For what it's worth, Greg Toman suggests a 1K resistor to be used with his >engine monitor warning light if replaced with an LED, but his circuit may >not sink the same amount of current as the LR-3....so maybe that's a moot >point. This would give you about 10 mA on most lamps. This will get you quite a bit of light too . . . Bob . . . |-------------------------------------------------------| | The man who does not read good books has no advantage | | over the man who cannot read them. | | - Mark Twain | |-------------------------------------------------------| ________________________________________________________________________________
From: "kc" <samdacat(at)elp.rr.com>
Subject: Re: Facet Electric fuel pump ?
Date: Feb 10, 2003
I have a new Facet #40108 that I won't need for the next month or two if that will help. ----- Original Message ----- From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: Re: Facet Electric fuel pump ? > > > > >Bill, I asked this question to Craig Weber, Facet's engineering rep, a > >while back and the answer for the pump Vans sells (model # 40108) is 1.4 > >amps. I went with the "beer can" style pump instead on my RV, not because > >it draws less current (1 A) but because I like the inlet filter screen and > >it also fit in the wingroot where I wanted to mount it. > > > >--Mark Navratil > >Cedar Rapids, Iowa > >RV-8A N2D firewall forward.... > > Does anyone have a Facet pump they could send me for some > REAL energy measurements? I'd like to set one up to pump > a fix pressure head and put a data acquisition system on > it to plot the current curve (ya can't put a simple ammeter > in series with a critter that pulses) . . . > > I'd really like to get some good data on one. > > Bob . . . > > ________________________________________________________________________________
From: Benford2(at)aol.com
Date: Feb 10, 2003
Subject: Garmin 196
The lighting is PERFECT !!!!! It still amazes me how damn smart and accurate that little box can be. Without a doubt the best 890.00$ I ever spent.Now, if they would make a bigger display I would get rid of my King KMD150 and make the 196 center of attention. ________________________________________________________________________________
Date: Feb 10, 2003
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Starter solenoid
Hello Bob and friends, There's nothing better than a simple experiment to lighten up. Today, I wanted to know how much current my starter solenoid was draining... I remember reading Bob's article, but I suppose I did not understand it and decided not to use an external starter contactor. Well, I connected a positive 12V to the solenoid tab of my starter and the fuse from my battery pack blew (a 15A fuse). I replaced it with a 20A fuse and it blew after a few seconds... wow. What's happening? I thought that the solenoid needed only 8 amps or so. Bob's article on starter solenoid explains that very well. There are probably two windings on the solenoid, one of them connected to the contactor on the motor side. So, initially, the solenoid can draw quite a bit of current, but that second coil becomes inactive when it receives the 12V from the contactor side. At that time the demand for current from the solenoid would get lower. In my case, I did not connect 12V to the contactor side of the starter (the bolt). So, It was always demanding the high current. Now I understand that peak current thing Bob explains and I can see how it would make a switch work harder... I modified my drawing to include a starter contactor. :-) Michel ===== ---------------------------- Michel Therrien CH601-HD http://mthobby.pcperfect.com/ch601 http://www.zenithair.com/bldrlist/profiles/mthobby http://pages.infinit.net/mthobby ________________________________________________________________________________
Date: Feb 10, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Facet Electric fuel pump ?
> >I have a new Facet #40108 that I won't need for the next month or two if >that will help. I believe I have one coming already. Thanks! Watch for data to be published as soon as I can get it gathered. Bob . . . ________________________________________________________________________________
Date: Feb 11, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: re: Crowbar Device
I have recently bought one of your crowbars to fit to my Europa + Rotax 912. It is a standard Europa Club modification and fitting instructions with a circuit diagram are published. Nigel Charles, who is the club's Modifications Representative had dealings with you some while ago. I installed the crowbar plus a 40A relay, but with a 5A fuse instead of the circuit breaker. At some stage during the first flight the Crowbar operated and the fuse blew. It may have been at start-up or early in the flight, but I didn't notice. I turned off all unnecessary electrics and completed the flight on the battery alone. On inspection the 22,000uF capacitor had also blown and had leaked soot and fluid. Hmmmm . . wonder if it was hooked up backwards. Electrolytic capacitors are polarity sensitive . . . Following recommendations, I replaced the capacitor and used a slow blow 5A fuse instead. The crowbar ov module should always be used with a 5A breaker . . . The next flight was uneventful and charged the whole time, but the following flight blew the fuse on start-up. I replaced the fuse and the flight was OK. Following further recommendations, I replaced the slow blow fuse with a 5A circuit breaker. Very good . . . I also wired up a multi-meter across the regulator output and earth to monitor voltage. The next flight was OK and charger at 14.05 V. After landing and waiting for about 5 mins I started again and the c.b. blew immediately. I tried resetting it a few times, but it would not remain connected. The multi-meter recorded voltages of 35 to 40 volts depending on rpm, so I shut down the engine. Further advice was to connect the regulator control wire directly to the regulator output wire instead of to the Master solonoid output terminal. This was a mod. to the Rotax suggested circuit diagram, but had not been made to my A/C wiring. (It had run for 400 hours like this without a problem) I made the change and ground ran the engine, but it would not charge. If you have this much output from the system under any circumstances, I suspect the regulator/rectifier is hurt . . . At this stage I decided to remove all new components and restore the original circuit. When doing so, I found that the c.b. would not function properly and the insulation to the two wires to the crowbar had melted and fused together. I bridged the reg. output wires to replace the relay and ran the engine. It gave a constant charge of 13.75 volts, but I have not yet flown since to test the system thoroughly. Interesting . . . I'm wondering where the 30 volt transient went . . . I am concerned that I might have damaged the regulator which might cause it to fail at a later stage. I am still keen to use one of your crowbar devices to protect my avionics, but I do not want to have any further bad experiences. I'd like to see your wiring diagram. Suggest you compare what you've done with Figure Z-16 of the AeroElectric Connection. Rotax is not known for their critical understanding of electrical systems. I should be most grateful if you would give me your advice on fitting another crowbar unit plus c.b. and relay and also whether or not you consider I should replace the regulator, so as to avoid future problems. If you would like to see my circuit diagrams, I could fax them to you if you could e-mail your fax number. I am afraid I do not have a scanner. You can fax a copy to 316.685.8617 Bob . . . ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: LEDs
Date: Feb 11, 2003
Cheers, There is one more consideration which builders may want to question: The angle of the display (azimuth?). I drilled a series of small holes in my innermost bulkheads and buried LEDs in them so that they would light up the darkest innards for repair or mod work. I neglected initially to check the angle at which the LED displays the light and so the first few are 'spots' where they should be 'floods' (yellow is a good substitute for white - less costly). I now plan using spots (10deg or less) for red instruments, one per dial, and flood whites for general cockpit area and dark corners. These 'spots' are also great for bedlights when one wants to read without flooding the partner. I got one wall insertion down to lighting just the page........ So consider lighting angle when you shop.......... Ferg Europa A064 ________________________________________________________________________________
From: "Doug Lawton" <skyrider2(at)earthlink.net>
Subject: Re: AeroElectric-List Digest: 17 Msgs - 02/10/03
Date: Feb 11, 2003
Bob, Just curious, is your website's order taking capability a secure transaction? It doesn't look to be so. I'd like to order a copy of the book, but I'm not in favor of insecure transactions over the internet. I tried calling your phone number to relay credit card information and got the fax. Just starting on the planning stages of my electrical system and need all the help I can get...... Doug Lawton Europa Mono-Motorglider A244 ________________________________________________________________________________
From: "Rob Housman" <RobH@hyperion-ef.com>
Subject: re: Crowbar Device
Date: Feb 11, 2003
...but you DO have a scanner. If you have a fax machine (as you say) and you have a PC (obviously, since you are on line) with a modem (and fax software), all you need to do is fax the document to your PC, and you have a scanned document. You do need two separate phone lines, one for each device. Best regards, Rob Housman Europa XS Tri-Gear A070 Airfarame complete Irvine, CA -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Robert L. Nuckolls, III Subject: AeroElectric-List: re: Crowbar Device I am afraid I do not have a scanner. You can fax a copy to 316.685.8617 Bob . . . ________________________________________________________________________________
From: "Steve Richard" <steve(at)oasissolutions.com>
Subject: solenoid
Date: Feb 11, 2003
I'm planning on mounting my oxygen tank in the rear of the plane. The tank has a simple lever actuated valve for opening and closing. I could run a cable to open and close, but I would rather have it done electrically. I'm looking for a solenoid with some special talents. I want it to stay in position even if power is lost. Has anyone seen such a device? Any and all suggestions taken. Steve Richard steve(at)oasissolutions.com ________________________________________________________________________________
Date: Feb 11, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Starter solenoid
> >Hello Bob and friends, > >There's nothing better than a simple experiment to >lighten up. Today, I wanted to know how much current >my starter solenoid was draining... I remember reading >Bob's article, but I suppose I did not understand it >and decided not to use an external starter contactor. >Now I understand that peak current thing Bob explains >and I can see how it would make a switch work >harder... I modified my drawing to include a starter >contactor. :-) > >Michel Repeatable results are the foundation upon which real science and understanding are based . . . good work. Bob . . . ________________________________________________________________________________
From: CozyGirrrl(at)aol.com
Date: Feb 11, 2003
Subject: Re: solenoid
In a message dated 2/11/2003 11:42:46 AM Central Standard Time, steve(at)oasissolutions.com writes: > > I'm planning on mounting my oxygen tank in the rear of the plane. The tank > has a simple lever actuated valve for opening and closing. I could run a > cable to open and close, but I would rather have it done electrically. I'm > looking for a solenoid with some special talents. I want it to stay in > position even if power is lost. Has anyone seen such a device? Any and > all > suggestions taken. > > Steve Richard > steve(at)oasissolutions.com Steve, I'm sure there are solenoid valves that move a piston one way then another, my concern with your plan would be in the event you lost all power, you still need a means of shutting off the bottle if you were going down. Oxygen could be just as bad as a fuel leak. ...Chrissi ________________________________________________________________________________
Date: Feb 11, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Secure site?
