AeroElectric-Archive.digest.vol-gu

March 13, 2007 - April 02, 2007



Date: Mar 13, 2007
From: "Michael T. Ice" <aurbo(at)ak.net>
Subject: Re: re: wiring diagram benefits
Erich, I can see both sides of this issue and they are both right. Roll your own. I am going the simplified route myself. I like the Z-11 as a basic and I have added a few extras. I am amazed though at the detail some folks put into their wire diagrams and web sites. You people are absolutely gifted. Where do you find the time to do all of that and build an airplane? I don't think I will ever sell my airplane but if I did it seems these planes sell themselves. Mike Ice RV-9 (yep! Little wheel in the back) Electrical done, canopy in progress (on and off the fuselage a zillion times) ----- Original Message ----- From: Erich_Weaver(at)URSCorp.com To: aeroelectric-list(at)matronics.com Sent: Tuesday, March 13, 2007 2:04 PM Subject: AeroElectric-List: re: wiring diagram benefits Thanks for the input on this guys. I remain open to what you are saying, but indulge my hard headedness for a minute longer. I readily admit that I will quickly forget details of my electrical system in the near future. However..... It seems to me that the wiring diagrams chief benefit is for mulling things over from the convenience of your own living room. If I start messing with my electrical system its likely to be because something isnt working, and this will require me to gain access to the various components of the electrical system. The hidden components of my electrical system (AHRS box , fuseholders, wig-wag flasher, voltage regulator, etc) are relatively easily accessible and if any of these are not easily identified by looks alone, they are labeled. Every wire coming from such components is labeled with respect to exactly where it is coming from and where it is going to. Therefore, I will be able to check that the electrical connections are sound at both ends of every wire segment. I will also be able to check that the wires go to the right connection point on each component by comparing my connections with what is presented in the manufacturer's documentation, which I have carefully cataloged in my building binders. I can further check that components are actually connected as labeled with a continuity tester. In short, it seems to me that most of the truly valuable information on my electrical system can be gained from the schematic and when necessary for repairs, visual inspection/testing of the individual components and at their electrical connection points. The actual route the wires take between components seems almost irrelevant to me. I am not terribly persuaded by arguments of some perceived future value to future buyers of my plane. First, Im not sure I buy the argument that my plane will be worth less. The phrase "Comprehensive wiring diagrams available" doesnt seem to show up much in adds for experimentals. And for those buyers that have the desire/need to know my electrical system, I still think the schematic and good labelling practices I have adhered to, along with manufacturers' documentation provide a solid basis for diagnosing and resolving problems. Okay, I can already see the aero-electric masses collectively shaking their heads back and forth at me. Nomex flame suit donned. Fire away. Concrete examples of how your wiring diagrams saved the day, and conversely, how my annotated Z-13/8 schematic and comprehensive component and wire labeling are woefully inadequate will be enthusiastically received. Just between us girls, I'll bet there are more than a few out there with virtually no electrical documentation combined with complete ignorance of their system. They may even be conspiring to sell these planes to others! : ) ________________________________________________________________________________
Subject: Re: RF noise from EFIS
From: "N777TY" <microsmurfer(at)yahoo.com>
Date: Mar 13, 2007
Bob, It may be hard to describe the noise, so I figured a video may help :) Here's a 1-minute video of my sniffing around with a handheld scanner (squelch turned down completely): http://www.vitez.net/noise.wmv You'll notice a few spots where there's no noise and you just hear regular radio static.. Maybe ignore that weird noise when scanner is under the panel, as I don't hear it like that in my panel radio. The radio is Garmin SL-40. Not sure what you mean by positioning of controls.. Also, the radio (well, both SL-40 and handheld) does a great job of "killing" the noise when it receives even a semi-decent transmission.. so this noise doesn't actually affect reception, except for very, very weak ones (where the noise can just about barely be heard in the background). However, it sounds horrible (and loud) when there's no transmission and squelch is pulled. Again, it never breaks the squelch... So, push the squelch and you'll probably never hear it (or barely ever notice it's there).. but I'm looking for "perfection" here :) The radio has this mode where it shows the signal level, and for RF level it shows around 18 when screens are off.. then jumps to about 40 when screens are turned on.... Not sure what these numbers exactly mean or what units those are.. but there's definitely a difference. (this is with no transmissions being received). Not sure if I mentioned this -- all these units are grounded on the firewall at a common grounding block. Tried grounding locally on the panel (both radio and screens as well as screens alone) and that didn't make any difference. One thing I haven't tried yet is transmitting -- not sure if there's any affect on clarity or strength of outgoing transmissions.. Any ideas are appreciated. Or am I getting worked up about nothing? Thanks! Radomir -------- RV-7A N777TY (res) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100373#100373 ________________________________________________________________________________
Date: Mar 13, 2007
From: sarg314 <sarg314(at)comcast.net>
Subject: Re: re: wiring diagram benefits
I drew a wiring diagram first because I wouldn't know how to wire it if I didn't (basically a Z-11). Every signal has a name, every wire is labeled. As one who has successfully used automotive wiring diagrams (and other schematics), I'm sure the diagram will save trouble shooting time down the road. It will influence a future buyer IF the guy is like me. A lot of us builders are nerd-geek-techies who think this stuff is important. -- Tom Sargent, RV-6A, in the act of wiring, no less. ________________________________________________________________________________
From: "Alex" <alex157(at)pwhome.com>
Subject: Comments please on this solid state contactor.......
Date: Mar 13, 2007
I have been testing my electrical system on my all- electric Velocity- with no load, only the coils energized for about 30 minutes my battery contactors were both quite hot- too hot to hold for more than say 5 seconds- comments from other builders agree that this is rather normal- someone suggested the "Czonka III" solid state unit- uses no appreciable power- good for tens of thousands of cycles at 200 amps- please see attached PDF- is there any foreseen drawback other than cost? Alex ________________________________________________________________________________
Date: Mar 13, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Comments please on this solid state contactor.......
>I have been testing my electrical system on my all- electric Velocity- with >no load, only the coils energized for about 30 minutes my battery contactors >were both quite hot- too hot to hold for more than say 5 seconds- comments >from other builders agree that this is rather normal- someone suggested the >"Czonka III" solid state unit- uses no appreciable power- good for tens of >thousands of cycles at 200 amps- please see attached PDF- is there any >foreseen drawback other than cost? None . . . but keep in mind that the "too hot to touch" contactors have been used for about 70 years with good return on investment. The "solid state" units have circuitry that drops coil current from an initial, full power pull-in current to some nominal holding current after a second or so. Problem with some devices is that the duty-cycle power controller generates noise in some systems. Further, it's unknown whether the circuitry as-supplied would live happily in known (DO-160) world of stresses. I'm not suggesting that it won't . . . just don't know. The continuous duty contactor dissipates about 10 watts. Sufficient power to raise the surface temperature to about 170F in a room temperature environment. See: http://www.aeroelectric.com/Pictures/Contactors/Battery_Contactor_Temps_1.jpg http://www.aeroelectric.com/Pictures/Contactors/Battery_Contactor_Temps_2.jpg This 'seems' hot but all of the materials used to fabricate the contactor are rated at 150C or better. It's no big deal in the grand scheme of things and it's hard to beat the price. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Mar 13, 2007
Subject: Re: wiring diagram benefits?
In a message dated 03/13/2007 11:36:15 AM Central Daylight Time, Erich_Weaver(at)URSCorp.com writes: "never did it, never needed it" ...until you do and didn't! If you did a good job on the design & install, you likely never will need it, but 5 years from now, wouldn't it be handy to know what ya got when you go to upgrade to that spiffy new holographic cockpit? Mark- RV-6A N51PW "Mojo", former industrial 'lectrician, confirmed Nuckollhead, and pretty anal when it comes to wiring diagrams, but YMMV, natcherly! _http://websites.expercraft.com/n51pw/index.php?q=log_entry&log_id=7604_ (http://websites.expercraft.com/n51pw/index.php?q=log_entry&log_id=7604) fer example


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From: "Alan K. Adamson" <aadamson(at)highrf.com>
Subject: Vertical power - Beta tester blog
Date: Mar 13, 2007
I've started a Blog of my testing activities around the Vertical Power VP-200 Duo going into my Lancair Legacy. Feel free to check in from time to time. If you have an RSS reader, there is both an RSS and an ATOM version of the blog. http://legacyair.blogspot.com Short version - Dual buss - Dual Alt - 24V - EFIS panel - VP-200 Duo - MVP-50 Engine monitor - utilizing the 4 channels of Overrides on the VP-200 - plus all the normal amazing features - going into a Lancair Legacy FG with IO-550 Also includes a few "requested features" - being a real beta tester :) - Automatic canopy seal - Remote based, electronic Canopy lock - Mac servo actuated RamAir Enjoy and let me know what you think as I progress along. Wiring should start in earnest next week. Alan ________________________________________________________________________________
Subject: Re: RF noise from EFIS
From: "N395V" <n395v(at)hughes.net>
Date: Mar 14, 2007
Rodney, You are correct, Bob did not name any particular personality in his comment.. > Which suggests a profound lack of knowledge However, in context it can be presumed to be aimed at either me or Blue Mountain (aka Greg). Given history I presumed it was aimed at Greg. In either case the words "suggests a profound lack of knowledge" are an eloquent way of saying you are stupid. This I take as an insult. There are many ways in which Bob could have structured his response to make his point, such as, "my experience suggests that a better way to approach this problem would be to....." but he chose terms that I find insulting no matter who they are aimed at. You and others may find my language offensive but if you are going to insult someone I see no need to hidei t with eloquence. As far as my going away Bob can take care of that ith the push of a button. Short of that you will have to suffer my occassional presence as there are many others on this list whose valuable contributions I find useful. -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100438#100438 ________________________________________________________________________________
Subject: Re: RF noise from EFIS
Date: Mar 14, 2007
From: "Chuck Jensen" <cjensen(at)dts9000.com>
Eloquence coutns. Even when slapped in the face, I much prefer it with a velvet glove!! Chuck Jensen -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of N395V Sent: Wednesday, March 14, 2007 9:08 AM Subject: AeroElectric-List: Re: RF noise from EFIS Rodney, You are correct, Bob did not name any particular personality in his comment.. > Which suggests a profound lack of knowledge However, in context it can be presumed to be aimed at either me or Blue Mountain (aka Greg). Given history I presumed it was aimed at Greg. In either case the words "suggests a profound lack of knowledge" are an eloquent way of saying you are stupid. This I take as an insult. There are many ways in which Bob could have structured his response to make his point, such as, "my experience suggests that a better way to approach this problem would be to....." but he chose terms that I find insulting no matter who they are aimed at. You and others may find my language offensive but if you are going to insult someone I see no need to hidei t with eloquence. As far as my going away Bob can take care of that ith the push of a button. Short of that you will have to suffer my occassional presence as there are many others on this list whose valuable contributions I find useful. -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100438#100438 ________________________________________________________________________________
Date: Mar 14, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RF noise from EFIS
> > > > Which suggests a profound lack of knowledge as > > to how noises should be kept inside the product > > >You just can't resist a dig at Greg can you? I can't resist a dig at poor science and equally poor teaching. Read my most earnest attempts to engage Greg in lucid, useful dialog at: http://aeroelectric.com/articles/richter/richter.html This exchange took place AFTER he took a whack at the AeroElectric Connection when he said, "I've seen so much truly atrocious work, much of it per Bob's book". But when asked to point out any writing in the 'Connection so poorly written as to induce one to do atrocious work, he was silent. >Now I know why so many others think you are an asshole. This isn't about me and Greg, it's about doing the best we know how to do for a price that a customer is happy to have paid. Products offered from the BMA website fall demonstrably short of those goals. I kept my assessments to myself for years but Greg chose to open the door with no prompting from me. He then demonstrated a lack of ability and/or willingness to engage in good critical review. I can't help what people think when they're offering opinions based upon a lack of knowledge and understanding. I'll invite you to hang around the list for awhile and gather enough data about me and what the List is about toward the goal of formulating your own, informed opinion. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 14, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: re: wiring diagram benefits
Erich_Weaver(at)URSCorp.com wrote: > I am not terribly persuaded by arguments of some perceived future > value to future buyers of my plane. First, Im not sure I buy the > argument that my plane will be worth less. The phrase "Comprehensive > wiring diagrams available" doesnt seem to show up much in adds for > experimentals. And for those buyers that have the desire/need to know > my electrical system, I still think the schematic and good labelling > practices I have adhered to, along with manufacturers' documentation > provide a solid basis for diagnosing and resolving problems. > > Okay, I can already see the aero-electric masses collectively shaking > their heads back and forth at me. Nomex flame suit donned. Fire away. > Concrete examples of how your wiring diagrams saved the day, and > conversely, how my annotated Z-13/8 schematic and comprehensive > component and wire labeling are woefully inadequate will be > enthusiastically received. > No need for flamesuits, Erich. If your documentation does it for you, more power to you. I seriously doubt most buyers would want to see a wiring diagram any more than they'd want to see the plans the plane was built from. The diagram is just a tool, not a holy document. But just as I can drive a screw with a hammer, it 'nice' to have a screwdriver for the job. -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Date: Mar 14, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RF noise from EFIS
Went back a few postings and found this . . . >Trying to figure out a problem I'm running into where an EFIS screen seems >to be putting RF noise into my radio. >The noise seems "small" -- as in it can't be heard if there's a strong >signal being received, but can be heard if there's no transmission or as >background while receiving poor signal. It never breaks the squelch on >the radio at all, so it can only be heard if I pull the squelch button on >my SL-40. When you say "small" . . . do you think it likely that you'll notice it in flight with wind and engine noises? I know this is a VERY subjective assessment. But I've worked with dozens of builders and airplane owners who struggled with noises heard in the quiet of the shop that would have been unnoticed in the air. I'm not suggesting that you shouldn't endeavor to know how the noise is happening and perhaps develop an approach to making it go away . . . but noise management is a give/take proposition and you MIGHT be spending a lot of $time$ on something that doesn't need fixing. >noise goes away if antenna is disconnected, in which case all I can hear >is normal radio static. Good data . . . it's radiated noise coming in through the antenna. >noise can be heard if rubber ducky antenna is connected instead of the >Comant antenna (so I'm not sure it's my real antenna installation at issue >here, but could be?) Due to the setup I have, I can hook this antenna >right behind the radio, or at the end of the coax run.. didn't notice any >difference between the two. Do you have a hand-held? Hand held radios with a rubber-duck or even short "probe" antennas of a couple inches long are helpful "sniffers". In the lab, I have access to a spectrum analyzer. It's a receiver that plots an amplitude vs. frequency display on a 'scope screen. I can attach a small probe to the end of a coax and poke around the noisy electro-whizzy to find where the noise is coming out. >Tried Radio Shack ferrite choke at various locations and it didn't seem to >do anything. The snap-on ferrites are never useful for conducted noise and only effective starting at about 100 MHz and going up. I've never seed a problem at comm frequencies fixed with a snap-on ferrite. I have seen useful applications of ferrites at UHF frequencies . . . but in every case, these situations would have been better addressed INSIDE the electro-whizzy as part of the original design. >Tried some RS in-line choke (in-line with radio +, as well as EFIS + and >ground) which also didn't do anything either. >coax doesn't run close to the EFIS screen, and for the most part, it's not >close to other wires. >I have a 2-screen setup and both (and either) produce this noise... Okay, you need to "sniff". Take a coax from the back of your comm radio (or a handheld) and terminate the loose end with one of these: http://www.aeroelectric.com/Pictures/Tools/Sniffer_Probes.jpg Poke around the openings and cables of the offending device to see if you can deduce the exit point for the noise. If you can't hear the noise with the suggested probes try larger ones. >Re AeroElectric-List RF noise.ems >have not tried transmitting, so no idea what kind of impact it'd have (if >any) on outgoing transmissions.. focused on reception at this point. It's exceedingly remote that radiated noises get into transmitted signals. >again, since it doesn't break the squelch, it's not a big big issue, but >it's annoying and would love to see it go away :) Sure . . . let's do the sniffing and see if you can identify the egress point. But let's not ignore the possibility that this noise may not be worth running to ground. Bob . . . ________________________________________________________________________________
Date: Mar 14, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RF noise from EFIS
> >This I take as an insult. There are many ways in which Bob could have >structured his response to make his point, such as, "my experience >suggests that a better way to approach this problem would be to....." >but he chose terms that I find insulting no matter who they are aimed >at. Being insulted is a choice. When assessing words about me, they can be sorted into two pots: (1) the words illustrate facts which call for considered integration into my future actions or (2) they're meaningless. In neither case are they worthy of an emotional investment. I can be insulted only if I allow it. In the instance before us, there were no words about you only about poor science, lack of understanding and poor teaching based on those shortcomings. We all suffer from lack of understanding to some degree on every topic. It's incumbent upon good teachers to remedy the former before attempting to do the later. Bob . . . ________________________________________________________________________________