> > >Bob, > >Just curious, is your website's order taking capability a secure >transaction? It doesn't look to be so. No. The costs of secure website software adds only a modicum of safety to an issue that is hundreds of times wider than encrypted transfers from your browser to my server . . . I've determined that the whole "secure server" thing is bogus and I elected not to load my customers with essentially worthless overhead. >I'd like to order a copy of the book, but I'm not in favor of insecure >transactions over the internet. I tried calling your phone number to relay >credit card information and got the fax. If I'm in the office, I pick up in 4 rings or less. Otherwise you get the fax. You could fax your order in. >Just starting on the planning stages of my electrical system and need all >the help I can get...... B&C stocks the book too . . . you can call them during your order. Call 316.283.8000 Thanks! Bob . . . |---------------------------------------------------| | A lie can travel half way around the world while | | the truth is till putting on its shoes . . . | | -Mark Twain- | |---------------------------------------------------| ________________________________________________________________________________
Date: Feb 11, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: solenoid
> >In a message dated 2/11/2003 11:42:46 AM Central Standard Time, >steve(at)oasissolutions.com writes: > > > > > > I'm planning on mounting my oxygen tank in the rear of the plane. The tank > > has a simple lever actuated valve for opening and closing. I could run a > > cable to open and close, but I would rather have it done electrically. I'm > > looking for a solenoid with some special talents. I want it to stay in > > position even if power is lost. Has anyone seen such a device? Any and > > all > > suggestions taken. > > > > Steve Richard > > steve(at)oasissolutions.com > >Steve, I'm sure there are solenoid valves that move a piston one way then >another, my concern with your plan would be in the event you lost all power, >you still need a means of shutting off the bottle if you were going down. >Oxygen could be just as bad as a fuel leak. If you're planning to architecture and maintain the airplane so as to ALWAYS have power, then what you're looking for is a motor driven valve. You may be able to adapt a MAC trim servo to the task. This would get you an off-the-shelf gear box, actuation mechanism, and limit switches. There may be other options in the form of DC motor/gearbox combinations that would facilitate the design. Can you get some torque measurements on the valve to help size the task? Bob . . . ________________________________________________________________________________
From: "Huw & Rachel" <huwrachel(at)earthlink.net>
Subject: EXPBUS
Date: Feb 11, 2003
> >In a message dated 2/5/2003 4:20:50 PM Eastern Standard Time, >owner-aeroelectric-list-server(at)matronics.com writes: > > > Still, I'm leaning towards the EXPBUS - as it must be the simplest and most > > well arranged system for the homebuilder. So - to all who has been there, > > done that: what's your experience/advice?? >> > If for no other reasons: > > (1) The EXPbus may or may not have all the circuit features > you need. What you see is what you get for now and > in the future. > > (2) The EXPbus is warmed-over 1960's certifie-iron architecture. > > (3) For what the EXPbus costs, we can buy all the circuit > protection, switches, terminals, wire, contactors and > installation supplies to do any of the Z-figures or > a variation thereof) and have money left over. > > Bob . . . > Bob Sorry, this is a long post, but, I need to get it off my chest somewhere, and this seems like the best place. I just wish I had the knowledge to put together an alternative to the EXPBUS using standard components. For modern engines a continuous supply of electricity is necessary for powered flight. We are installing an Eggenfellner Subaru in a Glastar and the package comes with a very comprehensive Installation Manual. The EXPBUS is so highly recommended for the Egg Sub installation that to go another route requires factory approval or it may invalidate the warranty. As far as I can make out, what the EXPBUS does for us is: 1 Provide Master Electrical Switch 2. Provide Alternator Field switch 3. Continuously monitors both batteries and picks the one with the greatest output - so giving automatic switching between batteries. 4. Monitors high and low voltage situations 5. Provides warm up circuits for lamps 6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, 11 amp. 7. Protects avionics at start up 8. Provide Keep Alive circuits There is a lot that the EXPBUS does not do and all of that is explained very well in the Installation Manual. I just wish that someone could lead me by the hand to circuits designs and components that would replace the EXPBUS. What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : "Although the EXPBUS provides the majority of your secondary circuit protection, several conventional circuit breakers and fuses will be required to complete your installation. These should be Klixon, Potter & Brumfield, or equivalent button type breakers." Additional circuit breakers include: 1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if desired) 2. 50A - Alternator to EXPBUS 3. 20A - Aux Battery to Bus Master switch 4. 10A - Starter Solenoid and Optional Cabin Heater 5. 10A - Optional Pitot Heater and/or Optional Cabin Heater Additional fuses include: 1. 10A - ATO Type - Main Fuel Pump 2. 10A - ATO Type - Aux Fuel Pump 3. 5A - ATO Type - Auto-Failover circuit and additional critical equipment. 4. 3A - ATO Type - Backup Gyro The 60A Main Battery circuit breaker is used to isolate the Main Battery in the event of a serious primary circuit short. Isolating the Main Battery could potentially offer additional emergency flight time when running off the Aux Battery by engaging the Aux Boost switch to cross-connect the two batteries. Fuses 1 through 4 are ATO Type fuses. These are common automotive "blade" type fuses and can share a quad fuse block. The purpose of the 10A Fuel Pump fuses is to provide a protective device which will blow slightly before the EXPBUS protection (11A) will trip. This allows other equipment which is using the EXPBUS circuits to continue to operate in the event of a shorted fuel pump circuit. " Any help would be much appreciated. from Huw & Rachel Williams huwrachel(at)earthlink.net ________________________________________________________________________________
Date: Feb 11, 2003
Subject: Re: EXPBUS
From: "Matt Prather" <mprather(at)spro.net>
> > > Bob > > Sorry, this is a long post, but, I need to get it off my chest ... > The EXPBUS is so highly recommended for the Egg Sub installation that to > go another route requires factory approval or it may invalidate the > warranty. Any idea whether Egg is in cahoots with Expbus? This kind of thing makes me wonder. None the less, if Egg is honest, I think they would recognize the robustness of the Aeroelectric inspired designs, and approval should be easy. > > As far as I can make out, what the EXPBUS does for us is: > 1 Provide Master Electrical Switch > 2. Provide Alternator Field switch > 3. Continuously monitors both batteries and picks the one with the > greatest output - so giving automatic switching between batteries. > 4. Monitors high and low voltage situations > 5. Provides warm up circuits for lamps > 6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, > 11 amp. > 7. Protects avionics at start up > 8. Provide Keep Alive circuits > I kind of liken this list of capabilities to Sears selling a machine that washes clothes, dishes, is a cd player and cooks for you you. And, you have to pay more because all of the capabilities are installed in one box (for 'convenience'). Those are all things that we like to have (maybe even need), but it may be inconvenient and impractical (and maybe less safe) to have them all located in the kitchen. It really doesn't make sense to pay extra for them either. If you think about the above list, its pretty short. > > There is a lot that the EXPBUS does not do and all of that is explained > very well in the Installation Manual. I just wish that someone could > lead me by the hand to circuits designs and components that would > replace the EXPBUS. > > What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : > > "Although the EXPBUS provides the majority of your secondary circuit > protection, several conventional circuit breakers and fuses will be > required to complete your installation. These should be Klixon, Potter & > Brumfield, or equivalent button type breakers." > > Additional circuit breakers include: > 1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if > desired) 2. 50A - Alternator to EXPBUS > 3. 20A - Aux Battery to Bus Master switch > 4. 10A - Starter Solenoid and Optional Cabin Heater > 5. 10A - Optional Pitot Heater and/or Optional Cabin Heater > Additional fuses include: > 1. 10A - ATO Type - Main Fuel Pump > 2. 10A - ATO Type - Aux Fuel Pump > 3. 5A - ATO Type - Auto-Failover circuit and additional critical > equipment. 4. 3A - ATO Type - Backup Gyro > If you duplicated a few of the items on the not-included list (add a couple of breakers/fuses for other electricals in the airplane), you would have to add only a couple of extra components (a few switches, a couple of contactors, a diode bridge, some heat-shrink) to completely replace the ExpBus with a more modular, custom designed system. I suspect that in the end, you are going to end up spending enough time studying your electrical system that you would have been able to understand it without the Expbus. At that point, if you have some kind of anomally, you have a clue about where it might be coming from. Hmm.... > > from > Huw & Rachel Williams > huwrachel(at)earthlink.net > Regards, Matt Prather ________________________________________________________________________________
Date: Feb 11, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: EXPBUS
> > >Bob > >Sorry, this is a long post, but, I need to get it off my chest somewhere, >and this seems like the best place. Yup . . . that's what we're all here for . . . >I just wish I had the knowledge to put together an alternative to the EXPBUS >using standard components. So did we all face a similar challenge at some point in the past . . . >For modern engines a continuous supply of electricity is necessary for >powered flight. We are installing an Eggenfellner Subaru in a Glastar and >the package comes with a very comprehensive Installation Manual. >The EXPBUS is so highly recommended for the Egg Sub installation that to go >another route requires factory approval or it may invalidate the warranty. I'm mystified as to why this should be so. But let's see what the requirements really are and then see if the EXPBUS offers some kind of magic that cannot be duplicated or replaced. >As far as I can make out, what the EXPBUS does for us is: >1 Provide Master Electrical Switch >2. Provide Alternator Field switch >3. Continuously monitors both batteries and picks the one with the greatest >output - so giving automatic switching between batteries. >4. Monitors high and low voltage situations >5. Provides warm up circuits for lamps >6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, 11 >amp. >7. Protects avionics at start up >8. Provide Keep Alive circuits > > >There is a lot that the EXPBUS does not do and all of that is explained very >well in the Installation Manual. I just wish that someone could lead me by >the hand to circuits designs and components that would replace the EXPBUS. > >What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : Exactly what I was eluding to earlier . . . the cookie cutter approach falls short in some ways . . . >"Although the EXPBUS provides the majority of your secondary circuit >protection, several conventional circuit breakers and fuses will be required >to complete your installation. These should be Klixon, Potter & Brumfield, >or equivalent button type breakers." > >Additional circuit breakers include: >1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if >desired) >2. 50A - Alternator to EXPBUS >3. 20A - Aux Battery to Bus Master switch >4. 10A - Starter Solenoid and Optional Cabin Heater >5. 10A - Optional Pitot Heater and/or Optional Cabin Heater >Additional fuses include: >1. 10A - ATO Type - Main Fuel Pump >2. 10A - ATO Type - Aux Fuel Pump >3. 5A - ATO Type - Auto-Failover circuit and additional critical >equipment. >4. 3A - ATO Type - Backup Gyro > >The 60A Main Battery circuit breaker is used to isolate the Main Battery in >the event of a serious primary circuit short. Isolating the Main Battery >could potentially offer additional emergency flight time when running off >the Aux Battery by engaging the Aux Boost switch to cross-connect the two >batteries. > >Fuses 1 through 4 are ATO Type fuses. These are common automotive "blade" >type fuses and can share a quad fuse block. The purpose of the 10A Fuel >Pump fuses is to provide a protective device which will blow slightly before >the EXPBUS protection (11A) will trip. This allows other equipment which is >using the EXPBUS circuits to continue to operate in the event of a shorted >fuel pump circuit. It's been a goal of the AeroElectric Connection (and I hope for those who participate on this list) to figure out ways to meet electrical operational needs of ANY collection of airborne hardware. The suite of architectures published in Appendix Z of the book evolved as solutions to a variety of unique requirements. All of them fabricated with simple, off-the-shelf components. There is no reason why we cannot modify one of the existing architectures as needed to satisfy your anticipated system needs along with some you may not have anticipated. To start with, how about sending me copies of the pertinent pages from the manual so I can familiarize myself with any special requirements for this engine. Bob . . . 6936 Bainbridge Road Wichita, KS 67226-1008 ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: EXPBUS
Date: Feb 11, 2003
Why would one wonder if they are in "cahoots"? I think we can discuss this without such implication. The EXPBUS was developed some time ago with a particular purpose in mind from a particular design perspective. I think it serves the purposes the designers intended. We may argue that those are not our purposes or that it does not serve our purposes as well as a more recently (or thoroughly) thought through design. That is not only fair but healthy to think through. It appears to me that the Eggenfellner people probably saw it as a tool that would get them part the way there in a manner that they were comfortable with for THEIR ENGINE INSTALLATION at the time they needed something. Now maybe if they had time, insight or money they could have gotten Bob (or some wise soul from this list) to do a better design (and maybe some day, if such is presented, they will adopt same) ... but they don't have to be in "cahoots" to have used the EXPBUS. James EXPBUS ...chosen for one RV project AeroElectric Way ... chosen for another ... different strokes for different projects > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Matt > Prather > Sent: Tuesday, February 11, 2003 7:28 PM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: EXPBUS > > > > > > > > > > > Bob > > > > Sorry, this is a long post, but, I need to get it off my chest > ... > > The EXPBUS is so highly recommended for the Egg Sub installation that to > > go another route requires factory approval or it may invalidate the > > warranty. > > > Any idea whether Egg is in cahoots with Expbus? This kind of thing > makes me wonder. None the less, if Egg is honest, I think they would > recognize the robustness of the Aeroelectric inspired designs, and > approval should be easy. > > > > > > As far as I can make out, what the EXPBUS does for us is: > > 1 Provide Master Electrical Switch > > 2. Provide Alternator Field switch > > 3. Continuously monitors both batteries and picks the one with the > > greatest output - so giving automatic switching between batteries. > > 4. Monitors high and low voltage situations > > 5. Provides warm up circuits for lamps > > 6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, > > 11 amp. > > 7. Protects avionics at start up > > 8. Provide Keep Alive circuits > > > > I kind of liken this list of capabilities to Sears selling a machine that > washes clothes, dishes, is a cd player and cooks for you you. And, > you have to pay more because all of the capabilities are installed in > one box (for 'convenience'). Those are all things that we like to have > (maybe even need), but it may be inconvenient and impractical (and > maybe less safe) to have them all located in the kitchen. It really > doesn't make sense to pay extra for them either. > > If you think about the above list, its pretty short. > > > > > There is a lot that the EXPBUS does not do and all of that is explained > > very well in the Installation Manual. I just wish that someone could > > lead me by the hand to circuits designs and components that would > > replace the EXPBUS. > > > > What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : > > > > "Although the EXPBUS provides the majority of your secondary circuit > > protection, several conventional circuit breakers and fuses will be > > required to complete your installation. These should be Klixon, Potter & > > Brumfield, or equivalent button type breakers." > > > > Additional circuit breakers include: > > 1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if > > desired) 2. 50A - Alternator to EXPBUS > > 3. 20A - Aux Battery to Bus Master switch > > 4. 10A - Starter Solenoid and Optional Cabin Heater > > 5. 10A - Optional Pitot Heater and/or Optional Cabin Heater > > Additional fuses include: > > 1. 10A - ATO Type - Main Fuel Pump > > 2. 10A - ATO Type - Aux Fuel Pump > > 3. 5A - ATO Type - Auto-Failover circuit and additional critical > > equipment. 4. 3A - ATO Type - Backup Gyro > > > > If you duplicated a few of the items on the not-included list (add a > couple of > breakers/fuses for other electricals in the airplane), you would have to > add only > a couple of extra components (a few switches, a couple of > contactors, a diode > bridge, some heat-shrink) to completely replace the ExpBus with a more > modular, custom designed system. I suspect that in the end, you > are going to > end up spending enough time studying your electrical system that you would > have been able to understand it without the Expbus. At that point, if you > have > some kind of anomally, you have a clue about where it might be > coming from. > Hmm.... > > > > > from > > Huw & Rachel Williams > > huwrachel(at)earthlink.net > > > > Regards, > > Matt Prather > > ________________________________________________________________________________