From: "Frank Stringham" <fstringham(at)hotmail.com>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Date: Mar 14, 2007
Any experience in the group with the products (Pro G Hub) supplied by Approach Fast Stack http://www.approachfaststack.com . At first glance it looks like a real elegant way to interconnect the insturments in the panel. Some of the questions I have include: 1. How is the company to work with? Is the install as easy as they say! Any maintence issues? Frank @ SGU RV7A "NDY" _________________________________________________________________ Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. Intro*Terms https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search=mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 ________________________________________________________________________________
Date: Mar 14, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RF noise from EFIS
>Rodney, > >You are correct, Bob did not name any particular personality in his >comment.. > > > > Which suggests a profound lack of knowledge > > >However, in context it can be presumed to be aimed at either me or Blue >Mountain (aka Greg). Given history I presumed it was aimed at Greg. > >In either case the words "suggests a profound lack of knowledge" are an >eloquent way of saying you are stupid. No, ignorant. Ignorance can be remedied by the civilized discourse between capable teachers and willing students. In this instance, Greg has yet to demonstrate a membership in either group. >As far as my going away Bob can take care of that with the push of a >button. Short of that you will have to suffer my occassional presence as >there are many others on this list whose valuable contributions I find >useful. I'm sorry that you don't find value in my offerings. This IS disheartening for a teacher to hear. If you perceive shortcomings in either the science or practice I have to offer, I'd be pleased to address those concerns. Nobody wants you to go away. Everybody wants our $time$ spent here on the List to yield a good return on the investment. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: <frank.phyllis(at)mindspring.com>
Subject: Popped CB
Date: Mar 14, 2007
Bob, The CB popped when I released the starter contactor (switch with key). Master was on BAT & ALT. I tried starting with just BAT & it did not pop. It did not pop when I switched to Alt after starting with Bat only. I noticed this time I'm not getting a charge from Alt (verified master switch on Alt) at 2400RPM. I overlooked the diode on the starter contactor so, no, I do not have one. Maybe that's the problem??? Thanks Frank -----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 Sent: Monday, March 12, 2007 2:16 PM Subject: Re: AeroElectric-List: Popped CB > >I started my 912ULS for the first time. Ran like a charm. However, at >both starts the alt cb popped. I used the Z16 diagram. Obviously I >have "crossed wires" some place--any ideas? When did the breaker pop? As soon as you pushed the starter button? When you released the starter button? Do you have a diode across the coil of your starter contactor? Did you have the alternator turned ON while cranking or did you turn it on after the engine was running? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Re: RF noise from EFIS
Date: Mar 14, 2007
I totally agree with Bob. My experience with BMA and the folks there have been the worst for me as compared to ALL of the other companies I deal with (to many to list). Let's summarize, BMA produces products that at face value looks cool and if it worked as advertised would be a good product. But when you dig into the finer points of BMA products such as: stability, installation, customer service, ergonomics, builder philosophy, function, and price they all fall short as compared to almost ALL the others. I work in the field with builders of experimental homebuilt airplanes. I spent seven years in an avionics shop, three years on a military R&D project, and 30 years total aircraft maintenance. I am not very polished in my delivery of words when it comes to basic avionics. I express my experience and you take it for what its worth. Here in Arizona we have a large group of builders who are actively building. We do not have any real profession support for avionics available here, so we get by with the local knowledge and experience of all the engineers and techs. here and of course Lectric Bob. So far we've had many successes and few failures. Of the 35+ airplanes under construction (not flying yet) that I have worked on in the past 365 days (this past year). I have seen my share of BMA products (including my own). After dealing with BMA too many times with problems I don't even call them any more. I can say that I have over 12 saves this past year regarding folks purchasing BMA stuff. Those of you who have purchased BMA and managed to get it to work to an acceptable level that's great. I would just like to say there are a whole host of products out there that perform much better. Mike Larkin -----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 Sent: Wednesday, March 14, 2007 8:06 AM Subject: Re: AeroElectric-List: Re: RF noise from EFIS > > > > Which suggests a profound lack of knowledge as > > to how noises should be kept inside the product > > >You just can't resist a dig at Greg can you? I can't resist a dig at poor science and equally poor teaching. Read my most earnest attempts to engage Greg in lucid, useful dialog at: http://aeroelectric.com/articles/richter/richter.html This exchange took place AFTER he took a whack at the AeroElectric Connection when he said, "I've seen so much truly atrocious work, much of it per Bob's book". But when asked to point out any writing in the 'Connection so poorly written as to induce one to do atrocious work, he was silent. >Now I know why so many others think you are an asshole. This isn't about me and Greg, it's about doing the best we know how to do for a price that a customer is happy to have paid. Products offered from the BMA website fall demonstrably short of those goals. I kept my assessments to myself for years but Greg chose to open the door with no prompting from me. He then demonstrated a lack of ability and/or willingness to engage in good critical review. I can't help what people think when they're offering opinions based upon a lack of knowledge and understanding. I'll invite you to hang around the list for awhile and gather enough data about me and what the List is about toward the goal of formulating your own, informed opinion. Bob . . . -- 2/8/2007 ________________________________________________________________________________
Date: Mar 14, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Popped CB
> >Bob, >The CB popped when I released the starter contactor (switch with key). >Master was on BAT & ALT. I tried starting with just BAT & it did not >pop. It did not pop when I switched to Alt after starting with Bat >only. > >I noticed this time I'm not getting a charge from Alt (verified master >switch on Alt) at 2400RPM. Hmmm . . . this needs troubleshooting. Has it worked in the past? >I overlooked the diode on the starter contactor so, no, I do not have >one. Maybe that's the problem??? I'll bet on it. But in any case, starting with the alternator off is a reasonable procedure too. However, your starter switch will appreciate having the diode added. Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Date: Mar 14, 2007
I looked at this too, and talked to a local avionics shop. I liked the idea of pre-made cables (not just harnesses) just plug them in and easy to upgrade in the future (assuming they stay in business) but the down side is, more weight, more cost and more connections to fail. I have come to conclude that wiring harnesses are not too difficult to install (I may even make my own) cost less, weigh less and just not going to save me enough time on the electrical install. There is still a lot of wiring to do and one will have to get competent at it and have the tools anyway. Bevan RV7A Finish kit -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Frank Stringham Sent: Wednesday, March 14, 2007 8:07 AM Subject: Re: AeroElectric-List: Re: Pro G Hub by http://www.approachfaststack.com/ --> Any experience in the group with the products (Pro G Hub) supplied by Approach Fast Stack http://www.approachfaststack.com . At first glance it looks like a real elegant way to interconnect the insturments in the panel. Some of the questions I have include: 1. How is the company to work with? Is the install as easy as they say! Any maintence issues? Frank @ SGU RV7A "NDY" _________________________________________________________________ Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. Intro*Terms https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 ________________________________________________________________________________
Date: Mar 14, 2007
From: Brett Ferrell <bferrell(at)123mail.net>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
I've installed the Pro G, and I love it. The company was great to work with, and the documentation was good, and it has performed as expected in my pre-flight testing. I should get in the air this spring, but so far I've got no complaints, and I'm happy that I didn't have to make my harnesses (the standard stuff plus transponder to EFIS, GPS to ELT, EFIS to Radios, etc.) Brett > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Frank > Stringham > Sent: Wednesday, March 14, 2007 8:07 AM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: Re: Pro G Hub by > http://www.approachfaststack.com/ > > --> > > Any experience in the group with the products (Pro G Hub) supplied by > Approach Fast Stack http://www.approachfaststack.com . At first glance it > looks like a real elegant way to interconnect the insturments in the panel. > > Some of the questions I have include: 1. How is the company to work with? Is > the install as easy as they say! Any maintence issues? > > Frank @ SGU RV7A "NDY" > > _________________________________________________________________ > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. > Intro*Terms > https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search > =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > ________________________________________________________________________________
From: "Frank Stringham" <fstringham(at)hotmail.com>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Date: Mar 14, 2007
Brett What are the various instruments in your panel.....and why did you choose them? Plus as I contemplate my decision to go with the fast satck are their any install gotchas' I should be aware of? TIA Frank @ SGU RV7A "NDY" >From: Brett Ferrell <bferrell(at)123mail.net> >Reply-To: aeroelectric-list(at)matronics.com >To: aeroelectric-list(at)matronics.com >Subject: RE: AeroElectric-List: Re: Pro G Hub by > http://www.approachfaststack.com/ >Date: Wed, 14 Mar 2007 08:53:35 -0700 > > > >I've installed the Pro G, and I love it. The company was great to work >with, >and the documentation was good, and it has performed as expected in my >pre-flight testing. I should get in the air this spring, but so far I've >got >no complaints, and I'm happy that I didn't have to make my harnesses (the >standard stuff plus transponder to EFIS, GPS to ELT, EFIS to Radios, etc.) > >Brett > > > > > -----Original Message----- > > From: owner-aeroelectric-list-server(at)matronics.com > > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Frank > > Stringham > > Sent: Wednesday, March 14, 2007 8:07 AM > > To: aeroelectric-list(at)matronics.com > > Subject: Re: AeroElectric-List: Re: Pro G Hub by > > http://www.approachfaststack.com/ > > > > --> > > > > Any experience in the group with the products (Pro G Hub) supplied by > > Approach Fast Stack http://www.approachfaststack.com . At first glance >it > > looks like a real elegant way to interconnect the insturments in the >panel. > > > > Some of the questions I have include: 1. How is the company to work >with? Is > > the install as easy as they say! Any maintence issues? > > > > Frank @ SGU RV7A "NDY" > > > > _________________________________________________________________ > > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a >month. > > Intro*Terms > > >https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search > > =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > > > > > > > > > > > > > > > > > > > > > > > > > _________________________________________________________________ Get a FREE Web site, company branded e-mail and more from Microsoft Office ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Date: Mar 14, 2007
Brett, Did you get documentation with the HUB so that cables could be made from scratch in the future, or do you always have to use their cables? Bevan -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Brett Ferrell Sent: Wednesday, March 14, 2007 8:54 AM Subject: RE: AeroElectric-List: Re: Pro G Hub by http://www.approachfaststack.com/ --> I've installed the Pro G, and I love it. The company was great to work with, and the documentation was good, and it has performed as expected in my pre-flight testing. I should get in the air this spring, but so far I've got no complaints, and I'm happy that I didn't have to make my harnesses (the standard stuff plus transponder to EFIS, GPS to ELT, EFIS to Radios, etc.) Brett > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of > Frank Stringham > Sent: Wednesday, March 14, 2007 8:07 AM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: Re: Pro G Hub by > http://www.approachfaststack.com/ > > --> > > Any experience in the group with the products (Pro G Hub) supplied by > Approach Fast Stack http://www.approachfaststack.com . At first > glance it looks like a real elegant way to interconnect the insturments in the panel. > > Some of the questions I have include: 1. How is the company to work > with? Is the install as easy as they say! Any maintence issues? > > Frank @ SGU RV7A "NDY" > > _________________________________________________________________ > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. > Intro*Terms > https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y& > search > =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > ________________________________________________________________________________
Date: Mar 14, 2007
From: Brett Ferrell <bferrell(at)123mail.net>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Frank My equipment list is below. THe only gotcha I had was that I intended to install a cell phone interface, and that is really a third comm to the Pro G Hub, so I had to return the unit for a minor retrofit. They were the only ones I knew of doing this kind of work when I got mine, and I'd decided that I'd had enough fun running my power wiring and EFIS engine probe leads, that I didn't need the experience of hooking up all of the avionics. Plus, they're so expensive, I didn't want to risk damaging them. It's nice because I can display the SL30 and 430 guidance data on the EFIS, my EFIS encoder goes to my transponder, my cell and entertainment inputs go to my intercomm, my GPS feeds my ELT, etc. 1) Blue Mountain EFIS/One - SL30 sends VOR CDI/GS info to E/1 for display 2) Blue Mountain EFIS/Sport (planned) - same SL30 interconnect 3) Garmin GTX-327 - Transonder gets gray code altitude data from E/1 4) Artex G406 - 3 mode ELT with GPS position broadcast, accepts data from Garmin, GPS nav interface board not yet purchased 5) Garmin 430 - GPS nav/comm 6) SL30 - Nav/comm 7) Blue Mountain 2-axis autopilot 8) Sirius radio into to intercomm 9) PMA7000B - w/record function & playback 10) DVD/CD entertainment for back seats, w/intercomm interconnect and isolate 11) Aux entertainment (MP3/iPod) input Brett Quoting Frank Stringham : > > > Brett > > What are the various instruments in your panel.....and why did you choose > them? Plus as I contemplate my decision to go with the fast satck are their > any install gotchas' I should be aware of? > > TIA > > Frank @ SGU RV7A "NDY" > > > >From: Brett Ferrell <bferrell(at)123mail.net> > >Reply-To: aeroelectric-list(at)matronics.com > >To: aeroelectric-list(at)matronics.com > >Subject: RE: AeroElectric-List: Re: Pro G Hub by > > http://www.approachfaststack.com/ > >Date: Wed, 14 Mar 2007 08:53:35 -0700 > > > > > > > >I've installed the Pro G, and I love it. The company was great to work > >with, > >and the documentation was good, and it has performed as expected in my > >pre-flight testing. I should get in the air this spring, but so far I've > >got > >no complaints, and I'm happy that I didn't have to make my harnesses (the > >standard stuff plus transponder to EFIS, GPS to ELT, EFIS to Radios, etc.) > > > >Brett > > > > > > > > -----Original Message----- > > > From: owner-aeroelectric-list-server(at)matronics.com > > > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Frank > > > Stringham > > > Sent: Wednesday, March 14, 2007 8:07 AM > > > To: aeroelectric-list(at)matronics.com > > > Subject: Re: AeroElectric-List: Re: Pro G Hub by > > > http://www.approachfaststack.com/ > > > > > > --> > > > > > > Any experience in the group with the products (Pro G Hub) supplied by > > > Approach Fast Stack http://www.approachfaststack.com . At first glance > >it > > > looks like a real elegant way to interconnect the insturments in the > >panel. > > > > > > Some of the questions I have include: 1. How is the company to work > >with? Is > > > the install as easy as they say! Any maintence issues? > > > > > > Frank @ SGU RV7A "NDY" > > > > > > _________________________________________________________________ > > > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a > >month. > > > Intro*Terms > > > > >https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search > > > =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > _________________________________________________________________ > Get a FREE Web site, company branded e-mail and more from Microsoft Office > > ________________________________________________________________________________
Date: Mar 14, 2007
From: Brett Ferrell <bferrell(at)123mail.net>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
Bevan, Well, I have the documentation from the component manufacturers, so I could always make the cables myself in the future. But the misconception is that their supplied Hub system is "just a harness". It's not, the hub's board handles cross-connecting multiple components to the same device, and there's a great deal of flexibility there. However, I found the docs from Fast STack to be quite complete and direct, and I found them easy to work with on the phone. Brett Quoting B Tomm : > > Brett, > > Did you get documentation with the HUB so that cables could be made from > scratch in the future, or do you always have to use their cables? > > Bevan > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Brett > Ferrell > Sent: Wednesday, March 14, 2007 8:54 AM > To: aeroelectric-list(at)matronics.com > Subject: RE: AeroElectric-List: Re: Pro G Hub by > http://www.approachfaststack.com/ > > --> > > I've installed the Pro G, and I love it. The company was great to work > with, and the documentation was good, and it has performed as expected in my > pre-flight testing. I should get in the air this spring, but so far I've > got no complaints, and I'm happy that I didn't have to make my harnesses > (the standard stuff plus transponder to EFIS, GPS to ELT, EFIS to Radios, > etc.) > > Brett > > > > > -----Original Message----- > > From: owner-aeroelectric-list-server(at)matronics.com > > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of > > Frank Stringham > > Sent: Wednesday, March 14, 2007 8:07 AM > > To: aeroelectric-list(at)matronics.com > > Subject: Re: AeroElectric-List: Re: Pro G Hub by > > http://www.approachfaststack.com/ > > > > --> > > > > Any experience in the group with the products (Pro G Hub) supplied by > > Approach Fast Stack http://www.approachfaststack.com . At first > > glance it looks like a real elegant way to interconnect the insturments in > the panel. > > > > Some of the questions I have include: 1. How is the company to work > > with? Is the install as easy as they say! Any maintence issues? > > > > Frank @ SGU RV7A "NDY" > > > > _________________________________________________________________ > > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a > month. > > Intro*Terms > > https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y& > > search > > =mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Mar 14, 2007