From: "Paul McAllister" <paul.mcallister(at)qia.net>
Subject: Re: re: Crowbar Device
Date: Feb 11, 2003
Bob, > The multi-meter recorded voltages of 35 to 40 volts depending on > rpm, so I shut down the engine. I am a Europa builder and I intend to fit a 912S. I am curious to see the report of over voltages this high. I was under the impression that the permanment magnet alternator did not have enough "grunt" to generate a significant overvoltage when a battery is connected to the system. Am I mistaken in this assumption and should I seriously consider installing a crowbar protection device ? Paul ________________________________________________________________________________
Date: Feb 11, 2003
From: Matt Prather <mprather(at)spro.net>
Subject: Re: EXPBUS
I would wonder because it was stated that Eggenfellner might not honor the warrantee on their product should it be installed without the purchase of companion products. None the less, I chose my wording poorly, and admit that for me to suggest that Control Vision or Eggenfellner might be involved in dishonest business dealings was foolish. I appologize for any angst I might have caused. Vendors of products designed for the custom aircraft market have enough roadblocks in the way of success and don't need people spreading baseless rumors or false accusations. I have heard good things of the Eggenfellner product and am personally excited about using a better engine than my old Continental. If these guys are doing it, good for them. As for the Exp Bus product, I haven't been able to understand its merits, though that doesn't demonstrate that it doesn't have any. I still stand by the ideal of education for the custom builder. I think we as a group should well understand the ins and outs of the systems that we install and use. I believe that it contributes to operational safety. If, after developing a clear understanding of the requirements of the electrical system on our aircraft the benefits of a particular product stand out over its weaknesses, then buy it and install it. Regards, Matt Prather N34RD James E. Clark wrote: > >Why would one wonder if they are in "cahoots"? > >I think we can discuss this without such implication. > >The EXPBUS was developed some time ago with a particular purpose in mind >from a particular design perspective. I think it serves the purposes the >designers intended. We may argue that those are not our purposes or that it >does not serve our purposes as well as a more recently (or thoroughly) >thought through design. That is not only fair but healthy to think through. > >It appears to me that the Eggenfellner people probably saw it as a tool that >would get them part the way there in a manner that they were comfortable >with for THEIR ENGINE INSTALLATION at the time they needed something. > >Now maybe if they had time, insight or money they could have gotten Bob (or >some wise soul from this list) to do a better design (and maybe some day, if >such is presented, they will adopt same) ... but they don't have to be in >"cahoots" to have used the EXPBUS. > > >James > >EXPBUS ...chosen for one RV project >AeroElectric Way ... chosen for another > >... different strokes for different projects > > >>-----Original Message----- >>From: owner-aeroelectric-list-server(at)matronics.com >>[mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Matt >>Prather >>Sent: Tuesday, February 11, 2003 7:28 PM >>To: aeroelectric-list(at)matronics.com >>Subject: Re: AeroElectric-List: EXPBUS >> >> >> >> >>> >>> >>>Bob >>> >>>Sorry, this is a long post, but, I need to get it off my chest >>> >>... >> >>>The EXPBUS is so highly recommended for the Egg Sub installation that to >>>go another route requires factory approval or it may invalidate the >>>warranty. >>> >> >>Any idea whether Egg is in cahoots with Expbus? This kind of thing >>makes me wonder. None the less, if Egg is honest, I think they would >>recognize the robustness of the Aeroelectric inspired designs, and >>approval should be easy. >> >> >>>As far as I can make out, what the EXPBUS does for us is: >>>1 Provide Master Electrical Switch >>>2. Provide Alternator Field switch >>>3. Continuously monitors both batteries and picks the one with the >>>greatest output - so giving automatic switching between batteries. >>>4. Monitors high and low voltage situations >>>5. Provides warm up circuits for lamps >>>6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, >>>11 amp. >>>7. Protects avionics at start up >>>8. Provide Keep Alive circuits >>> >>I kind of liken this list of capabilities to Sears selling a machine that >>washes clothes, dishes, is a cd player and cooks for you you. And, >>you have to pay more because all of the capabilities are installed in >>one box (for 'convenience'). Those are all things that we like to have >>(maybe even need), but it may be inconvenient and impractical (and >>maybe less safe) to have them all located in the kitchen. It really >>doesn't make sense to pay extra for them either. >> >>If you think about the above list, its pretty short. >> >>>There is a lot that the EXPBUS does not do and all of that is explained >>>very well in the Installation Manual. I just wish that someone could >>>lead me by the hand to circuits designs and components that would >>>replace the EXPBUS. >>> >>>What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : >>> >>>"Although the EXPBUS provides the majority of your secondary circuit >>>protection, several conventional circuit breakers and fuses will be >>>required to complete your installation. These should be Klixon, Potter & >>>Brumfield, or equivalent button type breakers." >>> >>>Additional circuit breakers include: >>>1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if >>>desired) 2. 50A - Alternator to EXPBUS >>>3. 20A - Aux Battery to Bus Master switch >>>4. 10A - Starter Solenoid and Optional Cabin Heater >>>5. 10A - Optional Pitot Heater and/or Optional Cabin Heater >>>Additional fuses include: >>>1. 10A - ATO Type - Main Fuel Pump >>>2. 10A - ATO Type - Aux Fuel Pump >>>3. 5A - ATO Type - Auto-Failover circuit and additional critical >>>equipment. 4. 3A - ATO Type - Backup Gyro >>> >>If you duplicated a few of the items on the not-included list (add a >>couple of >>breakers/fuses for other electricals in the airplane), you would have to >>add only >>a couple of extra components (a few switches, a couple of >>contactors, a diode >>bridge, some heat-shrink) to completely replace the ExpBus with a more >>modular, custom designed system. I suspect that in the end, you >>are going to >>end up spending enough time studying your electrical system that you would >>have been able to understand it without the Expbus. At that point, if you >>have >>some kind of anomally, you have a clue about where it might be >>coming from. >>Hmm.... >> >>>from >>>Huw & Rachel Williams >>>huwrachel(at)earthlink.net >>> >>Regards, >> >>Matt Prather >> >> > > ________________________________________________________________________________
Date: Feb 11, 2003
From: Mark Phillips <ripsteel(at)edge.net>
Subject: Re: EXPBUS
FWIW, the primary and MOST SIGNIFICANT reason to roll your own electrical system, preferably utilizing the long and hard learned lessons offered by Bob Nuckolls, is simply this: If you build it yourself, you must understand what you are doing, and you will be intimately familiar with the thing in its entirety. Therefore, if for some reason it DOESN'T perform as expected, takes a crap in the least desirable of times and places, or wants modifying at a later date, you, its creator, will be fully capable of dealing with it. If something on that board decides to go south and you are in East Bumflock, what are your alternatives? From The PossumWorks in TN Mark Phillips RV-6A - "almost" ready to order wires & stuff... > > Sorry, this is a long post, but, I need to get it off my chest somewhere, > and this seems like the best place. ________________________________________________________________________________
Date: Feb 11, 2003
From: Jim and Lucy <jpollard(at)mnsi.net>
Subject: Re: Starter solenoid
I think I must be missing something about the starter solenoid. After reading about it in the Connection and on the emails the only reason I have read not to use it is that it is hard on the starter switch. Would it not be easier just to get a better switch that can handle this? I have a lucas keyswitch on one machine that easily have 10000 start cycles on it from 35 years of use. Also there is about 20 different pieces of machinery around here and none of them have starter contactors except for a 30 year old ford dumptruck and another large motor with a 24 volt starter with a series parallel contactor (12 volt system with 24 volt starter) There is the question of the starter sticking but that can be taken care of by shutting of the master switch. Is the problem something to do with running all that power through the main buss?? I will be hooking up the starter soon like what Michel just talked about. It is a little bitty subaru starter. Got me wondering anyway Thanks Jim Pollard Merlin Ont ch601hds ea-81 ________________________________________________________________________________
Date: Feb 11, 2003
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Starter solenoid
What I'm thinking about Jim is to reduce the size of one fuse from the battery bus (in the back). Bob advises that the circuits from the BBus should be of 5A or less. Since I use an ignition key, I have one circuit that will drive the ignition 1 as well as the starter solenoid. One of my friends who use an ignition key in the same way determined that he needed a 10A fuse to accomodate the starting of the engine and the ignition together. Using the contactor will enable reducing this fuse to a 5A one. It will also simplify the wiring to the starter in the engine compartment. My batteries are in the back and the alternator B-Lead is to be connected to the starter (where the battery cables reach in the front). With the "Start" wire, that makes three wires going to the front of the engine. The contactor will enable routing a single wire (4AWG in my case) instead of the three. Michel --- Jim and Lucy wrote: > Lucy > > I think I must be missing something about the > starter > solenoid. After reading about it in the Connection > and > on the emails the only reason I have read not to use > it > is that it is hard on the starter switch. > > Would it not be easier just to get a better switch > that > can handle this? I have a lucas keyswitch on one > machine that easily have 10000 start cycles on it > from 35 years of use. > Also there is about 20 different pieces of machinery > around here and none of them have starter contactors > except for a 30 year old ford dumptruck and another > large motor with a 24 volt starter with a series > parallel > contactor (12 volt system with 24 volt starter) > > There is the question of the starter sticking but > that > can be taken care of by shutting of the master > switch. > > Is the problem something to do with running all that > power through the main buss?? > > I will be hooking up the starter soon like what > Michel > just talked about. It is a little bitty subaru > starter. > > Got me wondering anyway > > Thanks > > Jim Pollard > Merlin Ont > ch601hds > ea-81 > ===== ---------------------------- Michel Therrien CH601-HD http://mthobby.pcperfect.com/ch601 http://www.zenithair.com/bldrlist/profiles/mthobby http://pages.infinit.net/mthobby ________________________________________________________________________________
From: "James E. Clark" <jclark(at)conterra.com>
Subject: EXPBUS
Date: Feb 12, 2003
Good post. I, for one, applaud your response. Comments below. > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Matt > Prather > Sent: Tuesday, February 11, 2003 9:31 PM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: EXPBUS > > > I would wonder because it was stated that Eggenfellner might not > honor the warrantee on their product should it be installed without > the purchase of companion products. > I don't know, but I would think they are trying to minimize the number of variables at this point. There are probably a lot of people out there who have never heard of this list or read Bob's book but who are thinking about "tinkering" with the electrical design. This is what we do but I can see them having some concern in the early days of a new engine project. The Lycomings have had dozens of years for tinkering so people may not be as concerned. > None the less, I chose my wording poorly, and admit that for me to > suggest that Control Vision or Eggenfellner might be involved in > dishonest business dealings was foolish. I appologize for any angst I > might have caused. Vendors of products designed for the custom > aircraft market have enough roadblocks in the way of success and > don't need people spreading baseless rumors or false accusations. > We all make such mistakes. You put it quite well and summed up my reason for responding. > I have heard good things of the Eggenfellner product and am personally > excited about using a better engine than my old Continental. If these > guys are doing it, good for them. > Yes. > As for the Exp Bus product, I haven't been able to understand its merits, > though that doesn't demonstrate that it doesn't have any. > > I still stand by the ideal of education for the custom builder. > I think we > as a group should well understand the ins and outs of the systems that > we install and use. I believe that it contributes to operational > safety. If, > after developing a clear understanding of the requirements of the > electrical > system on our aircraft the benefits of a particular product stand out over > its weaknesses, then buy it and install it. > Yes you are most correct. I "evaluated" the EXPBUS for use for a particular situation and concluded it was fine for the chosen application. Maybe after I have done "Z-14" (or thereabouts) I will conclude that I could have come up with a better approach. I did though go in with eyes wide open and so far have been happy. James > Regards, > > Matt Prather > N34RD > > > James E. Clark wrote: > > > > > >Why would one wonder if they are in "cahoots"? > > > >I think we can discuss this without such implication. > > > >The EXPBUS was developed some time ago with a particular purpose in mind > >from a particular design perspective. I think it serves the purposes the > >designers intended. We may argue that those are not our purposes > or that it > >does not serve our purposes as well as a more recently (or thoroughly) > >thought through design. That is not only fair but healthy to > think through. > > > >It appears to me that the Eggenfellner people probably saw it as > a tool that > >would get them part the way there in a manner that they were comfortable > >with for THEIR ENGINE INSTALLATION at the time they needed something. > > > >Now maybe if they had time, insight or money they could have > gotten Bob (or > >some wise soul from this list) to do a better design (and maybe > some day, if > >such is presented, they will adopt same) ... but they don't have to be in > >"cahoots" to have used the EXPBUS. > > > > > >James > > > >EXPBUS ...chosen for one RV project > >AeroElectric Way ... chosen for another > > > >... different strokes for different projects > > > > > >>-----Original Message----- > >>From: owner-aeroelectric-list-server(at)matronics.com > >>[mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Matt > >>Prather > >>Sent: Tuesday, February 11, 2003 7:28 PM > >>To: aeroelectric-list(at)matronics.com > >>Subject: Re: AeroElectric-List: EXPBUS > >> > >> > >> > >> > >>> > >>> > >>>Bob > >>> > >>>Sorry, this is a long post, but, I need to get it off my chest > >>> > >>... > >> > >>>The EXPBUS is so highly recommended for the Egg Sub > installation that to > >>>go another route requires factory approval or it may invalidate the > >>>warranty. > >>> > >> > >>Any idea whether Egg is in cahoots with Expbus? This kind of thing > >>makes me wonder. None the less, if Egg is honest, I think they would > >>recognize the robustness of the Aeroelectric inspired designs, and > >>approval should be easy. > >> > >> > >>>As far as I can make out, what the EXPBUS does for us is: > >>>1 Provide Master Electrical Switch > >>>2. Provide Alternator Field switch > >>>3. Continuously monitors both batteries and picks the one with the > >>>greatest output - so giving automatic switching between batteries. > >>>4. Monitors high and low voltage situations > >>>5. Provides warm up circuits for lamps > >>>6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, > >>>11 amp. > >>>7. Protects avionics at start up > >>>8. Provide Keep Alive circuits > >>> > >>I kind of liken this list of capabilities to Sears selling a > machine that > >>washes clothes, dishes, is a cd player and cooks for you you. And, > >>you have to pay more because all of the capabilities are installed in > >>one box (for 'convenience'). Those are all things that we like to have > >>(maybe even need), but it may be inconvenient and impractical (and > >>maybe less safe) to have them all located in the kitchen. It really > >>doesn't make sense to pay extra for them either. > >> > >>If you think about the above list, its pretty short. > >> > >>>There is a lot that the EXPBUS does not do and all of that is explained > >>>very well in the Installation Manual. I just wish that someone could > >>>lead me by the hand to circuits designs and components that would > >>>replace the EXPBUS. > >>> > >>>What the EXPBUS does not do, (quoting from the Eggenfellner > Manual) is : > >>> > >>>"Although the EXPBUS provides the majority of your secondary circuit > >>>protection, several conventional circuit breakers and fuses will be > >>>required to complete your installation. These should be > Klixon, Potter & > >>>Brumfield, or equivalent button type breakers." > >>> > >>>Additional circuit breakers include: > >>>1. 