Subject: Pro G Hub by http://www.approachfaststack.com/
From: James H Nelson <rv9jim(at)juno.com>
Hi Frank, I have the Approach Pro G Hub in my "9". There is one thing you need to do if considering using them for wiring. It simplifies the wires but you must give them exactly what you are using and the options you will be using. Brand name of wing levelers, EFIS (if you are using them and what extras you will use from them) comm radios, Intercom and model and if its stereo / monoral, transponders and any interfacing required (such as mode "S", and if the altitude encoding is to be serial input or gray code.) All these things are necessary to get a good cable interface with their system. I'm not flying yet but I will be doing soon. So far the checks seem to be ok. Place you hub is a position behind your panel so you can get to it and remove the plug in 's You have to be able to twist the locking screws on the "D" sub B ends. It gets real busy so plan for the transition of the cables thru the bulkheads and around to the units desired. I cut several 2" holes to get the wiring where it needed to go. Jim Nelson www.websites.expercraft.com/jimn ________________________________________________________________________________
From: "Frank Stringham" <fstringham(at)hotmail.com>
Subject: Pro G Hub by http://www.approachfaststack.com/
Date: Mar 14, 2007
Jim, Brett and the rest of you good folks I am running with this thread on the Vansairforce forum and some over there seem to think that if the panel is simple VFR the hub is fine, but the more complex the panel the less capable the hub would be. At first blush I believe these are well meaning opinoins not based on facts. So are they talking fact or opinion. TIA Frank @ SGU RV7A "NDY" >From: James H Nelson <rv9jim(at)juno.com> >Reply-To: aeroelectric-list(at)matronics.com >To: aeroelectric-list(at)matronics.com >Subject: AeroElectric-List: Pro G Hub by http://www.approachfaststack.com/ >Date: Wed, 14 Mar 2007 14:08:10 -0400 > > >Hi Frank, > I have the Approach Pro G Hub in my "9". There is one thing you >need to do if considering using them for wiring. It simplifies the wires >but you must give them exactly what you are using and the options you >will be using. Brand name of wing levelers, EFIS (if you are using them >and what extras you will use from them) comm radios, Intercom and model >and if its stereo / monoral, transponders and any interfacing required >(such as mode "S", and if the altitude encoding is to be serial input or >gray code.) All these things are necessary to get a good cable interface >with their system. I'm not flying yet but I will be doing soon. So far >the checks seem to be ok. > Place you hub is a position behind your panel so you can get to >it and remove the plug in 's You have to be able to twist the locking >screws on the "D" sub B ends. It gets real busy so plan for the >transition of the cables thru the bulkheads and around to the units >desired. I cut several 2" holes to get the wiring where it needed to go. > > >Jim Nelson >www.websites.expercraft.com/jimn > > _________________________________________________________________ Find what you need at prices youll love. Compare products and save at MSN Shopping. http://shopping.msn.com/default/shp/?ptnrid=37,ptnrdata=24102&tcode=T001MSN20A0701 ________________________________________________________________________________
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
From: "N395V" <n395v(at)hughes.net>
Date: Mar 14, 2007
Frank, I considered faststack when I wired my panel but I enjoy doing the wiring myself so I did not go that route and have no first hand knowledge relative to the product. Below however are links to some discussions by others who have. Fast Stack 1 (http://www.bluemountainavionics.com/talk/showthread.php?t=1121&highlight=Fast+Stack+Hub) Fast Stach 2 (http://www.bluemountainavionics.com/talk/showthread.php?t=1252&highlight=Fast+Stack+Hub) Fast Stack 3 (http://www.bluemountainavionics.com/talk/showthread.php?t=1261&highlight=Fast+Stack+Hub) -------- Milt N395V F1 Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100542#100542 ________________________________________________________________________________
Date: Mar 14, 2007
From: Brett Ferrell <bferrell(at)123mail.net>
Subject: Pro G Hub by http://www.approachfaststack.com/
Frank, Well, I consider my panel a fairly complex IFR system, so I would disagree, even though I'm not flying. I haven't found something I wanted or needed that it couldn't do, so I'm not sure where that opinion would come from to be honest. Brett Quoting Frank Stringham : > > > Jim, Brett and the rest of you good folks > > I am running with this thread on the Vansairforce forum and some over there > seem to think that if the panel is simple VFR the hub is fine, but the more > complex the panel the less capable the hub would be. At first blush I > believe these are well meaning opinoins not based on facts. So are they > talking fact or opinion. > > TIA > > Frank @ SGU RV7A "NDY" > > > >From: James H Nelson <rv9jim(at)juno.com> > >Reply-To: aeroelectric-list(at)matronics.com > >To: aeroelectric-list(at)matronics.com > >Subject: AeroElectric-List: Pro G Hub by http://www.approachfaststack.com/ > >Date: Wed, 14 Mar 2007 14:08:10 -0400 > > > > > >Hi Frank, > > I have the Approach Pro G Hub in my "9". There is one thing you > >need to do if considering using them for wiring. It simplifies the wires > >but you must give them exactly what you are using and the options you > >will be using. Brand name of wing levelers, EFIS (if you are using them > >and what extras you will use from them) comm radios, Intercom and model > >and if its stereo / monoral, transponders and any interfacing required > >(such as mode "S", and if the altitude encoding is to be serial input or > >gray code.) All these things are necessary to get a good cable interface > >with their system. I'm not flying yet but I will be doing soon. So far > >the checks seem to be ok. > > Place you hub is a position behind your panel so you can get to > >it and remove the plug in 's You have to be able to twist the locking > >screws on the "D" sub B ends. It gets real busy so plan for the > >transition of the cables thru the bulkheads and around to the units > >desired. I cut several 2" holes to get the wiring where it needed to go. > > > > > >Jim Nelson > >www.websites.expercraft.com/jimn > > > > > > > > > > _________________________________________________________________ > Find what you need at prices youll love. Compare products and save at MSN > Shopping. > http://shopping.msn.com/default/shp/?ptnrid=37,ptnrdata=24102&tcode=T001MSN20A0701 > > ________________________________________________________________________________
Date: Mar 14, 2007
From: Mitchell Faatz <mitch(at)skybound.com>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
I purchased the Pro-G Hub, and I must say the company has been EXCELLENT to work with. I've emailed them quite a few times with questions about wiring and interconnections and they have almost always returned my email by the next day. I have a fairly complex panel (430, 330, STEC-30 autopilot, GPSS, Serial blind encoder, custom moving map, etc) and having them as a resource for wiring questions was worth the additional price I believe. Mitch Faatz RV-6A Finish Kit Auburn, CA Frank Stringham wrote: > > > Any experience in the group with the products (Pro G Hub) supplied by > Approach Fast Stack http://www.approachfaststack.com . At first > glance it looks like a real elegant way to interconnect the > insturments in the panel. > > Some of the questions I have include: 1. How is the company to work > with? Is the install as easy as they say! Any maintence issues? > > Frank @ SGU RV7A "NDY" > > _________________________________________________________________ > Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a > month. Intro*Terms > https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search=mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 > > ________________________________________________________________________________
Date: Mar 14, 2007
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
From: "Matt Prather" <mprather(at)spro.net>
Has anyone actually gone through the process of changing/upgrading radios that are installed with one of these systems? The website says they support that, but I didn't see any details on how it's done, and how much it costs to do so.. Regards, Matt- > > > I purchased the Pro-G Hub, and I must say the company has been EXCELLENT > to work with. I've emailed them quite a few times with questions about > wiring and interconnections and they have almost always returned my > email by the next day. I have a fairly complex panel (430, 330, STEC-30 > autopilot, GPSS, Serial blind encoder, custom moving map, etc) and > having them as a resource for wiring questions was worth the additional > price I believe. > > Mitch Faatz RV-6A Finish Kit Auburn, CA > > > Frank Stringham wrote: >> >> >> Any experience in the group with the products (Pro G Hub) supplied by >> Approach Fast Stack http://www.approachfaststack.com . At first >> glance it looks like a real elegant way to interconnect the >> insturments in the panel. >> >> Some of the questions I have include: 1. How is the company to work >> with? Is the install as easy as they say! Any maintence issues? >> >> Frank @ SGU RV7A "NDY" >> >> _________________________________________________________________ >> Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a >> month. Intro*Terms >> https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search=mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 >> >> >> >> >> >> > > ________________________________________________________________________________
From: "Michel Creek" <mwcreek(at)frontiernet.net>
Subject: Re: RF noise from EFIS
Date: Mar 14, 2007
Mike, Thanks, that is good info. Would you be willing to comment on Advanced Flight Systems, Dynon, and Grand Rapids? I'll be making panel decisions in May so your experience could help me out a lot and I suspect I'm not alone. I'll be mostly day and night VFR but want the option to do light IFR in the future. Thanks, Mike Creek -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Mike Sent: Wednesday, March 14, 2007 7:25 AM Subject: RE: AeroElectric-List: Re: RF noise from EFIS I totally agree with Bob. My experience with BMA and the folks there have been the worst for me as compared to ALL of the other companies I deal with (to many to list). Let's summarize, BMA produces products that at face value looks cool and if it worked as advertised would be a good product. But when you dig into the finer points of BMA products such as: stability, installation, customer service, ergonomics, builder philosophy, function, and price they all fall short as compared to almost ALL the others. I work in the field with builders of experimental homebuilt airplanes. I spent seven years in an avionics shop, three years on a military R&D project, and 30 years total aircraft maintenance. I am not very polished in my delivery of words when it comes to basic avionics. I express my experience and you take it for what its worth. Here in Arizona we have a large group of builders who are actively building. We do not have any real profession support for avionics available here, so we get by with the local knowledge and experience of all the engineers and techs. here and of course Lectric Bob. So far we've had many successes and few failures. Of the 35+ airplanes under construction (not flying yet) that I have worked on in the past 365 days (this past year). I have seen my share of BMA products (including my own). After dealing with BMA too many times with problems I don't even call them any more. I can say that I have over 12 saves this past year regarding folks purchasing BMA stuff. Those of you who have purchased BMA and managed to get it to work to an acceptable level that's great. I would just like to say there are a whole host of products out there that perform much better. Mike Larkin -----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 Sent: Wednesday, March 14, 2007 8:06 AM Subject: Re: AeroElectric-List: Re: RF noise from EFIS > > > > Which suggests a profound lack of knowledge as > > to how noises should be kept inside the product > > >You just can't resist a dig at Greg can you? I can't resist a dig at poor science and equally poor teaching. Read my most earnest attempts to engage Greg in lucid, useful dialog at: http://aeroelectric.com/articles/richter/richter.html This exchange took place AFTER he took a whack at the AeroElectric Connection when he said, "I've seen so much truly atrocious work, much of it per Bob's book". But when asked to point out any writing in the 'Connection so poorly written as to induce one to do atrocious work, he was silent. >Now I know why so many others think you are an asshole. This isn't about me and Greg, it's about doing the best we know how to do for a price that a customer is happy to have paid. Products offered from the BMA website fall demonstrably short of those goals. I kept my assessments to myself for years but Greg chose to open the door with no prompting from me. He then demonstrated a lack of ability and/or willingness to engage in good critical review. I can't help what people think when they're offering opinions based upon a lack of knowledge and understanding. I'll invite you to hang around the list for awhile and gather enough data about me and what the List is about toward the goal of formulating your own, informed opinion. Bob . . . -- 2/8/2007 ________________________________________________________________________________
From: RURUNY(at)aol.com
Date: Mar 14, 2007
Subject: Re: RF noise from EFIS
I've got a similar problem on my Zenith 701. I wired the loudspeaker to the ICOM A200 as per its drawings mounted on the front of the passenger seat. With my Dynon D10A on full bright I hear no buzzing noise...but when I dim the Dynon using its built in dimming feature in the menu system, the buzz gets louder and at a different frequency. The more I dim the worse it is. I'm using single point ground. No buzzing in headsets though, maybe the noise is going directly into the A200 to speaker and not into the 403MC intercom to headsets. Whatever is used to dim your EFIS might be making the noise. Something to play with... Brian Unruh Long Island, NY _www.701Builder.com_ (http://www.701Builder.com)


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From: <frank.phyllis(at)mindspring.com>
Subject: Popped CB
Date: Mar 14, 2007
I'll add the diode. Re the alternator not charging. This is a new engine with first starts so there's no history--hasn't worked from the beginning. Frank -----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 Sent: Wednesday, March 14, 2007 12:45 PM Subject: RE: AeroElectric-List: Popped CB > >Bob, >The CB popped when I released the starter contactor (switch with key). >Master was on BAT & ALT. I tried starting with just BAT & it did not >pop. It did not pop when I switched to Alt after starting with Bat >only. > >I noticed this time I'm not getting a charge from Alt (verified master >switch on Alt) at 2400RPM. Hmmm . . . this needs troubleshooting. Has it worked in the past? >I overlooked the diode on the starter contactor so, no, I do not have >one. Maybe that's the problem??? I'll bet on it. But in any case, starting with the alternator off is a reasonable procedure too. However, your starter switch will appreciate having the diode added. Bob . . . ________________________________________________________________________________
Date: Mar 14, 2007
From: Matt Reeves <mattreeves(at)yahoo.com>
Subject: Re: Pro G Hub by http://www.approachfaststack.com/
I have the Pro G hub in my Lancair and have changed out radios a couple of times and now have a nice Garmin stack with indicators, etc. My brother has the same set up. The company has been sold a couple of years ago and the new company has been just as awesome as the old company. The cables are top notch and well labelled and easy to install - only taking a few seconds. You will have some stragglers for power, etc, but they are well marked. No power goes through the hub so you don't have to worry about FAA paperwork, etc. I swear by it. My avionics guy inspected the cables and set up and said they use the best quality connectors, wire, labels, etc. He was very impressed. THE main reason I bought it is so I can change avionics whenever I want and not have to rewire a whole panel. My vote - LOVE it. Matt Reeves Rochester, NY Matt Prather wrote: Has anyone actually gone through the process of changing/upgrading radios that are installed with one of these systems? The website says they support that, but I didn't see any details on how it's done, and how much it costs to do so.. Regards, Matt- > > > I purchased the Pro-G Hub, and I must say the company has been EXCELLENT > to work with. I've emailed them quite a few times with questions about > wiring and interconnections and they have almost always returned my > email by the next day. I have a fairly complex panel (430, 330, STEC-30 > autopilot, GPSS, Serial blind encoder, custom moving map, etc) and > having them as a resource for wiring questions was worth the additional > price I believe. > > Mitch Faatz RV-6A Finish Kit Auburn, CA > > > Frank Stringham wrote: >> >> >> Any experience in the group with the products (Pro G Hub) supplied by >> Approach Fast Stack http://www.approachfaststack.com . At first >> glance it looks like a real elegant way to interconnect the >> insturments in the panel. >> >> Some of the questions I have include: 1. How is the company to work >> with? Is the install as easy as they say! Any maintence issues? >> >> Frank @ SGU RV7A "NDY" >> >> _________________________________________________________________ >> Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a >> month. Intro*Terms >> https://www2.nextag.com/goto.jsp?product=100000035&url=%2fst.jsp&tm=y&search=mortgage_text_links_88_h27f6&disc=y&vers=743&s=4056&p=5117 >> >> >> >> >> >> > > --------------------------------- Now that's room service! Choose from over 150,000 hotels in 45,000 destinations on Yahoo! Travel to find your fit. ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Re: RF noise from EFIS
Date: Mar 14, 2007
Mike, I have worked with all of the companies you have listed. I will try and keep this brief. A quick note, I find that the best way to figure out what you need it to start with the systems that have the functions you want and then start sorting out the weaker ones. Do a pro / con list. Advanced Flight Systems, they make very good products. I have only worked with their AF-2002/AF-2500 engine monitor. It's a great product, very stable, and most importantly the people are great to work with. For example, one system we were installing had a power problem and the AFS folks worked with us until we figured it out. They were ready to send a new unit if that's what it took. Every time I speak with them it's a great experience. I have seen their EFIS unit and chatted with them about it but have not installed or flown behind one yet. If it is like their other products it should be great. Dynon, I was one of their first customers back in the D-10 days. The company was small and the product very new. I had some minor problems and they were very quick to fix address them. Since that time I have worked on some installations with the newer units and find the product much improved from version one. The people there are easy to work with and know their product well. I have only experienced one failure and that was a new unit that would not boot properly and Dynon repaired it in record time. Grand Rapids Technology, I have two GRT EIS systems myself and have installed many of their ADC units on the crossbow Chelton EFIS systems. Their stuff isn't the most glamorous, but it works very well and I have not seen one fail yet. I have chatted with them many time at various shows and for tech support and they are always very knowledgeable and helpful. As far as the EFIS system goes, I have only flown behind one. I have not personal installed one. If you have more questions, email me at mlas(at)cox.net. I will be away until March 18th. Mike Larkin -----Original Message----- Mike, Thanks, that is good info. Would you be willing to comment on Advanced Flight Systems, Dynon, and Grand Rapids? I'll be making panel decisions in May so your experience could help me out a lot and I suspect I'm not alone. I'll be mostly day and night VFR but want the option to do light IFR in the future. Thanks, Mike Creek -- 2/8/2007 ________________________________________________________________________________
From: Jerry2DT(at)aol.com
Date: Mar 15, 2007
Subject: Re: wiring diagram benefits?
Just do it, you'll be happy you did, and may hate yourself if not I will do my first flight next week, and so far there have been 3 issues regarding electrical stuff which were a piece of cake to track down and fix because I took the trouble to do a 6 page diagram with Z11 as a base. Here's the deal... I wired it last year, and if you think you'll remember all those pathways about 2 years after first flight, you have a lot better memory than myself.It was a mystery to me until I pulled out my handy-dandy wirebook... Voila!!! No problema!!! HTH, Jerry Cochran Subject: AeroElectric-List: wiring diagram benefits? From: Erich_Weaver(at)URSCorp.com I may be asking for a beating here, but exactly why should I create detailed wiring diagrams? I wired my RV-7A myself following the Z-13/8


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AOL now offers free email to everyone. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
From: TSaccio(at)aol.com
Date: Mar 15, 2007
Subject: Re: ectric-List:Batteries
Hi Bob, It's Tom Saccio here. I need some advice. I'm at the point where I need to by some Batteries for the Seawind. I was thinking of two Odyssey batteries. As you know I have an all electric System. Two alternators two regulators. My panel has the Chelton sport system the MX200 and the Garmin 480. If you could give me some suggestions as to the type and size of the batteries I would need, it would be greatly appreciated. There are two separate busses so that if one alternator goes out, I can switch over to the other. At some point if you could give me your travel itinerary we could make arrangements to meet up. Thanks, Tom Saccio _tsaccio(at)aol.com_ (mailto:tsaccio(at)aol.com)


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AOL now offers free email to everyone. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
From: "Darwin N. Barrie" <ktlkrn(at)cox.net>
Subject: Pro G hub
Date: Mar 15, 2007
As typical of many discussions people throw out comments without specific experience with the product. After reviewing many of the posts here are my comments. First, the company was sold a while back and is in the hands of some great people in Minnesota. I purchased mine from the previous owners. I was working on an issue and contacted the new owner (Tim) and he was 100% helpful. The previous people were great too. Everything worked as it should from the first time the power was applied. There were a couple of minor issues encountered that are discussed below. Someone mentioned the weight difference. I think in the overall scheme it may add a little but so does failing to go to the bathroom before flying!!! It will handle ANY system. As far as upgrading, it is as simple as adding the appropriate cable. There may be a chance you would have to send in the hub, but not sure. How many people change out their panel anyway. If you needed to can the who thing, this would be the cheapest thing to replace anyway. You get the complete wiring diagram and specific "pin outs" for each cable. Not being familiar with this aspect of building, I found the diagrams and pinouts easy to read. I mounted the Hub just behind the panel (tip up) on the right side. It is 100% accessible and looks very neat with the cables tied together and running to the avionics. All of the cables have the computer look with sealed connectors at each end. (except the audio panel at the avionics end) I figure I added about $400 to the overall cost of the wiring with the system. The $400 was well worth the reduction of the BS factor on the install. The install is quite simple with biggest issue being the audio panel with lots of loose wires to find their homes. I have the Pro G hub with the following equipment integrated with the hub. Garmin 340 audio panel Garmin 430 GPS Nav/Comm Garmin SL40 Garmin 330 Mode S transponder Garmin 106A CDI Trutrak Digiflight II VSGV auto pilot ACK encoder The only issues I had with the purchase was not know what the full capabilities of the avionics I selected. As an example, I did not know that I needed 4 unswitched audios for various components. The old Approach Systems apparently did not either and didn't wire for these. With the guidance of Approach Systems I was able to pin out a few more wires. Also the Garmin 330 Mode S transponder has Density Altitude capability if wired for a temperature probe. I did not know this. Again I wired a couple of wires and it was done. I spoke with the new owners about this. I recommended that they conference with customers as to their equipment and the capabilities so everything is wired as desired and the full capabilities are experienced. Tim related they would do that. I should also point out that their knowledge of individual pieces of avionics is exceptional. Since they are an avionics shop the knowledge base is excellent. In summary, if you are concerned about your ability to wire your panel, simple or complex, do not hesitate use the Approach Systems product. Despite the nominal extra cost you will reduce your wiring time 10 fold with a system that works as it is supposed to. Sorry for the length but I wanted to clear up some of the misconceptions reported. Darwin N. Barrie Chandler AZ RV7 N717EE ________________________________________________________________________________
From: "Frank Stringham" <fstringham(at)hotmail.com>
Subject: Pro G hub
Date: Mar 15, 2007
Darwin Thanks for the info....especially knowing it is real world stuff. I think I could wire up the various cables....but why......at least for me this is one area where i will error on the side of an expert. I talked with Tim yesterday and he is a stand up guy. I will proceed with the hub / cable system they provide and thank you and the others that have shed some light on my lack of knowledge. Frank @ SGU RV7A "NDY" >From: "Darwin N. Barrie" <ktlkrn(at)cox.net> >Reply-To: aeroelectric-list(at)matronics.com >To: >Subject: AeroElectric-List: Pro G hub >Date: Thu, 15 Mar 2007 07:59:32 -0700 > >As typical of many discussions people throw out comments without specific >experience with the product. After reviewing many of the posts here are my >comments. First, the company was sold a while back and is in the hands of >some great people in Minnesota. I purchased mine from the previous owners. >I was working on an issue and contacted the new owner (Tim) and he was 100% >helpful. The previous people were great too. Everything worked as it should >from the first time the power was applied. There were a couple of minor >issues encountered that are discussed below. > >Someone mentioned the weight difference. I think in the overall scheme it >may add a little but so does failing to go to the bathroom before flying!!! > >It will handle ANY system. As far as upgrading, it is as simple as adding >the appropriate cable. There may be a chance you would have to send in the >hub, but not sure. How many people change out their panel anyway. If you >needed to can the who thing, this would be the cheapest thing to replace >anyway. > >You get the complete wiring diagram and specific "pin outs" for each cable. >Not being familiar with this aspect of building, I found the diagrams and >pinouts easy to read. > >I mounted the Hub just behind the panel (tip up) on the right side. It is >100% accessible and looks very neat with the cables tied together and >running to the avionics. All of the cables have the computer look with >sealed connectors at each end. (except the audio panel at the avionics end) > >I figure I added about $400 to the overall cost of the wiring with the >system. The $400 was well worth the reduction of the BS factor on the >install. The install is quite simple with biggest issue being the audio >panel with lots of loose wires to find their homes. > >I have the Pro G hub with the following equipment integrated with the hub. > >Garmin 340 audio panel >Garmin 430 GPS Nav/Comm >Garmin SL40 >Garmin 330 Mode S transponder >Garmin 106A CDI >Trutrak Digiflight II VSGV auto pilot >ACK encoder > >The only issues I had with the purchase was not know what the full >capabilities of the avionics I selected. As an example, I did not know that >I needed 4 unswitched audios for various components. The old Approach >Systems apparently did not either and didn't wire for these. With the >guidance of Approach Systems I was able to pin out a few more wires. Also >the Garmin 330 Mode S transponder has Density Altitude capability if wired >for a temperature probe. I did not know this. Again I wired a couple of >wires and it was done. > >I spoke with the new owners about this. I recommended that they conference >with customers as to their equipment and the capabilities so everything is >wired as desired and the full capabilities are experienced. Tim related >they would do that. I should also point out that their knowledge of >individual pieces of avionics is exceptional. Since they are an avionics >shop the knowledge base is excellent. > >In summary, if you are concerned about your ability to wire your panel, >simple or complex, do not hesitate use the Approach Systems product. >Despite the nominal extra cost you will reduce your wiring time 10 fold >with a system that works as it is supposed to. > >Sorry for the length but I wanted to clear up some of the misconceptions >reported. > >Darwin N. Barrie >Chandler AZ >RV7 N717EE > > _________________________________________________________________ Get a FREE Web site, company branded e-mail and more from Microsoft Office ________________________________________________________________________________
Subject: Molex connector sexual orientation
From: "bmeyette" <brianpublic2(at)starband.net>
Date: Mar 15, 2007
I was putting together some Molex connectors for the first time. The plastic parts have a male and a female half. The terminals also are either male or female. However, I am a bit unclear as to how to mate these parts. Intuition would tell me that the male terminals go into the male plastic part. Yet, I have a feeling it's actually the other way around. Is a male metal terminal supposed to go into the male plastic housing, or the female plastic housing, or doesn't it matter? thanks, brian -------- Brian Meyette, Cornish, NH RV-7A QB tipup, Eggenfellner supercharged STi engine, MT CS prop, all glass day/night/IFR panel, being built with solar and wind power N432MM reserved http://brian76.mystarband.net/RV-7Ahome.htm Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100754#100754 ________________________________________________________________________________
Date: Mar 15, 2007
From: Bill Bradburry <bbradburry(at)allvantage.com>
Subject: Re: Pro G Hub
I bought a partially completed Lancair kit and the Pro-G Hub and several cables came with the kit. I have since decided not to use it. It has never been installed. I can make someone a great deal if they are interested. E-mail me off list and I will give you the details of which cables I have, etc. Bill B ________________________________________________________________________________
Date: Mar 15, 2007
From: "Larry James" <larry(at)ncproto.com>
Subject: ANR Headset Power without batteries
I have a Telex Stratus 50D that I ordered with a "Lemo" connector (to use ship's power) and battery pack as an accessory. This battery pack uses 6 each AA batteries. My dilemma is that I own 2 aircraft (both tandem seating) and several headsets (all ANR) and need to eliminate all battery packs. I have a strong dislike of things flopping around in the cockpit. This dilemma seems to be exasperated by the lack of a standard power voltage and connector to drive the ANR in all headsets. My questions are: 1) What voltage does my 50D headset ANR run on ?? The specs in the Telex website differ from my actual unit in that my unit is using 6 ea AA batteries. The website says this unit runs on 4 each AA batteries. If it is running on 9 volts it will help my situation. I've contacted Telex about this and am waiting for an answer. 2) One of my other ANR Headsets is a helmet with Headsets Inc. ANR system that runs on 9vdc. I spoke with Headsets Inc. and he didn't know what connector he is using for the power - would anyone here know ?? 3) Does anyone have a sense of a "standard" connector configuration emerging ?? 4) I believe the connector configuration I will be choosing will be: a. Standard microphone connector b. Standard headset connector c. Similar style but different sized plug for ANR power - powered at 9 vdc. This would allow each headset with this configuration to be used in any of my aircraft; or any other aircraft with either no ANR or an auxiliary battery pack to power the ANR. Would you please give me feedback on this plan ?? Is it optimal ?? 5) What power connector would anyone here recommend ?? 6) Is there any other source for this magic Power Supply to supply good 9 vdc ?? 7) My wife has the Bose headset - I'm guessing it runs off a different voltage given it uses 2 each AA batteries. What can I do to make it fit into my scheme ?? My design goals are: A) Inter-compatibility (or as much as possible) between my headsets and my aircraft. B) No battery packs in my 2 aircraft C) Ability to allow anyone else with standard headsets to plug into my aircraft (with or without their own ANR). D) Ability to use my headsets in other aircraft not equipped with my ANR Power plugs - using an auxiliary battery pack of my own. E) Keep all of my headset cords short with connectors located near my shoulders (I have done this before and it works very well). If this is of interest to anyone else I would be happy to post whatever findings I come up with. Larry E. James Bellevue, WA Super Decathlon Rocket (fuselage / systems) ________________________________________________________________________________
From: "Ron Raby" <ronr(at)advanceddesign.com>
Subject: Re: Molex connector sexual orientation
Date: Mar 15, 2007
Brian Here is the molex web site. You should be able to find your answer here. Regards Ron Raby http://www.molex.com ----- Original Message ----- From: "bmeyette" <brianpublic2(at)starband.net> Sent: Thursday, March 15, 2007 12:40 PM Subject: AeroElectric-List: Molex connector sexual orientation > > > I was putting together some Molex connectors for the first time. The > plastic parts have a male and a female half. The terminals also are > either male or female. > > However, I am a bit unclear as to how to mate these parts. Intuition > would tell me that the male terminals go into the male plastic part. Yet, > I have a feeling it's actually the other way around. > > Is a male metal terminal supposed to go into the male plastic housing, or > the female plastic housing, or doesn't it matter? > > thanks, > brian > > -------- > Brian Meyette, Cornish, NH > > RV-7A QB tipup, Eggenfellner supercharged STi engine, MT CS prop, all > glass day/night/IFR panel, being built with solar and wind power > > N432MM reserved > > http://brian76.mystarband.net/RV-7Ahome.htm > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=100754#100754 > > > ________________________________________________________________________________
Date: Mar 15, 2007
From: Richard Dudley <rhdudley1(at)bellsouth.net>
Subject: Re: Molex connector sexual orientation
Brian, I believe that you can think of the male pins being protected by what you call the "female" shell. The female receptacle pins are protected by being internal in the "male" shell. So both are mechanically shielded by their shells. Hope this helps. Richard Dudley RV-6A flying bmeyette wrote: > >I was putting together some Molex connectors for the first time. The plastic parts have a male and a female half. The terminals also are either male or female. > >However, I am a bit unclear as to how to mate these parts. Intuition would tell me that the male terminals go into the male plastic part. Yet, I have a feeling it's actually the other way around. > >Is a male metal terminal supposed to go into the male plastic housing, or the female plastic housing, or doesn't it matter? > >thanks, >brian > >-------- >Brian Meyette, Cornish, NH > >RV-7A QB tipup, Eggenfellner supercharged STi engine, MT CS prop, all glass day/night/IFR panel, being built with solar and wind power > >N432MM reserved > >http://brian76.mystarband.net/RV-7Ahome.htm > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=100754#100754 > > > > ________________________________________________________________________________
From: "Bruce Gray" <Bruce(at)glasair.org>
Subject: Molex connector sexual orientation
Date: Mar 15, 2007
The male pins go in the female connector. Such is life! Bruce www.glasair.org -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of bmeyette Sent: Thursday, March 15, 2007 1:40 PM Subject: AeroElectric-List: Molex connector sexual orientation I was putting together some Molex connectors for the first time. The plastic parts have a male and a female half. The terminals also are either male or female. However, I am a bit unclear as to how to mate these parts. Intuition would tell me that the male terminals go into the male plastic part. Yet, I have a feeling it's actually the other way around. Is a male metal terminal supposed to go into the male plastic housing, or the female plastic housing, or doesn't it matter? thanks, brian -------- Brian Meyette, Cornish, NH RV-7A QB tipup, Eggenfellner supercharged STi engine, MT CS prop, all glass day/night/IFR panel, being built with solar and wind power N432MM reserved http://brian76.mystarband.net/RV-7Ahome.htm Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100754#100754 ________________________________________________________________________________
Date: Mar 15, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: Molex connector sexual orientation
bmeyette wrote: > >I was putting together some Molex connectors for the first time. The plastic parts have a male and a female half. The terminals also are either male or female. > >However, I am a bit unclear as to how to mate these parts. Intuition would tell me that the male terminals go into the male plastic part. Yet, I have a feeling it's actually the other way around. > >Is a male metal terminal supposed to go into the male plastic housing, or the female plastic housing, or doesn't it matter? > > > While technically it will work either way, the convention is that boys go with girls. Your intuition is correct in this case. -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Date: Mar 15, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: ANR Headset Power without batteries
I have Telex headsets, and they use a miniDIN connector into their battery pack. I made up small connector panels for each of the headset positions, placed them close to the shoulders as you described, and ran a twisted pair to each. The twisted pairs all come back to an LM317 based power regulator set to provide 9V. Any headsets I purchase will be 9V compatible. I can add the miniDIN connector if it isn't there already. 4 AAs will be 6V I believe, and 2 AAs will be 3V. 1.5V for each cell. But they may be wired in parallel within the battery pack, instead of in series. Series configuration multiplies the voltage. Parallel configuration multiplies the (capability to supply) current. It's not save to assume. It would be relatively easy to set up the LM317 to switch between regulating resistors, but you stand a STRONG chance of ruining a very expensive piece of headset gear. If you must have varied types of headsets, the real solution is to have construct a regulator for each, put it in a tiny box that stays attached to the ANR power cord and will then interface with ships power. You can set each headset to what it expects. Larry James wrote: > My design goals are: > > A) Inter-compatibility (or as much as possible) between my headsets > and my aircraft. > > B) No battery packs in my 2 aircraft > > C) Ability to allow anyone else with standard headsets to plug into my > aircraft (with or without their own ANR). > > D) Ability to use my headsets in other aircraft not equipped with my > ANR Power plugs using an auxiliary battery pack of my own. > > E) Keep all of my headset cords short with connectors located near my > shoulders (I have done this before and it works very well). > -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Subject: ANR Headset Power without batteries
Date: Mar 15, 2007
From: David Chalmers <david(at)ChalmersFamily.com>
In my Quickie Q200 I installed Bose connectors and paralleled them up with standard headphone/microphone jacks to allow use of either Bose powered headsets or regular headsets. Works great but you need a battery pack for other ANR headsets. If I did it again I would just install Bose connectors and make up some short pigtails with a Bose male on one end and standard headphone sockets on the other. You could add a power connector to the pigtail for other ANR headsets. To deal with the stereo/mono issue I used stereo headphone jacks with a few hundred ohm resistor in series with left and right to allow use of mono or stereo headphones. IIRC this was suggested by the intercom manufacturer. David Chalmers Redmond,WA Tri-Q200 N4016G -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Larry James Sent: Thursday, March 15, 2007 10:52 AM Subject: AeroElectric-List: ANR Headset Power without batteries I have a Telex Stratus 50D that I ordered with a "Lemo" connector (to use ship's power) and battery pack as an accessory. This battery pack uses 6 each AA batteries. My dilemma is that I own 2 aircraft (both tandem seating) and several headsets (all ANR) and need to eliminate all battery packs. I have a strong dislike of things flopping around in the cockpit. This dilemma seems to be exasperated by the lack of a standard power voltage and connector to drive the ANR in all headsets. My questions are: 1) What voltage does my 50D headset ANR run on ?? The specs in the Telex website differ from my actual unit in that my unit is using 6 ea AA batteries. The website says this unit runs on 4 each AA batteries. If it is running on 9 volts it will help my situation. I've contacted Telex about this and am waiting for an answer. 2) One of my other ANR Headsets is a helmet with Headsets Inc. ANR system that runs on 9vdc. I spoke with Headsets Inc. and he didn't know what connector he is using for the power - would anyone here know ?? 3) Does anyone have a sense of a "standard" connector configuration emerging ?? 4) I believe the connector configuration I will be choosing will be: a. Standard microphone connector b. Standard headset connector c. Similar style but different sized plug for ANR power - powered at 9 vdc. This would allow each headset with this configuration to be used in any of my aircraft; or any other aircraft with either no ANR or an auxiliary battery pack to power the ANR. Would you please give me feedback on this plan ?? Is it optimal ?? 5) What power connector would anyone here recommend ?? 6) Is there any other source for this magic Power Supply to supply good 9 vdc ?? 7) My wife has the Bose headset - I'm guessing it runs off a different voltage given it uses 2 each AA batteries. What can I do to make it fit into my scheme ?? My design goals are: A) Inter-compatibility (or as much as possible) between my headsets and my aircraft. B) No battery packs in my 2 aircraft C) Ability to allow anyone else with standard headsets to plug into my aircraft (with or without their own ANR). D) Ability to use my headsets in other aircraft not equipped with my ANR Power plugs - using an auxiliary battery pack of my own. E) Keep all of my headset cords short with connectors located near my shoulders (I have done this before and it works very well). If this is of interest to anyone else I would be happy to post whatever findings I come up with. Larry E. James Bellevue, WA Super Decathlon Rocket (fuselage / systems) ________________________________________________________________________________
Date: Mar 15, 2007
From: Ken <klehman(at)albedo.net>
Subject: Re: Molex connector sexual orientation
Yes that is what I do. In addition though I always arrange that the male shell (plastic surrounds each female pin) is wired to the side that is hot (hardwired to aircraft power). That insures that two pins can't be pushed together and short out the power source. These are low cost connectors and that can happen even sometimes while trying to connect the two halves. Ken Murphy Rebel, subaru ej22, built with cheap grid power in a shop heated by wood grown with solar power... ;) Richard Dudley wrote: > > > Brian, > I believe that you can think of the male pins being protected by what > you call the "female" shell. The female receptacle pins are protected > by being internal in the "male" shell. So both are mechanically > shielded by their shells. > Hope this helps. > Richard Dudley > RV-6A flying > > bmeyette wrote: > >> >> >> I was putting together some Molex connectors for the first time. The >> plastic parts have a male and a female half. The terminals also are >> either male or female. >> >> However, I am a bit unclear as to how to mate these parts. >> Intuition would tell me that the male terminals go into the male >> plastic part. Yet, I have a feeling it's actually the other way around. >> >> Is a male metal terminal supposed to go into the male plastic >> housing, or the female plastic housing, or doesn't it matter? >> >> thanks, >> brian >> >> -------- >> Brian Meyette, Cornish, NH >> >> RV-7A QB tipup, Eggenfellner supercharged STi engine, MT CS prop, all >> glass day/night/IFR panel, being built with solar and wind power >> >> N432MM reserved >> >> http://brian76.mystarband.net/RV-7Ahome.htm > > ________________________________________________________________________________