60A - Main Battery to EXPBUS (May also use an > ANL-Type fuse if > >>>desired) 2. 50A - Alternator to EXPBUS > >>>3. 20A - Aux Battery to Bus Master switch > >>>4. 10A - Starter Solenoid and Optional Cabin Heater > >>>5. 10A - Optional Pitot Heater and/or Optional Cabin Heater > >>>Additional fuses include: > >>>1. 10A - ATO Type - Main Fuel Pump > >>>2. 10A - ATO Type - Aux Fuel Pump > >>>3. 5A - ATO Type - Auto-Failover circuit and additional critical > >>>equipment. 4. 3A - ATO Type - Backup Gyro > >>> > >>If you duplicated a few of the items on the not-included list (add a > >>couple of > >>breakers/fuses for other electricals in the airplane), you would have to > >>add only > >>a couple of extra components (a few switches, a couple of > >>contactors, a diode > >>bridge, some heat-shrink) to completely replace the ExpBus with a more > >>modular, custom designed system. I suspect that in the end, you > >>are going to > >>end up spending enough time studying your electrical system > that you would > >>have been able to understand it without the Expbus. At that > point, if you > >>have > >>some kind of anomally, you have a clue about where it might be > >>coming from. > >>Hmm.... > >> > >>>from > >>>Huw & Rachel Williams > >>>huwrachel(at)earthlink.net > >>> > >>Regards, > >> > >>Matt Prather > >> > >> > > > > > > ________________________________________________________________________________
From: "Gary Casey" <glcasey(at)adelphia.net>
Subject:
Date: Feb 12, 2003
<> How about a door lock actuator from almost any late model car? They are small electric motor powered devices that will go to either position and stop. Much lighter than a solenoid that would have the same force and travel. Gary Casey ________________________________________________________________________________
Date: Feb 11, 2003
Subject: Wire gage
From: cecilth(at)juno.com
I am purchasing wire to wire the panel of my RV6A. Am I correct that 95% of the job can be done with 16 gage wire? CH ________________________________________________________________________________
From: John Schroeder <jschroeder(at)perigee.net>
Date: Feb 12, 2003
Subject: Re: Wire gage
I believe Bob said that 90% can be done with AWG 20. John 2/11/2003 10:35:05 AM, cecilth(at)juno.com wrote: > > >I am purchasing wire to wire the panel of my RV6A. Am I correct that 95% >of the job can be done with 16 gage wire? >CH > ________________________________________________________________________________
Date: Feb 12, 2003
From: "William Yamokoski" <yamokosk(at)lmc.cc.mi.us>
Subject: Re: EXPBUS
Just wanted to add my two cents on this. I have a Glastar with the Egfgenfellner package. I do not use the EXPBUS. It was quite easy to adapt one of Bob's drawings to accomodate the all-electric, fuel-injected engine's needs. One of the goals that Jan Eggenfellner has espoused is to offer a very complete package....something that really appealed to this novice. As such, he sees an advantage to having all of his customers using the same parts, be it electrical or plumbing or whatever. Makes his job of supporting his customers less complicated. I haven't been a particitant in his user's group for a while, but when I was there he never discouraged the use of alternative electrical approaches. He just re-iterated that he couldn't (and shouldn't) answer too many questions on systems he didn't design. Maybe that has changed in the past few weeks...I don't know. As to the warranty, isn't just about every warranty filled with loopholes if you alter the product in any way? Bill Yamokoski very happy with my non-EXPBUS Glastar >>> huwrachel(at)earthlink.net 02/11/03 19:12 PM >>> > >In a message dated 2/5/2003 4:20:50 PM Eastern Standard Time, >owner-aeroelectric-list-server(at)matronics.com writes: > > > Still, I'm leaning towards the EXPBUS - as it must be the simplest and most > > well arranged system for the homebuilder. So - to all who has been there, > > done that: what's your experience/advice?? >> > If for no other reasons: > > (1) The EXPbus may or may not have all the circuit features > you need. What you see is what you get for now and > in the future. > > (2) The EXPbus is warmed-over 1960's certifie-iron architecture. > > (3) For what the EXPbus costs, we can buy all the circuit > protection, switches, terminals, wire, contactors and > installation supplies to do any of the Z-figures or > a variation thereof) and have money left over. > > Bob . . . > Bob Sorry, this is a long post, but, I need to get it off my chest somewhere, and this seems like the best place. I just wish I had the knowledge to put together an alternative to the EXPBUS using standard components. For modern engines a continuous supply of electricity is necessary for powered flight. We are installing an Eggenfellner Subaru in a Glastar and the package comes with a very comprehensive Installation Manual. The EXPBUS is so highly recommended for the Egg Sub installation that to go another route requires factory approval or it may invalidate the warranty. As far as I can make out, what the EXPBUS does for us is: 1 Provide Master Electrical Switch 2. Provide Alternator Field switch 3. Continuously monitors both batteries and picks the one with the greatest output - so giving automatic switching between batteries. 4. Monitors high and low voltage situations 5. Provides warm up circuits for lamps 6. Provides fused supplies at various rates 3 amp, 5 amp, 7 amp, 9 amp, 11 amp. 7. Protects avionics at start up 8. Provide Keep Alive circuits There is a lot that the EXPBUS does not do and all of that is explained very well in the Installation Manual. I just wish that someone could lead me by the hand to circuits designs and components that would replace the EXPBUS. What the EXPBUS does not do, (quoting from the Eggenfellner Manual) is : "Although the EXPBUS provides the majority of your secondary circuit protection, several conventional circuit breakers and fuses will be required to complete your installation. These should be Klixon, Potter & Brumfield, or equivalent button type breakers." Additional circuit breakers include: 1. 60A - Main Battery to EXPBUS (May also use an ANL-Type fuse if desired) 2. 50A - Alternator to EXPBUS 3. 20A - Aux Battery to Bus Master switch 4. 10A - Starter Solenoid and Optional Cabin Heater 5. 10A - Optional Pitot Heater and/or Optional Cabin Heater Additional fuses include: 1. 10A - ATO Type - Main Fuel Pump 2. 10A - ATO Type - Aux Fuel Pump 3. 5A - ATO Type - Auto-Failover circuit and additional critical equipment. 4. 3A - ATO Type - Backup Gyro The 60A Main Battery circuit breaker is used to isolate the Main Battery in the event of a serious primary circuit short. Isolating the Main Battery could potentially offer additional emergency flight time when running off the Aux Battery by engaging the Aux Boost switch to cross-connect the two batteries. Fuses 1 through 4 are ATO Type fuses. These are common automotive "blade" type fuses and can share a quad fuse block. The purpose of the 10A Fuel Pump fuses is to provide a protective device which will blow slightly before the EXPBUS protection (11A) will trip. This allows other equipment which is using the EXPBUS circuits to continue to operate in the event of a shorted fuel pump circuit. " Any help would be much appreciated. from Huw & Rachel Williams huwrachel(at)earthlink.net ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Starter solenoid