Date: Mar 15, 2007
From: Ralph Hoover <hooverra(at)verizon.net>
Subject: ANR Headset Power without batteries
Larry, I just received Jacks for my Headsets Inc. install from Mouser. If you wish to isolate the ground you will also need .312 I.D. Shoulder washers. I didn't order any and had to machine a pair!! www.mouser.com ----------------------------------------------------------------- ORDERED STOCK NUMBER SHIPPED PRICE EXTENDED ----------------------------------------------------------------- 2 502-L722A 2 4.290 8.58 Switchcraft L722A DC Jacks PWR JCK LNG BSHG "2) One of my other ANR Headsets is a helmet with Headsets Inc. ANR system that runs on 9vdc. I spoke with Headsets Inc. and he didnt know what connector he is using for the power would anyone here know ??" -- Ralph C. Hoover RV7A hooverra at verizon dot net ________________________________________________________________________________
Date: Mar 15, 2007
From: Ralph Hoover <hooverra(at)verizon.net>
Subject: ANR Headset Power without batteries
Carl, The jury is still out,I have not flown with the ANR conversion yet. When I first turned them on in the shop the fan the was running disappeared. It seems like they will work just fine. Headsets Inc recommends there power adaptor, I believe I will brew my own although I am planning on using a switching regulator. The converter they supply is ground isolated and that is what I plan on replicating. The converter I selected is on backorder until the end of April :( . The audio and dc power share grounds so there is a chance of introducing noise into the system using a LM317 locally at the jacks. I may try the LM317, it sure is a lot simpler and cheaper (LM317's) live in my junk box! The actual installation of the ANR modules was straightforward, the hardware is well done. I replaced the cable with the optional cable that they offer as I don't like the idea of the power cable zip tied to the audio cable. -- Ralph C. Hoover RV7A hooverra at verizon dot net ________________________________________________________________________________
From: "Carl Morgan" <zk-vii(at)rvproject.gen.nz>
Subject: ANR Headset Power without batteries
Date: Mar 16, 2007
Can you provide some details of the ground isolated converter that you are looking at - I'm just starting on the learning curve for the PCB type stuff - would be good to see / try and understand how it could be done. $50 per 9V regulated supply seems a bit steep to me..... Likewise I would go with a single cord - otherwise looks a bit 'amateurish', and going DC Mono H10-13.4 to stereo ANR is attractive. Cheers, Carl > -----Original Message----- > From: Ralph Hoover [mailto:hooverra(at)verizon.net] > Sent: Friday, 16 March 2007 3:39 p.m. > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: ANR Headset Power without batteries > > > > > Carl, > The jury is still out,I have not flown with the ANR conversion yet. > When I first turned them on in the shop the fan the was running > disappeared. It seems like they will work just fine. Headsets Inc > recommends there power adaptor, I believe I will brew my own although I > am planning on using a switching regulator. The converter they supply is > ground isolated and that is what I plan on replicating. The converter I > selected is on backorder until the end of April :( . The audio and dc > power share grounds so there is a chance of introducing noise into the > system using a LM317 locally at the jacks. I may try the LM317, it sure > is a lot simpler and cheaper (LM317's) live in my junk box! > The actual installation of the ANR modules was straightforward, the > hardware is well done. I replaced the cable with the optional cable that > they offer as I don't like the idea of the power cable zip tied to the > audio cable. > > -- > Ralph C. Hoover > RV7A > hooverra at verizon dot net ________________________________________________________________________________
Date: Mar 16, 2007
From: Dave N6030X <N6030X(at)DaveMorris.com>
Subject: Single radio, two frequencies
Does anyone know of a COM radio that can monitor the standby frequency at the same time as the primary frequency, as the XCOM 760 does? I'm looking for one in a standard thin radio stack form factor as opposed to a round instrument package. Basically I'm looking for a way to eliminate one of my two COM radios but maintain the ability to listen to ATIS/AWOS without leaving the primary frequency I'm on. Dave Morris ________________________________________________________________________________
Date: Mar 16, 2007
From: Richard Dudley <rhdudley1(at)bellsouth.net>
Subject: Re: Single radio, two frequencies
Dave, You mentioned a COM radio. The SL-30 NAV/COM has the capability of monitoring a standby frequency while being tuned to a primary one. It also has a very thin vertical profile with standard width. Regards, Richard Dudley RV-6A flying Dave N6030X wrote: > > > Does anyone know of a COM radio that can monitor the standby frequency > at the same time as the primary frequency, as the XCOM 760 does? I'm > looking for one in a standard thin radio stack form factor as opposed > to a round instrument package. > > Basically I'm looking for a way to eliminate one of my two COM radios > but maintain the ability to listen to ATIS/AWOS without leaving the > primary frequency I'm on. > > Dave Morris > > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 16, 2007
Subject: Re: Single radio, two frequencies
Good Morning Dave, The Garmin SL 30 and SL 40 both have that capability. Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 3/16/2007 8:48:36 A.M. Central Daylight Time, N6030X(at)DaveMorris.com writes: --> AeroElectric-List message posted by: Dave N6030X Does anyone know of a COM radio that can monitor the standby frequency at the same time as the primary frequency, as the XCOM 760 does? I'm looking for one in a standard thin radio stack form factor as opposed to a round instrument package. Basically I'm looking for a way to eliminate one of my two COM radios but maintain the ability to listen to ATIS/AWOS without leaving the primary frequency I'm on. Dave Morris ************************************** AOL now offers free email to everyone. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
Date: Mar 16, 2007
Subject: Re: Single radio, two frequencies
From: john(at)ballofshame.com
How much do you want to spend? The Garmin SL40 is a very nice radio with standby frequency monitoring. -John www.ballofshame.com > > > Does anyone know of a COM radio that can monitor the standby > frequency at the same time as the primary frequency, as the XCOM 760 > does? I'm looking for one in a standard thin radio stack form factor > as opposed to a round instrument package. > > Basically I'm looking for a way to eliminate one of my two COM radios > but maintain the ability to listen to ATIS/AWOS without leaving the > primary frequency I'm on. > > Dave Morris > > ________________________________________________________________________________
From: "Bill Denton" <bdenton(at)bdenton.com>
Subject: Single radio, two frequencies
Date: Mar 16, 2007
Garmin SL40 Com only Garmin SL30 Nav/Com -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Dave N6030X Sent: Friday, March 16, 2007 8:43 AM Subject: AeroElectric-List: Single radio, two frequencies Does anyone know of a COM radio that can monitor the standby frequency at the same time as the primary frequency, as the XCOM 760 does? I'm looking for one in a standard thin radio stack form factor as opposed to a round instrument package. Basically I'm looking for a way to eliminate one of my two COM radios but maintain the ability to listen to ATIS/AWOS without leaving the primary frequency I'm on. Dave Morris ________________________________________________________________________________
From: Prue Motorgliders <pruemotorgliders(at)cox.net>
Subject: Re: Single radio, two frequencies
Date: Mar 16, 2007
Dave King made a 2 channel frequency selection tied into one transmit section. I have one stored and am not sure of the model number but think it is similar in form to a KX-170. Its old technology and probably does not meet current frequency requirements. I assume more info is available from the experienced people. I can dig it out if there is any interest Jerry N414PM Reserved On Mar 16, 2007, at 6:43, Dave N6030X wrote: > > > Does anyone know of a COM radio that can monitor the standby frequency > at the same time as the primary frequency, as the XCOM 760 does? I'm > looking for one in a standard thin radio stack form factor as opposed > to a round instrument package. > > Basically I'm looking for a way to eliminate one of my two COM radios > but maintain the ability to listen to ATIS/AWOS without leaving the > primary frequency I'm on. > > Dave Morris > > ________________________________________________________________________________
Date: Mar 16, 2007
From: Dave N6030X <N6030X(at)DaveMorris.com>
Subject: Single radio, two frequencies
I had forgotten about the SL-40. I'm trying to come up with an alternative to spending $10,000 on a 430. Thanks for all the suggestions, guys. Dave At 09:04 AM 3/16/2007, you wrote: > >Garmin SL40 Com only > >Garmin SL30 Nav/Com > >-----Original Message----- >From: owner-aeroelectric-list-server(at)matronics.com >[mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Dave >N6030X >Sent: Friday, March 16, 2007 8:43 AM >To: aeroelectric-list(at)matronics.com >Subject: AeroElectric-List: Single radio, two frequencies > > >Does anyone know of a COM radio that can monitor the standby >frequency at the same time as the primary frequency, as the XCOM 760 >does? I'm looking for one in a standard thin radio stack form factor >as opposed to a round instrument package. > >Basically I'm looking for a way to eliminate one of my two COM radios >but maintain the ability to listen to ATIS/AWOS without leaving the >primary frequency I'm on. > >Dave Morris > > ________________________________________________________________________________
From: "Carlos Trigo" <trigo(at)mail.telepac.pt>
Subject: Re: ANR Headset Power without batteries
Date: Mar 16, 2007
Larry I'm not answering to your questions, which are partially also mine. I will appreciate if you share the conclusions you arrived at. TIA Carlos ----- Original Message ----- From: Larry James To: AeroElectric-List(at)matronics.com Sent: Thursday, March 15, 2007 5:52 PM Subject: AeroElectric-List: ANR Headset Power without batteries I have a Telex Stratus 50D that I ordered with a "Lemo" connector (to use ship's power) and battery pack as an accessory. This battery pack uses 6 each AA batteries. My dilemma is that I own 2 aircraft (both tandem seating) and several headsets (all ANR) and need to eliminate all battery packs. I have a strong dislike of things flopping around in the cockpit. This dilemma seems to be exasperated by the lack of a standard power voltage and connector to drive the ANR in all headsets. My questions are: 1) What voltage does my 50D headset ANR run on ?? The specs in the Telex website differ from my actual unit in that my unit is using 6 ea AA batteries. The website says this unit runs on 4 each AA batteries. If it is running on 9 volts it will help my situation. I've contacted Telex about this and am waiting for an answer. 2) One of my other ANR Headsets is a helmet with Headsets Inc. ANR system that runs on 9vdc. I spoke with Headsets Inc. and he didn't know what connector he is using for the power - would anyone here know ?? 3) Does anyone have a sense of a "standard" connector configuration emerging ?? 4) I believe the connector configuration I will be choosing will be: a. Standard microphone connector b. Standard headset connector c. Similar style but different sized plug for ANR power - powered at 9 vdc. This would allow each headset with this configuration to be used in any of my aircraft; or any other aircraft with either no ANR or an auxiliary battery pack to power the ANR. Would you please give me feedback on this plan ?? Is it optimal ?? 5) What power connector would anyone here recommend ?? 6) Is there any other source for this magic Power Supply to supply good 9 vdc ?? 7) My wife has the Bose headset - I'm guessing it runs off a different voltage given it uses 2 each AA batteries. What can I do to make it fit into my scheme ?? My design goals are: A) Inter-compatibility (or as much as possible) between my headsets and my aircraft. B) No battery packs in my 2 aircraft C) Ability to allow anyone else with standard headsets to plug into my aircraft (with or without their own ANR). D) Ability to use my headsets in other aircraft not equipped with my ANR Power plugs - using an auxiliary battery pack of my own. E) Keep all of my headset cords short with connectors located near my shoulders (I have done this before and it works very well). If this is of interest to anyone else I would be happy to post whatever findings I come up with. Larry E. James Bellevue, WA Super Decathlon Rocket (fuselage / systems) ________________________________________________________________________________
Subject: Re: 8AWG Wire to Fast-On Connection
From: "ryan42" <falcobuilder(at)gmail.com>
Date: Mar 16, 2007
Out of curiosity Bob, would you then mainly advocate z-14 for new designs with a 20A alternator. In the past it seems you have suggested z-14 over z-12 for people in the planning stages (correct me if I'm wrong). Maybe a z-14 that uses the second bus as a smaller main alt. out e-bus, not used for starting...smaller battery... In what instance would you use z-12 over z-14 with a 20A alternator? Save a little $ and #? -Ryan (In the pondering stage) Read this topic online here: http://forums.matronics.com/viewtopic.php?p=101129#101129 ________________________________________________________________________________
From: "Rodney Dunham" <rdunhamtn(at)hotmail.com>
Subject: Molex connector sexual orientation
Date: Mar 17, 2007
Brian, It doesn't matter at all! When the two halves are mated together, there is no chance of a short between the pins and you ALWAYS disconnect the BAT ground before fooling with ANYTHING elctrical, don't you??? I use these goodies a lot and I seldom put all of one "sex" on one end. I mix them up so that I can't accidentally connect two connectors that don't belong together. For instance, on my Blue Sea fuse block I twisted pairs and assigned the "1" fuse to the "1" pin on my "molex" connector. The corresponding ground (built in to the Blue Sea fuse block) went to the "2" pin and so on. Grounds are male and +12V are female. There are 6 fuses on one side numbered odd 1 through 11 and 6 on the other side numbered even 2 through 12. So... on the even side, the "1" pin is ground (male) and the "2" pin is +12V (female) and so on... Both shells are female so I cannot accidentally connect the two together. Besides, if the BAT ground is disconnected, it wouldn't hurt to do so anyway! Each wire or bundle is clearly labeled at the connector. I just make each one unigue and there is a good mix of 2, 3, 4, 6, 9 and 12 pin connectors. No two are the same so it isn't possible to connect anything wrong. If it fits, it right! Always read the label. And ALWAYS disconnect BAT ground before working on your plane! Simple. Rodney in Tennessee _________________________________________________________________ i'm making a difference.Make every IM count for the cause of your choice. Join Now. ________________________________________________________________________________
From: "John Richardson" <jrichard(at)ccser.com>
Subject: Comments please on this solid state contactor.......
Date: Mar 17, 2007
Hello Alex I have installed the EV200 contactor in my Lancair Legacy as the master contactor after some investigation. I posted a similar question on the list about a year ago and Bob answered me back (thanks again Bob). He said it looked good from the data sheet, but very expensive when compared to the normal contactors from B&C. I think the current switching and carrying capability is a little over-kill for our applications in light airplanes. However, in an all electric system, I think this is not all bad. There's no weight or size penalty. It's reassuring to note the device has a mechanical life cycle spec and a cycles under load spec. As a master contactor, most of the load is removed during the switching event. Load carrying is speced at 200 A continuous and 500 A for 10 sec. However, as a starter contactor, load switching is an issue but that's where this thing really shines. Because of cost, I ended up using a regular contactor for the starter. The coil energizing circuit is unique. It draws about 3 A during coil pull in then drops back to 0.07 A (24V) to hold. I talked to the design engineer to learn this low holding current is achieved by a pulsing circuit that applies the 3 amps at a very low duty cycle. A possible down side of the pulsing is radio frequency interference. I did a rough test with my handheld placing the antenna all around the device and the coil leads and found no interference across the nav and com bands. I'm not flying yet, so I'm still waiting to conduct the real test. In comparison, a continuous duty standard contactor I have has coil resistance of about 70 ohms for 24 volt operation. At 28 volts that will draw about 0.4 A and dissipate about 11 watts. Not that much in the big picture. Obviously, the EV200 does not get hot at all due to coil current. Finally, it's reassuring to note the coil circuit operates over the range of 9 to 36 volts and will hold in (stay closed) down to 7.5 volts. In a 24 volt system, this is more than adequate margin to operate under low bus voltage, even when starting. I think it's about the same as a 12 v contactor too. It is definitely a quality component and I'm banking on it keeping my two Odyssey PC 625 batteries connected to the panel. Regards, John Richardson -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Alex Sent: Tuesday, March 13, 2007 5:36 PM Subject: AeroElectric-List: Comments please on this solid state contactor....... I have been testing my electrical system on my all- electric Velocity- with no load, only the coils energized for about 30 minutes my battery contactors were both quite hot- too hot to hold for more than say 5 seconds- comments from other builders agree that this is rather normal- someone suggested the "Czonka III" solid state unit- uses no appreciable power- good for tens of thousands of cycles at 200 amps- please see attached PDF- is there any foreseen drawback other than cost? Alex ________________________________________________________________________________
Date: Mar 17, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: How reliable is reliable
> >Out of curiosity Bob, would you then mainly advocate z-14 for new designs >with a 20A alternator. In the past it seems you have suggested z-14 over >z-12 for people in the planning stages (correct me if I'm wrong). Maybe a >z-14 that uses the second bus as a smaller main alt. out e-bus, not used >for starting...smaller battery... > >In what instance would you use z-12 over z-14 with a 20A alternator? Save >a little $ and #? > >-Ryan (In the pondering stage) To my way of thinking, perhaps 1-2% of all OBAM aircraft under construction will be used in ways that justify a Z-14 installation. Here's a post I made in 2005 to a similar question: ------------------------ >Thank you for your thoughtful reply. The 2 batt/2 alt setup (Z11) did get me >excited but the type of flying (very occasional dusk VFR, no IFR, over water >at times) plus a common sensical KISS principle to govern decisions may >dampen my enthusiasm for Z11. Let's try to put some things into perspective. There are tons of dark-n-stormy night stories wherein alternators and batteries are star performers in the role of villain. Given the proven reliability of modern automotive alternators . . . in particular the converted Nipon Denso products from B&C . . . probability of alternator failure is a small fraction of what we've come to expect from certified iron. Combine this with the very robust, sealed lead-acid batteries -AND- a truly meaningful preventative maintenance plan and we've beat the worst worries into submission. If one simply installs Van's a-la C-172 wiring with a modern alternator and well maintained RG battery, probability of having to take a staring role in a dark-n-stormy night play due to electrical systems issues is very low. By taking advantage of variations on a theme described in the z-figures, one can push those probabilities still lower. In 10+ years of suggesting builders consider the e-bus, I've had only one reader write and tell me the e-bus turned an alternator failure into a ho-hum event. However, I've had perhaps a half dozen people write and thank me for the OVM-14 crowbar ov module. Far more folks have experienced an ov condition that forced alternator shutdown than simple alternator failure. I don't recall the numbers of ov experiences that benefited from an e-bus installation after the alternator was shut off. Even if the builder did not have an e-bus, keeping a well maintained RG battery on board goes a long way to saving the day. >In the final analysis, I think it all boils down to whether I want full >electronic ignition, partial, or all mags. If you go electronic ignition, consider at least one p-mag which does not depend on electrical system for operation. >I am finishing the wings which means that I have a long way to go - you'll >see my posts as the situation evolves. I have a client with enough funds to strive for the "ultimate" system which may include dual efis, dual electronic ignition, dual autopilots . . . For the moment, I'm still trying to justify ruling out a Figure Z-13/8 installation thus saving about a 23 pound penalty for going with Z-14. Reliability doesn't have to be heavy or expensive . . . just well considered. Since the e-mag/p-mag guys came along, reliability is getting easier, lighter and less expensive all the time. ------------------ end of quotation ------------------------- If I owned a certified machine, I would endeavor to (1) add ACTIVE NOTIFICATION OF LOW VOLTAGE. (2) install and MAINTAIN an RG battery. (3) Modify the architecture to turn the avionics bus into an E-BUS. (4) When an if the stock alternator craps, I'd get a modern automotive adaptation in place. These simple changes alone would elevate the spam can's SYSTEM reliability by a quantum jump. Implementation of an e-bus/bat-maintenance protocol makes the vast majority of demonstrated concerns go away. Virtually every dark-n-stormy night story I've read that concerned electrical systems would never had been written had the owner-operators of the subject airplanes availed themselves of the knowledge and understanding offered to you here on this List. Now, if you don't plan to have a vacuum system then the vacuum pump pad is open and you'll be many watt-hours ahead in planning for alternator failure by adding the SD-8 and perhaps even downsizing the battery for a wash in weight. Z-13/8 is an exceedingly robust system that should handle everything you or I would want to do at reliability levels that far exceed those of the certified ships that we're ALREADY using do do the same kinds of flights. Now, Z-12 and Z-14 have some appeal but I'd recommend Z-12 only as an upgrade to an existing Z-11 or spam-can clone and Z-14 for ships like a Lancair IVP with full-up dual IFR panels. Obviously, if you have the $time$ and don't mind the weight, you can pile on as many backups to backups that suits your worry levels . . . but I'll suggest that Z-13/8 is the value leader in return for reliability with the lowest investment in $time$ and loss of payload. It would cost more dollars and talented manpower than you or I are willing to expend to put numbers on the relative reliability of Z-13/8 vs Z-14 for the various operating scenarios. But it's my considered judgement that Z-14 is overkill for most of the OBAM aircraft under construction. Bob . . . ________________________________________________________________________________
Date: Mar 17, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: wiring diagram benefits?
>Just do it, you'll be happy you did, and may hate yourself if not I will >do my first flight next week, and so far there have been 3 issues >regarding electrical stuff which were a piece of cake to track down and >fix because I took the trouble to do a 6 page diagram with Z11 as a base. > >Here's the deal... I wired it last year, and if you think you'll remember >all those pathways about 2 years after first flight, you have a lot better >memory than myself.It was a mystery to me until I pulled out my >handy-dandy wirebook... Voila!!! No problema!!! This doesn't have to be time consuming or expensive. Do page per system drawings in pencil and keep a Pink Pearl eraser handy for corrections. You can do the drawings in a 3-ring notebook. When the airplane is done, "fog" the penciled pages with clear Krylon finish to "set" the pencil for longevity that rivals ink. Total time added to your task will be trivial in the grand scheme of things. Further, as others have suggested you'll be glad you did it a few years hence. The wirebook can also cite component part numbers to make spares procurement easier as well. Another thing I've been doing for about the last 7 years or so is ordering parts and supplies as much as possible over the 'net. When an order has be submitted, you almost always get a screen dump of the order that includes where you got the parts, what the numbers are, how much they cost, etc. I print these screens (or e-mail confirmations) to pdf files using Adobe Acrobat (other pdf generators may work as well). Name the file with a date-supplier protocol like 70320B01_Digikey. This decodes to Bob's first purchase on March 20, 2007 and placed with Digikey. When all these files get dumped into a purchasing directory, I have a complete history of orders that sort in date order and can be searched. It takes seconds to record the order to a common data folder and a few seconds longer to search later and find where I purchased an MS21919 clamp or a DPX5050 pressure transducer. When your airplane is done, you can print out these files to paper, punch them and put them in the back of your wirebook too. Takes mere minutes to collect the information and offers fast access to tons of maintenance data. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: "go-fly-away(at)juno.com" <go-fly-away(at)juno.com>
Date: Mar 17, 2007
Subject: Rheostat Diagrams
Hi Bob, I have your book but am looking for proper use of a rheostat to dim the annuciators on a KLN 90-B. I have ground plus the annunciator light wir es. I am having a brain dump on this one. Any suggestions?? Thanks, Mark

Hi Bob,

I have your book but am looking for proper use of a rheostat to dim t he annuciators on a KLN 90-B.  I have ground plus the annunciator l ight wires.  I am having a brain dump on this one.  Any sugges tions??

Thanks,  Mark


      
      
      
________________________________________________________________________________
Date: Mar 17, 2007
From: Dave N6030X <N6030X(at)DaveMorris.com>
Subject: Dragging certified aircraft screaming and kicking into
the 21st Century Bob, for those of us who have certified airplanes and want active notification of low voltage, EI sells a cheap ($285) voice annunciator that will say "Check Bus Voltage" in a soft female voice right into your headset if the voltage drops below 13V, without being hooked to anything but power. (She'll say 16 other things, too, if hooked up to various instruments' alarm outputs). It certainly always gets my attention when I chop the power on approach and switch on the landing light and she reminds me that I'm now sucking some battery power. Also there may be some people who think the annual battery condition test is a complicated process that requires construction of devices with light bulbs and timers and things. I did it yesterday without removing the battery from the airplane. You can do it by replacing whatever crappy ammeter came with your airplane with a Volt-Ammeter like the one from EI. I simply switched on the master and enough additional devices to pull about 4.5A of current (which I have determined in advance is more than sufficient for a daytime VFR cross country in my plane), and then checked back every 15 minutes to see how the voltage was holding up. After 90 minutes, I stopped the test, as the voltage was still holding at 11.81 Volts. That gave me the warm fuzzy that I could take as long as 90 minutes to find my destination and still be assured of plenty of voltage to run my COM radio, transponder. (By the way, I flew today all the way from Dallas down to the 50's diner at Brenham in that amount of time, so 90 minutes is a very long time!) To make the condition test really accurate, one could power up a few more devices and find out if the 4 hour current rating is valid while going to lunch or cleaning up the hangar. (Not sure I would want to fly for more than 4 hours without a pit stop and with no alternator.) Since my certified airplane (1960 vintage Mooney) does not have an E-bus, I have taken the battery load chart, derated it by 20% to be really conservative, and posted a synopsis of Current versus Time in a small chart below my volt-ammeter. (Photo: http://tinyurl.com/38tpwn ) If I suffer a generator failure, I can switch the meter to Amps, turn off devices I don't need, look up the time I should have for that current on the chart, and start my stopwatch. It's not as quick and efficient as an E-bus, but it should get the job done without causing me to break a sweat, and it doesn't require an STC or a 337 or any other governmental bureaucratic safety-inhibiting nonsense. It's doubtful any of the authors of dark and stormy night stories ever went to the trouble to create a little chart like that. It takes 10 minutes to do. I also keep in my flight bag a handheld comm radio with a rechargeable battery pack and a separate alkaline battery pack. Zeftronics makes a line of modern voltage regulators to replace the horrible Delco Remy mechanical gizmo from the 60's with a nice device that features OV and LV lights as well as Overvoltage protection using an external relay. Those are just some of the things I have discovered that hopefully some of the certified people on this list might find useful. Dave Morris www.N6030X.com At 05:46 PM 3/17/2007, you wrote: > If I owned a certified machine, I would endeavor to > (1) add ACTIVE NOTIFICATION OF LOW VOLTAGE. (2) > install and MAINTAIN an RG battery. (3) Modify > the architecture to turn the avionics bus into an > E-BUS. (4) When an if the stock alternator craps, > I'd get a modern automotive adaptation in place. > > These simple changes alone would elevate the spam > can's SYSTEM reliability by a quantum jump. Implementation > of an e-bus/bat-maintenance protocol makes the vast > majority of demonstrated concerns go away. Virtually > every dark-n-stormy night story I've read that concerned > electrical systems would never had been written had > the owner-operators of the subject airplanes availed > themselves of the knowledge and understanding offered > to you here on this List. ________________________________________________________________________________
From: <frank.phyllis(at)mindspring.com>
Subject: Popped CB
Date: Mar 17, 2007
Bob, It looks (in the wiring diagram) like the starter contactor diode is internal. Do I need to purchase another contactor with the diode across the coil or is there a way to add it externally? Re the alternator not charging. This is a new engine with first starts so there's no history--hasn't worked from the beginning. I've re-checked the wiring and it seems to be connected properly but . . . still not showing a charge. Frank -----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 Sent: Wednesday, March 14, 2007 12:45 PM Subject: RE: AeroElectric-List: Popped CB > >Bob, >The CB popped when I released the starter contactor (switch with key). >Master was on BAT & ALT. I tried starting with just BAT & it did not >pop. It did not pop when I switched to Alt after starting with Bat >only. > >I noticed this time I'm not getting a charge from Alt (verified master >switch on Alt) at 2400RPM. Hmmm . . . this needs troubleshooting. Has it worked in the past? >I overlooked the diode on the starter contactor so, no, I do not have >one. Maybe that's the problem??? I'll bet on it. But in any case, starting with the alternator off is a reasonable procedure too. However, your starter switch will appreciate having the diode added. Bob . . . ________________________________________________________________________________
Date: Mar 18, 2007
From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net>
Subject: Non coax to BNC connector.
Have an Electronics International Capacitive Fuel Gauge for Van's capacitive senders in my RV-6 fuel tanks. Van's sender kit included female BNC connectors that are pro-sealed right into the tank. Fuel gauge comes with harness and two sets of short cables (that include converter circuit cards molded into them) that takes two wires out of the tank and converts to three wires for connection to the gauge. The converter cable assemblies have two AWG20 wires going in and three AWG20 wires that connect to the gauge. I need to somehow hook the two AWG20 wires to a BNC male connector to mate with the connector on each tank. The center conductor is a no brainer but what would be the best way to hook the other wire to what would normally be the shield of the coax crimped under the cylindrical cover (on the outside of the coax)? Thanks. Dean RV-6A N197DM Last details before inspection. ________________________________________________________________________________
From: "Mark Banus" <mbanus(at)hotmail.com>
Subject: Dragging certified aircraft screaming and kicking into
Date: Mar 18, 2007
Dave, Do you have a link to the EI voice annunciator? Thanks Mark Banus ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Non coax to BNC connector.
> > >Have an Electronics International Capacitive Fuel Gauge for Van's capacitive >senders in my RV-6 fuel tanks. Van's sender kit included female BNC >connectors that are pro-sealed right into the tank. Fuel gauge comes with >harness and two sets of short cables (that include converter circuit cards >molded into them) that takes two wires out of the tank and converts to three >wires for connection to the gauge. The converter cable assemblies have two >AWG20 wires going in and three AWG20 wires that connect to the gauge. I >need to somehow hook the two AWG20 wires to a BNC male connector to mate >with the connector on each tank. The center conductor is a no brainer but >what would be the best way to hook the other wire to what would normally be >the shield of the coax crimped under the cylindrical cover (on the outside >of the coax)? Thanks. Do you know where I can download the installation manual for your system . . . or do you have it in .pdf form that you can e-mail to me? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Rheostat Diagrams
>Hi Bob, > >I have your book but am looking for proper use of a rheostat to dim the >annuciators on a KLN 90-B. I have ground plus the annunciator light >wires. I am having a brain dump on this one. Any suggestions?? > >Thanks, Mark A simple series rheostat may not be what you want. Do you know if the lighting is incandescent lamps or LEDs? How much current does the lighting input draw? The pinout data I have for the KLN90 reads like there are two 14v lamp strings that are hooked in series for 28v and parallel for 14v systems. A voltage regulating dimmer like http://www.aeroelectric.com/articles//DimmerFabrication.pdf will always work. A rheostat's resistance and wattage needs to be sized to the total load while the voltage regulating dimmer's control functionality is relatively independent of total load and needs only sizing for total load. Is the KLN90 the ONLY circuit you plan to tie onto your dimmer control? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Popped CB
> >Bob, >It looks (in the wiring diagram) like the starter contactor diode is >internal. Do I need to purchase another contactor with the diode across >the coil or is there a way to add it externally? The diode can be inside or outside . . . some of my drawings show it inside because the starter contactor I used to sell had it built in . . . but you can put one on the outside. >Re the alternator not charging. This is a new engine with first starts >so there's no history--hasn't worked from the beginning. I've >re-checked the wiring and it seems to be connected properly but . . . >still not showing a charge. How do you deduce whether or not it's charging? What kind of instrumentation do you have? Bob . . . ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Dragging certified aircraft screaming and kicking
into the 21st Century > >Bob, for those of us who have certified airplanes and want active >notification of low voltage, EI sells a cheap ($285) voice annunciator >that will say "Check Bus Voltage" in a soft female voice right into your >headset if the voltage drops below 13V, without being hooked to anything >but power. (She'll say 16 other things, too, if hooked up to various >instruments' alarm outputs). It certainly always gets my attention when I >chop the power on approach and switch on the landing light and she reminds >me that I'm now sucking some battery power. > >Also there may be some people who think the annual battery condition test >is a complicated process that requires construction of devices with light >bulbs and timers and things. >I also keep in my flight bag a handheld comm radio with a rechargeable >battery pack and a separate alkaline battery pack. > >Zeftronics makes a line of modern voltage regulators to replace the >horrible Delco Remy mechanical gizmo from the 60's with a nice device that >features OV and LV lights as well as Overvoltage protection using an >external relay. > >Those are just some of the things I have discovered that hopefully some of >the certified people on this list might find useful. As you've illustrated, there are several ways to skin this cat . . . have a plan-b. It does take some consideration and PERIODIC verification but there are a variety of ways to do it. Thanks for sharing this with us! Bob . . . ________________________________________________________________________________
Subject: BNC connector
From: "Dennis Jones" <djones(at)northboone.net>
Date: Mar 18, 2007
Bob Help. I can't seem to get a quaility crimp on B and C electrics' BNC male connectors. I have followed your instructions using the RCT crimping tool also from B and C. I used the .213 hex die. I have crimped twice and both times I have come up with a crimped ferrule that has a set of flanges on two sides and some of the flats have a dimple in them. I made sure the round end of the die is facing toward the coax cable. I know the end product is not correct. Could the tool be out of calabration? This is the first time the tool has ever been used. I'am sure it's operator error. What am I to do? Thanks Jonsey Read this topic online here: http://forums.matronics.com/viewtopic.php?p=101464#101464 ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: BNC connector
> > >Bob > >Help. I can't seem to get a quaility crimp on B and C electrics' BNC male >connectors. I have followed your instructions using the RCT crimping tool >also from B and C. I used the .213 hex die. I have crimped twice and both >times I have come up with a crimped ferrule that has a set of flanges on >two sides and some of the flats have a dimple in them. I made sure the >round end of the die is facing toward the coax cable. I know the end >product is not correct. Could the tool be out of calabration? This is the >first time the tool has ever been used. I'am sure it's operator error. >What am I to do? Hmmmm . . . I have encountered tools where the ".213" die was undersized . . . also other brands of connectors that were oversized and would produce the effects you've cited. I used to fit check batches of tools I sold with connectors I sold so as to avoid this situation but I can't speak for B&C's policies on this. Does your tool have a "jam release" lever? If so, don't close the tool down all the way. In fact, when I had a bunch of slightly mis-matched connectors to install I found combination of shim stock pieces that I could close the tool down on to set the crimp and then use the jam-release to get the connector out. If you had a lot of connectors to install, it might be worth the trouble to get a better match but I think I'd just explore the incomplete-closure approach and truck on. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: An extra credit quiz . . .