> >I think I must be missing something about the starter >solenoid. After reading about it in the Connection and >on the emails the only reason I have read not to use it >is that it is hard on the starter switch. > >Would it not be easier just to get a better switch that >can handle this? I have a lucas keyswitch on one >machine that easily have 10000 start cycles on it >from 35 years of use. >Also there is about 20 different pieces of machinery >around here and none of them have starter contactors >except for a 30 year old ford dumptruck and another >large motor with a 24 volt starter with a series parallel >contactor (12 volt system with 24 volt starter. > >There is the question of the starter sticking but that >can be taken care of by shutting of the master switch. Not all starters use the two-stage engagement solenoid. The only ones I am aware of offered to aviation are the B&C and Skytec products . . . there are undoubtedly others but some may not use this technology. In particular, smaller starters using the inertial engagement (Bendix) technique for the pinion gear has no particular need of a robust solenoid. >Is the problem something to do with running all that >power through the main buss?? Close . . B&C suggests that wear and tear on the pinion and ring gears is minimized by providing the shortest, most energetic engagement of the mechanisms as practical. The high inrush current through the longer wires between starter solenoid and push-button worked against this . . . A secondary consideration was that B&C wanted their product to be a drop in replacement for the Prestolite Pig starters that did not have built in engagement solenoids. Soooo . . . by jumpering the solenoid terminal to the main power terminal, and suggesting the use of an external starter contactor, both conditions were satisfied. PM motor starters CANNOT be configured by simple jumpering Figure Z-22 in the 'Connection shows how an externally wired "boost" relay can be used to relieve the panel mounted controls of the high inrush current while providing positive control of the built in soleniod to prevent run-on engagement of the pinion gear after the start button is released. This same boost relay has been used with the B&C starters to (1) eliminate the larger, external starter contactor and (2) relieving the panel mounted controls of the high inrush and (3) keeping leadwires driving the solenoid short for best engagement performance. Bob . . . ________________________________________________________________________________
From: "Werner Schneider" <wernerschneider(at)compuserve.com>
Subject: Re: Wire gage
Date: Feb 12, 2003
I would say 70% AWG22, 20% AWG20 (behind the panel) Werner (still crimping) ----- Original Message ----- From: "John Schroeder" <jschroeder(at)perigee.net> Subject: Re: AeroElectric-List: Wire gage > > I believe Bob said that 90% can be done with AWG 20. > > John > > 2/11/2003 10:35:05 AM, cecilth(at)juno.com wrote: > > > > > > >I am purchasing wire to wire the panel of my RV6A. Am I correct that 95% > >of the job can be done with 16 gage wire? > >CH > > > > ________________________________________________________________________________
From: "Steve Richard" <steve(at)oasissolutions.com>
Subject: oxygen tank valve actuator
Date: Feb 12, 2003
MAC servo's, dual solenoids from McMasters, and a car lock. Thanks for all the great ideas! Steve Richard steve(at)oasissolutions.com ________________________________________________________________________________
From: N823ms(at)aol.com
Date: Feb 12, 2003
Subject: Re: Wire gage
John: I finally just begin to teach myself this turbocad until I acquire the AutoCAD LT. Took a few diagrams, cut and pasted the external power section on to Z-14. Seems to be OK. I am looking for the symbols that Bob had offered at one time. Do you know where they are? Ed Silvanic ________________________________________________________________________________
From: "Wayne Sweet" <wsweet(at)attbi.com>
Subject: Re: Starter solenoid
Date: Feb 12, 2003
I went through 3 standard Bendix starter solenoids in as many years. Don't know why the gear was stripping, since the engine/prop and all the accessories came off a Mooney M20B. Went to B&C stuff, starter, alternator, regulator, battery; for the last 9 years no( meaning zero, natta) trouble with any of the stuff. It spins my IO-360A1A every time, all the time. Am I an unpaid supporter of B you bet. Oh, BTW, got the tip about B his hangar is three down from mine). Wayne ----- Original Message ----- From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net> Subject: Re: AeroElectric-List: Starter solenoid > > > > >I think I must be missing something about the starter > >solenoid. After reading about it in the Connection and > >on the emails the only reason I have read not to use it > >is that it is hard on the starter switch. > > > >Would it not be easier just to get a better switch that > >can handle this? I have a lucas keyswitch on one > >machine that easily have 10000 start cycles on it > >from 35 years of use. > >Also there is about 20 different pieces of machinery > >around here and none of them have starter contactors > >except for a 30 year old ford dumptruck and another > >large motor with a 24 volt starter with a series parallel > >contactor (12 volt system with 24 volt starter. > > > >There is the question of the starter sticking but that > >can be taken care of by shutting of the master switch. > > Not all starters use the two-stage engagement solenoid. > The only ones I am aware of offered to aviation are > the B&C and Skytec products . . . there are undoubtedly > others but some may not use this technology. In particular, > smaller starters using the inertial engagement (Bendix) > technique for the pinion gear has no particular need > of a robust solenoid. > > > >Is the problem something to do with running all that > >power through the main buss?? > > Close . . B&C suggests that wear and tear > on the pinion and ring gears is minimized by > providing the shortest, most energetic engagement > of the mechanisms as practical. The high inrush > current through the longer wires between > starter solenoid and push-button worked against > this . . . > > A secondary consideration was that B&C wanted > their product to be a drop in replacement for > the Prestolite Pig starters that did not have > built in engagement solenoids. > > Soooo . . . by jumpering the solenoid terminal > to the main power terminal, and suggesting > the use of an external starter contactor, both > conditions were satisfied. > > PM motor starters CANNOT be configured by simple > jumpering Figure Z-22 in the 'Connection shows > how an externally wired "boost" relay can be used > to relieve the panel mounted controls of the high > inrush current while providing positive control > of the built in soleniod to prevent run-on engagement > of the pinion gear after the start button is released. > This same boost relay has been used with the B&C > starters to (1) eliminate the larger, external starter > contactor and (2) relieving the panel > mounted controls of the high inrush and (3) keeping > leadwires driving the solenoid short for best > engagement performance. > > Bob . . . > > ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Figure Z-14 and crossfeed contactor location
Hi Bob: I'm not sure this is the place to try to contact you but I'll try anyway. I'll also try signing up through the consulting web site. bob.nuckolls(at)cox.net is a better address. nuckolls(at)aeroelectric.com is so loaded with spam that my you are at risk of being missed. Also, I'll suggest you join the aeroelectric-list on matronics.com . . . these kinds of questions are best answered in an environment where lots of folks can share in the discussions and solutions. I attended your seminar in Racine, WI in the summer of 2001 and am building a two alternator, two battery Lancair Super ES. My electrical system uses your Fig Z-14 as a model. My main alternator is a 60 amp provided by Continental on my IO-550 engine. The no. 2 alt is a B&C 20 amp. I'm also using B&C voltage reg's, batt contactor, crossfeed contactor and starter contactor, etc. The distance from the aft mounted batteries to the firewall mounted starter contactor is 10.5 ft. Understand Questions: 1.Z-14 shows a 2AWG strap fro the Batt Contactor to the Crossfeed Contactor, implying [I think] a short distance between the two. Question: Given the distance between the battery cx and the firewall [10.5 ft] could the crossfeed cx be installed on the firewall near the starter cx? If your batteries are in the back, I'd recommend a 2AWG common ground for batteries, and two 4AWG feeders from battery conactors to the crossfeed contactor mounted on the FIREWALL. 2. If the answer to question 1 is no, the crossfeed contactor will be installed near the battery contactors in the aft fuselage. Question: Would AWG 2 flexible cables work just as well as straps to connect batt contactors to crossfeed contactors? Sure . . . 3. Z-14 shows a 10AWG cable connecting the aux battery connector the aux alternator. Question: Given the 10.5 ft distance between the two would 2AWG or 4 AWG cables be a better choice? If the crossfeed contactor is on firewall, then aux altenrator can feed the aux battery at the firewall too . . . 10AWG is fine. Bob . . . ________________________________________________________________________________
From: John Schroeder <jschroeder(at)perigee.net>
Date: Feb 12, 2003
Subject: Re: Wire gage
Hi Ed - Look on the CD ROM with MS Explorer and go to the folder: AutoCAD Drawings. Select the symbols folder. Most all of the symbols he uses are in that folder as .dwg files. Import them into a drawing as a block (Insert on the menu bar). They are all to the same scale as his entire drawing catalog. There is also another file of symbols in the drawings folder entitled: Symbols3.dwg. It is a series of drawings, each containing one or more blocks. You can import them into a drawing. Good luck and I hope this helps. John 2/12/2003 1:19:44 PM, N823ms(at)aol.com wrote: > >John: > > I finally just begin to teach myself this turbocad until I acquire the >AutoCAD LT. Took a few diagrams, cut and pasted the external power section on >to Z-14. Seems to be OK. I am looking for the symbols that Bob had offered at >one time. Do you know where they are? > > >Ed Silvanic > > ________________________________________________________________________________