A writer for Kitplanes attended my seminar in Grass Valley, CA last year and promised to do an aricle about the 'Connection and my seminars. The article appeared in the April issue and I just downloaded a copy. I'd offered to proof it for him last year but he seemed to dismiss the value for doing so. Anyhow, Kitplanes readers here on the List are invited to do a critical review of the article and submit their findings here. For the most part the article was fair and accurate but it does have a few toe-snaggers in it. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: <frank.phyllis(at)mindspring.com>
Subject: Popped CB
Date: Mar 18, 2007
> >Bob, >It looks (in the wiring diagram) like the starter contactor diode is >internal. Do I need to purchase another contactor with the diode across >the coil or is there a way to add it externally? The diode can be inside or outside . . . some of my drawings show it inside because the starter contactor I used to sell had it built in . . . but you can put one on the outside. Is it possible to put a diode on the outside of a three connector relay? >Re the alternator not charging. This is a new engine with first starts >so there's no history--hasn't worked from the beginning. I've >re-checked the wiring and it seems to be connected properly but . . . >still not showing a charge. How do you deduce whether or not it's charging? What kind of instrumentation do you have? I'm using the Grand Rapids Tech EIS. The window where "Voltage" is displayed showed ~ 10.8 volts. Rotax manual indicates a permanent output of 13.5 v. Additionally, the Dynon EFIS would not come on with the Master, but it did come on with the EBus switched on (with the master also on). (When testing during installation I noted previously the Dynon will come on with the master if the battery is fully charged. When battery is not fully charged the Master does not bring it on line but the EBus will.) Frank ________________________________________________________________________________
Subject: Re: How reliable is reliable
From: "ryan42" <falcobuilder(at)gmail.com>
Date: Mar 18, 2007
> Z-13/8 is an exceedingly robust system that should > handle everything you or I would want to do at > reliability levels that far exceed those of the > certified ships that we're ALREADY using do do the > same kinds of flights. > > Now, Z-12 and Z-14 have some appeal but I'd recommend > Z-12 only as an upgrade to an existing Z-11 or spam-can > clone and Z-14 for ships like a Lancair IVP with full-up > dual IFR panels. > > Obviously, if you have the $time$ and don't mind the > weight, you can pile on as many backups to backups that > suits your worry levels . . . but I'll suggest that > Z-13/8 is the value leader in return for reliability > with the lowest investment in $time$ and loss of > payload. > > It would cost more dollars and talented manpower than > you or I are willing to expend to put numbers on the > relative reliability of Z-13/8 vs Z-14 for the various > operating scenarios. But it's my considered judgement > that Z-14 is overkill for most of the OBAM aircraft > under construction. That sounds entirely reasonable. It just seems that by removing the z-13/20 drawing (which I have no problem with), IF the airplane meets the kind of requirements and worry levels to warrent a backup 20 amp alternator, it sounds like you suggest z-14 over z-12 for new ships? Read this topic online here: http://forums.matronics.com/viewtopic.php?p=101525#101525 ________________________________________________________________________________
From: "Dennis Jones" <djones(at)northboone.net>
Subject: BNC connector
Date: Mar 18, 2007
It does have the jamb release. I will try that approach and let you know how it worked. Thanks Again Jonsey -----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 Sent: Sunday, March 18, 2007 4:25 PM Subject: Re: AeroElectric-List: BNC connector > > >Bob > >Help. I can't seem to get a quaility crimp on B and C electrics' BNC male >connectors. I have followed your instructions using the RCT crimping tool >also from B and C. I used the .213 hex die. I have crimped twice and both >times I have come up with a crimped ferrule that has a set of flanges on >two sides and some of the flats have a dimple in them. I made sure the >round end of the die is facing toward the coax cable. I know the end >product is not correct. Could the tool be out of calabration? This is the >first time the tool has ever been used. I'am sure it's operator error. >What am I to do? Hmmmm . . . I have encountered tools where the ".213" die was undersized . . . also other brands of connectors that were oversized and would produce the effects you've cited. I used to fit check batches of tools I sold with connectors I sold so as to avoid this situation but I can't speak for B&C's policies on this. Does your tool have a "jam release" lever? If so, don't close the tool down all the way. In fact, when I had a bunch of slightly mis-matched connectors to install I found combination of shim stock pieces that I could close the tool down on to set the crimp and then use the jam-release to get the connector out. If you had a lot of connectors to install, it might be worth the trouble to get a better match but I think I'd just explore the incomplete-closure approach and truck on. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 18, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: How reliable is reliable
> > > > Z-13/8 is an exceedingly robust system that should > > handle everything you or I would want to do at > > reliability levels that far exceed those of the > > certified ships that we're ALREADY using do do the > > same kinds of flights. > > > > Now, Z-12 and Z-14 have some appeal but I'd recommend > > Z-12 only as an upgrade to an existing Z-11 or spam-can > > clone and Z-14 for ships like a Lancair IVP with full-up > > dual IFR panels. > > > > Obviously, if you have the $time$ and don't mind the > > weight, you can pile on as many backups to backups that > > suits your worry levels . . . but I'll suggest that > > Z-13/8 is the value leader in return for reliability > > with the lowest investment in $time$ and loss of > > payload. > > > > It would cost more dollars and talented manpower than > > you or I are willing to expend to put numbers on the > > relative reliability of Z-13/8 vs Z-14 for the various > > operating scenarios. But it's my considered judgement > > that Z-14 is overkill for most of the OBAM aircraft > > under construction. > > >That sounds entirely reasonable. It just seems that by removing the >z-13/20 drawing (which I have no problem with), IF the airplane meets the >kind of requirements and worry levels to warrent a backup 20 amp >alternator, it sounds like you suggest z-14 over z-12 for new ships? Depends on the airplane and the missions. If you're building a long-legged, $200,000 cross country rocket and you intend to spend hours crossing weather fronts, then something like Z-14 (along with a second pilot in the right seat) is the uptown way to go. If you have an as-purchased airplane wired ah-la C172/ A-36 and you'd like to go all-electric with minimal changes to the system, then Z-12 is an option to consider. If you're starting from scratch and intend to use your airplane like 95% of your brothers use their airplanes, then I'm betting that Z-13/8 has a high probability of meeting your mission requirements at a minimum of cost and weight. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: "Dennis Jones" <djones(at)northboone.net>
Subject: BNC connector
Date: Mar 18, 2007
I tried to no avail. The first stop that caused the ferrule to lock into place caused it to flange and dimple. I will call Bill tomorrow and see if he has an explanation. Jonsey -----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 Sent: Sunday, March 18, 2007 4:25 PM Subject: Re: AeroElectric-List: BNC connector > > >Bob > >Help. I can't seem to get a quaility crimp on B and C electrics' BNC male >connectors. I have followed your instructions using the RCT crimping tool >also from B and C. I used the .213 hex die. I have crimped twice and both >times I have come up with a crimped ferrule that has a set of flanges on >two sides and some of the flats have a dimple in them. I made sure the >round end of the die is facing toward the coax cable. I know the end >product is not correct. Could the tool be out of calabration? This is the >first time the tool has ever been used. I'am sure it's operator error. >What am I to do? Hmmmm . . . I have encountered tools where the ".213" die was undersized . . . also other brands of connectors that were oversized and would produce the effects you've cited. I used to fit check batches of tools I sold with connectors I sold so as to avoid this situation but I can't speak for B&C's policies on this. Does your tool have a "jam release" lever? If so, don't close the tool down all the way. In fact, when I had a bunch of slightly mis-matched connectors to install I found combination of shim stock pieces that I could close the tool down on to set the crimp and then use the jam-release to get the connector out. If you had a lot of connectors to install, it might be worth the trouble to get a better match but I think I'd just explore the incomplete-closure approach and truck on. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 19, 2007
Subject: Will steel affect antenna operation?
From: <rparigor(at)SUFFOLK.LIB.NY.US>
We are doing battle with filling pinholes and small sand marks in Europa fiberglass fuse. After trying several methods, Dolphin Glaze thick and thin, Expancel and Aeropoxy (plastic micro) and Q-Cel and Aeropoxy (glass micro), I tried JB Weld Kwik. Seems the JB Weld Kwik is the hands down winner. It is very thick (thicker than JB Weld) and very sticky. Can squeegee it in place with a razor blade, and get off 99% and it fills everything and does not shrink or allow trapped air to force it into a pimple. Sets up in 4 minutes, full cured pretty hard. JB Kwik uses steel as a filler. I don't think it is conductive. I tried putting a magnet on cured sample and tubes and it does not appear to be conductive. I will have a Com, a Nav/Com and a Transponder Antenna in the fuse and rudder. Think there is a chance that JB Kwik filling small pinholes and very fine scratches, and lets say some areas with one or 2 ten/thousands" skim on it will degrade antenna performance to the point that I should not consider using it? Thanking in advance Ron Parigoris ________________________________________________________________________________
Date: Mar 18, 2007
Subject: Re: Will steel affect antenna operation?
From: "Matt Prather" <mprather(at)spro.net>
My WAG is that the amount/coverage of JB Weld left on the skin will not have any effect on antenna performance. I do, however, wonder about your problems with using epoxy for filling pinholes. I know the EZ builders have had good success filling everything with micro, sanding to 36 grit contour, and then using pure resin to fill pinholes and sanding scratches - squeegee'ed on in multiple coats without sanding between. I could imagine that cabosil might be used used to make the resin less runny, which might help the resin fill better. Cory Bird's description of the process is here: http://www.sportsmanpilot.com/AL/articles/spr2003/Spring2003.htm "Next came what Cory calls a resin wipe. After going over the surfaces with 36 grit sandpaper he spread on a coat of pure resin, then immediately began squeegeeing it all off. With a little time for cure between applications, this process was repeated five times, leaving just a film of resin maybe two or three thousandths thick, filling every 36 grit scratch and all the pin holes. That was followed by wet sanding with 150 grit, then a coat of DP-48 epoxy primer and a guide coat of some color - just enough to see when it is sanded off." Matt- > > We are doing battle with filling pinholes and small sand marks in Europa > fiberglass fuse. After trying several methods, Dolphin Glaze thick and > thin, Expancel and Aeropoxy (plastic micro) and Q-Cel and Aeropoxy (glass > micro), I tried JB Weld Kwik. > > Seems the JB Weld Kwik is the hands down winner. It is very thick (thicker > than JB Weld) and very sticky. Can squeegee it in place with a razor > blade, and get off 99% and it fills everything and does not shrink or > allow trapped air to force it into a pimple. Sets up in 4 minutes, full > cured pretty hard. > > JB Kwik uses steel as a filler. I don't think it is conductive. I tried > putting a magnet on cured sample and tubes and it does not appear to be > conductive. > > I will have a Com, a Nav/Com and a Transponder Antenna in the fuse and > rudder. > > Think there is a chance that JB Kwik filling small pinholes and very fine > scratches, and lets say some areas with one or 2 ten/thousands" skim on it > will degrade antenna performance to the point that I should not consider > using it? > > Thanking in advance > Ron Parigoris > > ________________________________________________________________________________
Date: Mar 19, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: BNC connector
> > >I tried to no avail. The first stop that caused the ferrule to lock into >place caused it to flange and dimple. I will call Bill tomorrow and see if >he has an explanation. > >Jonsey Very well. The tool doesn't match the connectors. It's time to implement plan-C. Bob . . . ________________________________________________________________________________
Date: Mar 19, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Will steel affect antenna operation?
> >We are doing battle with filling pinholes and small sand marks in Europa >fiberglass fuse. After trying several methods, Dolphin Glaze thick and >thin, Expancel and Aeropoxy (plastic micro) and Q-Cel and Aeropoxy (glass >micro), I tried JB Weld Kwik. > >Seems the JB Weld Kwik is the hands down winner. It is very thick (thicker >than JB Weld) and very sticky. Can squeegee it in place with a razor >blade, and get off 99% and it fills everything and does not shrink or >allow trapped air to force it into a pimple. Sets up in 4 minutes, full >cured pretty hard. > >JB Kwik uses steel as a filler. I don't think it is conductive. I tried >putting a magnet on cured sample and tubes and it does not appear to be >conductive. > >I will have a Com, a Nav/Com and a Transponder Antenna in the fuse and >rudder. > >Think there is a chance that JB Kwik filling small pinholes and very fine >scratches, and lets say some areas with one or 2 ten/thousands" skim on it >will degrade antenna performance to the point that I should not consider >using it? The filler will have no effect upon your embedded atennas. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 19, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Popped CB
> > How do you deduce whether or not it's charging? What > kind of instrumentation do you have? > >I'm using the Grand Rapids Tech EIS. The window where "Voltage" is >displayed showed ~ 10.8 volts. Rotax manual indicates a permanent >output of 13.5 v. >Additionally, the Dynon EFIS would not come on with the Master, but it >did come on with the EBus switched on (with the master also on). (When >testing during installation I noted previously the Dynon will come on >with the master if the battery is fully charged. When battery is not >fully charged the Master does not bring it on line but the EBus will.) Okay, you need to put a voltmeter on the AC input wires to the regulator with the engine running (yellow) and see what voltage you get there at moderate RPMs (don't need to run up to full throttle . . . just see that here's a substantial voltage there - 20 volts or more). Do I presume correctly that you're wired per the latest verstion of Z-16? Is the relay closing (hear it 'click') when you move the master switch to full up position? You can do this while the engine is not running so you can listen. If the regulator is still the same version I looked at some years ago, it depends on a GOOD ground between regulator case and your firewall ground bolt. Bob . . . ________________________________________________________________________________
Subject: Extra credit quiz
From: Erich_Weaver(at)URSCorp.com
Date: Mar 19, 2007
I was glad to see anything promoting the Aeroelectric connection, but f ound the article to have very limited information. What really bugged me wa s that the pictures of connectors were for ones that are NOT recommended. To be fair, this was pointed out in the caption, but how about showing peo ple what the good ones look like instead of leaving people guessing? Erich Weaver ________________________________________________________________________________
Date: Mar 19, 2007
From: Bob White <bob@bob-white.com>
Subject: Re: Popped CB
wrote: > > The diode can be inside or outside . . . some of my drawings > show it inside because the starter contactor I used to sell > had it built in . . . but you can put one on the outside. > > Is it possible to put a diode on the outside of a three connector relay? > > > Frank > Hi Frank, As best I can tell, this question wasn't addressed so I will take the liberty of replying. Yes. One side of the coil is connected internally to the contact that goes to the battery, and the other side of the coil is grounded by a switch on the panel. To put the diode across the coil, connect the cathode to the battery contact and the anode on the coil terminal. small sketch attached. Bob W. -- N93BD - Rotary Powered BD-4 - http://www.bob-white.com First Flight: 11/23/2006 7:50AM - 3.8 Hours Total Time Cables for your rotary installation - http://www.roblinphoto.com/shop/ ________________________________________________________________________________
Date: Mar 20, 2007
From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net>
Subject: Fuel guage non-coax to BNC
It's an Electronics International FL-2CA Gauge Bob. I looked on their website and they show it but I don't see an install manual available. EI recommends their own P-300C probes but since this was the gauge Van's recommended for use with the RV series capacitive senders (large flat plates mounted vertically on the ribs inside the tanks) I assume there was some collaboration to ensure things would work. I looked through the install manual I have and I'm afraid it doesn't say a whole lot. It shows the pre-wired connector and identifies red, black and white wires which go to each (right and left) sensor converter cable assembly but doesn't say what their functions are(I assume they are power, ground and signal). The factory bundled each of these sets of three wires with a "left" and "right" tag so you know which is which but, that's all the information they supply. Each sensor/converter cable assembly has five, individual, single conductor, unshielded wires that go into what looks to me to be a tiny circuit board about a half inch square that's covered with black heat-shrink. The three (red, black and white) wires connect to the gauge harness mentioned above and the other two wires connect to the senders in the tank (or the EI P-300 probe). I assume that if the wires from the tank to the converter cable CCA needed to be shielded then EI would have provided them that way. I think Van's just chose a BNC connection because it is very easy to drill a small hole in the fuel tank and pro-seal the connector in (no mess, no fuss, no leaking fuel, assuming the dielectric in the female BNC is resistant to attack from gasoline). And the BNC is a nice positive connection well protected from outside contamination. So... I just need to figure how mate one of the tank sensor wires to what would be the shield crimp on a BNC male connector. Thanks for the help. Dean _________________________ Original Message _______________________________ >From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net> >Subject: Re: AeroElectric-List: Non coax to BNC connector. > >Have an Electronics International Capacitive Fuel Gauge for Van's >capacitive senders in my RV-6 fuel tanks....... > > Do you know where I can download the installation manual > for your system . . . or do you have it in .pdf form that > you can e-mail to me? > > Bob . . . ________________________________________________________________________________
Date: Mar 20, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: OV protection
I know there's been a lot of discussion about OV protection, but I'm wondering if anyone has come up with OV protection for the Van's internal regulated alternator? I'm hesitant to connect my expensive panel with out it. Thanks, Sam Marlow ________________________________________________________________________________
From: "Dennis Jones" <djones(at)northboone.net>
Subject: BNC connector
Date: Mar 20, 2007
Bob I talked to B and C today. They did a test drive of the connectors and the same tool. He adjusted the crimping pressure however he still ended up with the flanges. He called them a slight flange. So I guess I need to find a different coupler that will fit with the tool. Any suggestions? Jonsey -----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 Sent: Monday, March 19, 2007 7:38 AM Subject: RE: AeroElectric-List: BNC connector > > >I tried to no avail. The first stop that caused the ferrule to lock into >place caused it to flange and dimple. I will call Bill tomorrow and see if >he has an explanation. > >Jonsey Very well. The tool doesn't match the connectors. It's time to implement plan-C. Bob . . . ________________________________________________________________________________
Subject: RF antenna connectors
From: "Dennis Jones" <djones(at)northboone.net>
Date: Mar 19, 2007
Bob Do you or anyone else out there, have information on installing RF antenna connectors for a tray mount to RG-400? I know the center conductor is soldered to the center pin and the shield is soldered to the side enterence. Does the shield go all the way to the enterence to the main cup? Does the insullation go flush with enterance to the side entery? And if so how would one get the sodder into the side enterence? How far does the shield go inside? Is it flush with the inside of the cup? Jonsey Read this topic online here: http://forums.matronics.com/viewtopic.php?p=101824#101824 ________________________________________________________________________________