Date: Feb 12, 2003
Subject: New Drawings for Dual Electrical
From: Walter Casey <mikec(at)caseyspm.com>
I took Robert Nuckolls drawing Z-14 and redid it in Adobe Illustrator. This should make it easier for some of you to print and edit the file. You can access the PDF's at http://www.caseyspm.com/RV7A.html Walter ________________________________________________________________________________
Date: Feb 12, 2003
From: Miller Robert <rmiller3(at)earthlink.net>
Subject: Re: EXPBUS
"Robert L. Nuckolls, III" wrote: To start with, how about sending me copies of the > pertinent pages from the manual so I can familiarize myself > with any special requirements for this engine. > > Bob . . . > > 6936 Bainbridge Road > Wichita, KS 67226-1008 Bob: Would love to see a well-developed system that does not use the EXPBus for the Eggenfellner Subaru. I intend to use this engine package, but have never gotten quite comfortable with the EXPBUS, in spite of the well-thought out circuit design given by Gary. The redundancy presently built into the electrical system, as shown in the manual, must be retained.... (electrically dependent engine, after all). The beautifully done installation manual can be downloaded from Jan's site. I look forward to the possibility of a robust off-the-shelf electrical package that does it all., without the EXPBUS Robert ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Xfeed switch
>Bob: >Im reading from the revision 10 of the aeroelectric connection. >On your Z-14 wire diagram you show a S700-2-5 switch for the >crossfeed/starter switch. It appears that this switch needs to go down >for the cross feed and up for the starter. Is that right? Don't we want >a switch that is off in the down position crossfeed on in the middle >position and start in the full up spring loaded position? On page 17-10 >under duel Alt/duel Batt description you describe the crossfeed switch as >a S700-2-50 switch. But that doesnt look like a spring loaded switch in >the full up position according to fig11-14 pp11-18. What don't I >understand and which switch is it? Thanks Tim The cross-feed switch is supposed to be an S700-2-50 and will be fixed at next revision. Use terminals 4-5 to control crossfeed contactor, terminals 1-3 for the starter contactor. This gives you OFF-XFEED-START as the three positions for the switch. Bob . . . ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Fwd: Wiring Plan et al
>It appears the Carling S2-50 switch you provided has the terminals on the >opposite side from what is shown on the Microswitch terminal numbering chart. yes. see http://www.aeroelectric.com/articles/Carling_Micro/Carling_Micro.pdf > Does the negative terminal on the D 25 rectifier module need to grounded? no > Is a 5A breaker adequate for the alternator field line? yes > Do you sell or recommend a particular breaker for this application? B&C stocks miniature, pullable breakers which are available from their website at http://www.bandc.biz/cgi-bin/ez-catalog/cat_display.cgi?7X358218 > Any reason I should not use the solid state adjustable regulator > (Transpo M5-130A) I already have? nope . . . > Are 1/4 watt diodes really adequate for protecting the > starter and DC power switches from the corresponding contactors? 1/4W? 1N400x series are 1A devices MORE than capable electrically but rather fragile mechanically. You can see how we use the more robust 1N540x series devices on our contactors at: http://www.aeroelectric.com/Catalog/switch/switch.html#s701-1 and http://www.aeroelectric.com/Catalog/switch/s701-1l.jpg >Must it be across the coil of the starter contactor or can it >be across the battery and starter contacts on the key switch >as the manufacturer's diagram shows? If you use our starter contactor at : http://www.aeroelectric.com/Catalog/switch/switch.html#s702-1 the diode is already built in. If you use another contactor, you need to add the diode across the contactor's coil terminals. Putting it across the switch contacts doesn't work as I explain and demonstrate in: http://www.aeroelectric.com/articles/spikecatcher.pdf Bob . . . ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: Oxygen bottle electrics
> ><tank >has a simple lever actuated valve for opening and closing. I could run a >cable to open and close, but I would rather have it done electrically. I'm >looking for a solenoid with some special talents. I want it to stay in >position even if power is lost. Has anyone seen such a device? Any and all >suggestions taken. > >Steve Richard >steve(at)oasissolutions.com>> > >How about a door lock actuator from almost any late model car? They are >small electric motor powered devices that will go to either position and >stop. Much lighter than a solenoid that would have the same force and >travel. > >Gary Casey Neat idea. I need to go look at those critters. Bob . . . ________________________________________________________________________________
Date: Feb 12, 2003
Subject: Feild Breaker/ Switch Selection/ Nav/Pos Hookup
From: Don Boardman <dboardm3(at)twcny.rr.com>
Hi Bob, A few questions if I may. ( All Electric on Budget ) 1) I am happy to be using fuse blocks. So happy in fact, I would rather not use the 5A breakers you call for in the Alt Field circuits. Why are they necessary? If I must use breakers I will probably mount them on the swing down panel I am using to mounting the fuse blocks on. They could be re-set with a short reach under the panel. 2) I have seen two ways to set up the Master switch. One using a 2-3 and one using a 2-10 . Why is it an advantage to be able to turn on the BAT only in the middle position? Does it hurt to have the Bat and ALT Field active when you might just want to play with the Radios or GPS and the engine is not running? 3) Speaking of playing with the GPS. Does it make any sense to put the Electric Horizon and DG on a separate switch so that they are not spinning up every time the Master is turned on and flight is not the intention. 4) I have the strobe/nav/position fixtures from Aeroflash. I see no reason not to have the Nav and Position lights come on together, controlled by a single toggle. Is there any problem using a single fuse and running a single conductor from the switch out to the wingtips and connecting both lamp leads to the conductor? Night flying is a rare occurrence and only for a short time at the end of a trip. Loss of the Nav/Pos lights would be backed up by the strobes and wig-wag Landing Taxi lights. Regards, Don Boardman & Partner, Randy Bowers AeroElectric Powered Super Moose #130 M-14PF 400HP, MT-prop, Aerocet 3500 amphibs, Rome, NY ________________________________________________________________________________
Date: Feb 12, 2003
From: "Robert L. Nuckolls, III" <bob.nuckolls(at)cox.net>
Subject: Re: EXPBUS and Eggenfellner
> > >Just wanted to add my two cents on this. I have a Glastar with the >Egfgenfellner package. I do not use the EXPBUS. It was quite easy to >adapt one of Bob's drawings to accomodate the all-electric, >fuel-injected engine's needs. > One of the goals that Jan Eggenfellner has espoused is to offer a very >complete package....something that really appealed to this novice. As >such, he sees an advantage to having all of his customers using the same >parts, be it electrical or plumbing or whatever. Makes his job of >supporting his customers less complicated. I haven't been a >particitant in his user's group for a while, but when I was there he >never discouraged the use of alternative electrical approaches. He just >re-iterated that he couldn't (and shouldn't) answer too many questions >on systems he didn't design. Maybe that has changed in the past few >weeks...I don't know. > As to the warranty, isn't just about every warranty filled with >loopholes if you alter the product in any way? >Bill Yamokoski >very happy with my non-EXPBUS Glastar Bill, did you document your approach in a way that's easy to share? I'd like to see what you did and then perhaps add a figure to the 'Connection that's unique to the needs of the Eggenfellner system. I've looked over his installation manual briefly . . . mostly good stuff but I think we can help him out a little here. Let's put our heads together and see what the elegant solution looks like. Anyone else out flying the Eggenfellner package with a non-EXPBUS architecture? Bob . . . ________________________________________________________________________________
From: LRE2(at)aol.com
Date: Feb 12, 2003
Subject: Re: Oxygen bottle electrics
Steve, You know there is a much simpler and more elegant solution to your problem. Mountain High Oxygen Systems ( www.mtn-high.com )offers very nice panel mounted regulators, so that you can plumb your O2 bottle to the panel where you have direct control over not only on/off, but also flow rates. The


January 28, 2003 - February 12, 2003

AeroElectric-Archive.digest.vol-bp