From: luigit(at)freemail.it
Subject: Fiberglass fuselage
Date: Mar 20, 2007
--- MIME Errors - No Plain-Text Section Found --- A message with no text/plain MIME section was received. The entire body of the message was removed. Please resend the email using Plain Text formatting. HOTMAIL is notorious for only including an HTML section in their client's default configuration. If you're using HOTMAIL, please see your email application's settings and switch to a default mail option that uses "Plain Text". --- MIME Errors No Plain-Text Section Found --- ________________________________________________________________________________
From: "Allan Aaron" <aaaron(at)tvp.com.au>
Subject: Progressive loss of radio quality
Date: Mar 20, 2007
My friend has a cozy (fibreglas construction) with an icom a200 (i think) tranceiver. When he transmits the initial quality is good but if the transmission continues for many seconds it degrades to the point of being unreadable. Is this likely to be an antenna grounding issue, a factor related to it being a glass plane or a fault with the radio? Any thoughts appreciated. allan ________________________________________________________________________________
From: "Dale Fultz" <dfultz7(at)earthlink.net>
Subject: Re: OV protection
Date: Mar 20, 2007
Sam, if it is a PLANE POWER altenator that Van's sold you, then you have nothing to worry about if installed properly.. ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RF antenna connectors
> > >Bob > >Do you or anyone else out there, have information on installing RF antenna >connectors for a tray mount to RG-400? I know the center conductor is >soldered to the center pin and the shield is soldered to the side >enterence. Does the shield go all the way to the enterence to the main >cup? Does the insullation go flush with enterance to the side entery? And >if so how would one get the sodder into the side enterence? How far does >the shield go inside? Is it flush with the inside of the cup? > >Jonsey If you'll send me your coax fitting I'll install what ever length of RG-400 you wish onto it and use the fitting to craft a comic-book on the subject for posting on my website. I've been wanting to do this article but haven't had access to the fitting. Bob . . . AeroElectric Connection 6936 Bainbridige Road Wichita, KS 67226 ________________________________________________________________________________
Date: Mar 20, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: OV protection
I'm not at the hangar, so I'm not sure of the brand, but it came with the RV10 firewall forward kit. Dale Fultz wrote: > Sam, if it is a PLANE POWER altenator that Van's sold you, then you > have nothing to worry about if installed properly.. > > > > * > > > * ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: BNC connector
> > >Bob > >I talked to B and C today. They did a test drive of the connectors and the >same tool. He adjusted the crimping pressure however he still ended up with >the flanges. He called them a slight flange. So I guess I need to find a >different coupler that will fit with the tool. Any suggestions? > >Jonsey Hmmm . . . Did you get the connectors and tool from different sources? One of my suppliers was Jameco but they don't stock the import connector I used to sell any more but they do offer name-brand connectors. Suggest you try https://www.jameco.com/Jameco/Products/ProdDS/355240.pdf It's their stock# 355240 1e564b.jpg Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Extra credit quiz
>I was glad to see anything promoting the Aeroelectric connection, but >found the article to have very limited information. What really bugged me >was that the pictures of connectors were for ones that are NOT >recommended. To be fair, this was pointed out in the caption, but how >about showing people what the good ones look like instead of leaving >people guessing? I think the thrust of the article was about the seminars, not so much simple ideas. Did you spot any errors in simple ideas beyond the terminal illustration? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Progressive loss of radio quality
> >My friend has a cozy (fibreglas construction) with an icom a200 (i think) >tranceiver. When he transmits the initial quality is good but if the >transmission continues for many seconds it degrades to the point of being >unreadable. Is this likely to be an antenna grounding issue, a factor >related to it being a glass plane or a fault with the radio? Any thoughts >appreciated. if it has anything to do with local RF getting back into the radio, a dummy load check will show this up. Put this device on the transceiver's feedline. http://www.aeroelectric.com/Pictures/Tools/DummyLoad.jpg Listen on adjacent airplane or handheld while transmitting on subject radio. If the problem goes away when the antenna is out of the loop, then the investigation will focus outside the radio. Is this a new condition or has it existed since day-one? Bob . . . ________________________________________________________________________________
Date: Mar 20, 2007
Subject: OV protection
From: James H Nelson <rv9jim(at)juno.com>
Sam, If your not real sure about the alternator, AND if you have not hooked up the Van's unit and its in its original box, Van will take it back and you can go to the "Plane Power" 60A unit that has a built in OV protection module. I traded mine and the Plane Power alternator looks real nice. I have not run it yet but this summer it will be flying. Bob Nuckols has talked with the people at PP and is satisfied that the OV unit will work as advertised. It trips the field current and the alternator goes dead. That is what you want. Jim Nelson ________________________________________________________________________________
Date: Mar 20, 2007
From: Dave N6030X <N6030X(at)DaveMorris.com>
Subject: Re: Progressive loss of radio quality
It could be that the SWR on the antenna is so high that the transmitter is protecting itself by reducing power. I don't know about the A200 but a lot of modern transmitters have that feature. Make sure all connectors are good and that the coax isn't shorted somewhere. Dave Morris At 05:22 AM 3/20/2007, you wrote: > >My friend has a cozy (fibreglas construction) with an icom a200 (i >think) tranceiver. When he transmits the initial quality is good but >if the transmission continues for many seconds it degrades to the >point of being unreadable. Is this likely to be an antenna grounding >issue, a factor related to it being a glass plane or a fault with >the radio? Any thoughts appreciated. >allan > ________________________________________________________________________________
Date: Mar 20, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: OV protection
I already installed it, and almost ready to fly. I'm just a bit to cautious I guess. James H Nelson wrote: > > Sam, > If your not real sure about the alternator, AND if you have not > hooked up the Van's unit and its in its original box, Van will take it > back and you can go to the "Plane Power" 60A unit that has a built in OV > protection module. I traded mine and the Plane Power alternator looks > real nice. I have not run it yet but this summer it will be flying. Bob > Nuckols has talked with the people at PP and is satisfied that the OV > unit will work as advertised. It trips the field current and the > alternator goes dead. That is what you want. > > Jim Nelson > > > ________________________________________________________________________________
Subject: Fiberglass fuselage
Date: Mar 20, 2007
From: <longg(at)pjm.com>
Luigi, I will do the same with two of the EI bipole antennas. The word is there is no affect from the fiberglass. Do not try the same with carbon fibre which will block the signal. In fact, I have now seen a number of aircraft with the antenna farm in the tail. I am building a Legacy FG which will include two comm, one gs and one marker beacon in the tail. That's the nice thing about fiberglass, you can always move it after testing if necessary. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of luigit(at)freemail.it Sent: Tuesday, March 20, 2007 4:24 AM To: aeroelectric-list(at)matronics.com Subject: AeroElectric-List: Fiberglass fuselage On my Esqual, installing the radio system, an Icom- ICA 200, I wish to put the antenna inside the fusolage, behind the seat or inside the tail. Are there any experience/suggestion to keep ? Length of coaxial cable, position, shield..... Thank-you for any help. Really appreciated, indeed. Luigi, Rome, Italy -- Uso la webmail Dada.net <http://it.email.dada.net/cgi-bin/login.chm> , l'email delle persone che contano e che si raccontano :) -- http://www.matronics.com/Navigator?AeroElectric-List the =========== ________________________________________________________________________________
Subject: OV protection
Date: Mar 20, 2007
From: <longg(at)pjm.com>
Call them and ask? If they don't provide it, there are products out there with internal regulators that DO provide overload protection. Why pack extra equipment? The only thing you will need after that is a dashboard indicator. Perhaps Bob has a diagram for wiring an indicator light from an alternator with built in OV protection. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Sam Marlow Sent: Tuesday, March 20, 2007 1:50 AM To: aeroelectric-list(at)matronics.com Subject: AeroElectric-List: OV protection I know there's been a lot of discussion about OV protection, but I'm wondering if anyone has come up with OV protection for the Van's internal regulated alternator? I'm hesitant to connect my expensive panel with out it. Thanks, Sam Marlow ________________________________________________________________________________
From: luigit(at)freemail.it
Subject: Re: Fiberglass fuselage
Date: Mar 20, 2007
--- MIME Errors - No Plain-Text Section Found --- A message with no text/plain MIME section was received. The entire body of the message was removed. Please resend the email using Plain Text formatting. HOTMAIL is notorious for only including an HTML section in their client's default configuration. If you're using HOTMAIL, please see your email application's settings and switch to a default mail option that uses "Plain Text". --- MIME Errors No Plain-Text Section Found --- ________________________________________________________________________________
Date: Mar 20, 2007
From: Dave N6030X <N6030X(at)DaveMorris.com>
Subject: Re: Fiberglass fuselage
If your tailcone has a diameter of around 31 inches, you can try the Morris Com Loop antenna, which does not require a ground plane and is a better antenna than the typical quarter wave whip. www.DaveMorris.com/MorrisComLoop Dave Morris At 03:24 AM 3/20/2007, you wrote: > >On my Esqual, installing the radio system, an Icom- ICA 200, I >wish to put the antenna inside the fusolage, behind the seat or >inside the tail. > >Are there any experience/suggestion to keep ? Length of coaxial >cable, position, shield..... > >Thank-you for any help. > >Really appreciated, indeed. > >Luigi, Rome, Italy > > >-- Uso la <http://it.email.dada.net/cgi-bin/login.chm>webmail >Dada.net, l'email delle persone che contano e che si raccontano :) >http://www.matronics.com/Navigator?AeroElectric-List ________________________________________________________________________________
Date: Mar 20, 2007
From: Jay Brinkmeyer <jaybrinkmeyer(at)yahoo.com>
Subject: Re: Will steel affect antenna operation?
>JB Kwik uses steel as a filler. I don't think it is conductive. I tried >putting a magnet on cured sample and tubes and it does not appear to be >conductive. Its been a while since my days as a struggling student How do magnetic properties of a material intersect with the desired electrical conductivity characteristics of antenna operation? Maybe I missed something? Jay Get your own web address. http://smallbusiness.yahoo.com/domains/?p=BESTDEAL ________________________________________________________________________________
From: "Jerry Grimmonpre" <jerry(at)mc.net>
Subject: Miniature Toggle Switch
Date: Mar 20, 2007
Bob ... I want to operate a 12V DC computer fan with a cruise load of .58A ... Will a miniature toggle single pole/throw suffer abuse of the contacts for this load? The switch shows a rating of 5A @ 125V AC ... Thanks Jerry ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Miniature Toggle Switch
> >Bob ... >I want to operate a 12V DC computer fan with a cruise load of .58A ... >Will a miniature toggle single pole/throw suffer abuse of the contacts for >this load? >The switch shows a rating of 5A @ 125V AC ... >Thanks >Jerry That switch is more likely to die with age than from any sort of "overload" in this application. See: http://www.aeroelectric.com/articles/swtchrat.pdf Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 20, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Will steel affect antenna operation?
> > > >JB Kwik uses steel as a filler. I don't think it is conductive. I tried > >putting a magnet on cured sample and tubes and it does not appear to be > >conductive. > >Its been a while since my days as a struggling student How do magnetic >properties of a material intersect with the desired electrical conductivity >characteristics of antenna operation? Maybe I missed something? > >Jay Influence due to magnetic properties is not so strong as conductivity, i.e. sheet resistance of the material in question. For single, relatively thin conductors like antenna elements, resistive losses of say stainless steel versus copper can be easily measured but not terribly significant in terms of overall performance on airplanes (we talk line-of-sight and can tolerate rather poor antenna performance). For ground planes, you have an infinite number of radials all operating in parallel such that effects of sheet resistance variability for copper versus aluminum versus stainless under the antenna would be exceedingly difficult to measure in the lab. I can't think of any reason that magnetic properties of the material being considered would offer an effect worth considering beyond that of it's heating losses due to inability to perfectly conduct a current. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 20, 2007
Subject: Re: Will steel affect antenna operation?
From: <rparigor(at)SUFFOLK.LIB.NY.US>
"I can't think of any reason that magnetic properties of the material being considered would offer an effect worth considering beyond that of it's heating losses due to inability to perfectly conduct a current." I was trying to beat up use, and putting something magnetic near remote magnetometer for Dynon D10A was a passing thought. When the extra turbulence on the right side of the aeroplane due to P-Factor temporarily were to put a magnetic charge on the JB Weld, then slip to landing took it off................. White elephant attack I know, but I mentioned that if it is magnetic, I could not detect any force change with a powerful magnet. I figured I would mention in case someone had same thought that it mat interfere with compass/s Ron Parigoris ________________________________________________________________________________
Date: Mar 20, 2007
From: Earl_Schroeder <Earl_Schroeder(at)juno.com>
Subject: Re: Fiberglass fuselage
Hi Luigi, In my Lancair [fiberglass not carbon] I have my Icom-200 connected to a Jim Weir dipole made from 1/2 wide copper tape. Works great! Ref URL: www.rst-engr.com/ Earl luigit(at)freemail.it wrote: > > On my Esqual, installing the radio system, an Icom- ICA 200, I wish > to put the antenna inside the fusolage, behind the seat or inside the > tail. > > Are there any experience/suggestion to keep ? Length of coaxial > cable, position, shield..... > > Thank-you for any help. > > Really appreciated, indeed. > > Luigi, Rome, Italy > > ________________________________________________________________________________
From: "Rob Wright" <armywrights(at)adelphia.net>
Subject: OV protection
Date: Mar 20, 2007
I didn't specify, because I thought it was replaced with the PP unit as standard. When my FWF kit came I found out that the stock alternator is the "Ford" one that is so endearing to the list. I'm a ways from flying so haven't sent it back yet. Will decide exactly how to proceed later. Rob Wright RV-10 #392 Fuse _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Tuesday, March 20, 2007 8:59 AM Subject: RE: AeroElectric-List: OV protection Call them and ask? If they don't provide it, there are products out there with internal regulators that DO provide overload protection. Why pack extra equipment? The only thing you will need after that is a dashboard indicator. Perhaps Bob has a diagram for wiring an indicator light from an alternator with built in OV protection. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Sam Marlow Sent: Tuesday, March 20, 2007 1:50 AM Subject: AeroElectric-List: OV protection I know there's been a lot of discussion about OV protection, but I'm wondering if anyone has come up with OV protection for the Van's internal regulated alternator? I'm hesitant to connect my expensive panel with out it. Thanks, Sam Marlow href="http://www.matronics.com/Navigator?AeroElectric-List">http://www.matro nics.com/Navigator?AeroElectric-List href="http://forums.matronics.com">http://forums.matronics.com ________________________________________________________________________________
From: "William Gill" <wgill10(at)comcast.net>
Subject: OV protection
Date: Mar 20, 2007
Van' sells the PlanePower 60-amp alternator for $375 60 amp Alternator and Kit w/OV protection Part Number = ES ALTERNATOR DELUXE Price = $375.00 Their standard 60-amp is $270 Complete Alternator Kit 60 AMP Part Number = ES ALTERNATOR 60A KIT Price = $270.00 Just return the one you have and upgrade for an additional $105 (I too believed the PP unit was standard) Bill -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rob Wright Sent: Tuesday, March 20, 2007 11:06 PM Subject: RE: AeroElectric-List: OV protection I didn't specify, because I thought it was replaced with the PP unit as standard. When my FWF kit came I found out that the stock alternator is the "Ford" one that is so endearing to the list. I'm a ways from flying so haven't sent it back yet. Will decide exactly how to proceed later. Rob Wright RV-10 #392 Fuse _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Tuesday, March 20, 2007 8:59 AM Subject: RE: AeroElectric-List: OV protection Call them and ask? If they don't provide it, there are products out there with internal regulators that DO provide overload protection. Why pack extra equipment? The only thing you will need after that is a dashboard indicator. Perhaps Bob has a diagram for wiring an indicator light from an alternator with built in OV protection. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Sam Marlow Sent: Tuesday, March 20, 2007 1:50 AM Subject: AeroElectric-List: OV protection I know there's been a lot of discussion about OV protection, but I'm wondering if anyone has come up with OV protection for the Van's internal regulated alternator? I'm hesitant to connect my expensive panel with out it. Thanks, Sam Marlow href="http://www.matronics.com/Navigator?AeroElectric-List">http://www.m atronics.com/Navigator?AeroElectric-List href="http://forums.matronics.com">http://forums.matronics.com http://www.matronics.com/Navigator?AeroElectric-List http://forums.matronics.com ________________________________________________________________________________
Subject: Re: Extra credit quiz
From: Erich_Weaver(at)URSCorp.com
Date: Mar 21, 2007
Bob said "Did you spot any errors in simple ideas...?" Okay, now I see what you intended - should have paid more attention to the thread subject line. Perusing the Kit Planes article once more, the information regarding th e correct size fuse or circuit breader for a 60-amp alternator doesnt sou nd like what I thought I learned in the 'Connection. The article says use 70 or 80 amps to "prevent nuisance tripping because alternator ratings are minimum ratings." I believe nuisance tripping on my Z-13/8 based syste m with 40 amp alternator is handeled not by oversizing a fuse or breaker on the alternator B-lead, but by using a 5-amp breaker on the alternator field. My B-lead is protected with a 40 amp ANL current limiter which I believe is the correct size for my alternator. Im also bothered by the "minimum rating" part of the statement, as this would seem to imply that the alternator could easily produce that curre nt for long periods of time. We are supposed to be operating at about 75% of the alternator rating, no? Is this more on track, or do I get the booby prize and have to go back and read 'Connection yet again until it finally sinks in? Erich Weaver This e-mail and any attachments are confidential. If you receive this message in error or are not the intended recipient, you should not reta in, distribute, disclose or use any of this information and you should dest roy the e-mail and any attachments or copies. ________________________________________________________________________________
From: "brian Williams" <bw(at)llanddewi.plus.com>
Subject: Radio aerial groundplane
Date: Mar 21, 2007
Hi Bob and list. Have been following list for some time, really excellent source of information. I have a carbon fibre shell aircraft, Pioneer 300, can I use the carbon fibre belly pan as a ground plane or should I fit a separate one. The same question is asked about the transponder aerial, and how far from the comms aerial should it be. Thanks for great list. Brian ________________________________________________________________________________
From: <frank.phyllis(at)mindspring.com>
Subject: Popped CB
Date: Mar 21, 2007
> > How do you deduce whether or not it's charging? What > kind of instrumentation do you have? > >I'm using the Grand Rapids Tech EIS. The window where "Voltage" is >displayed showed ~ 10.8 volts. Rotax manual indicates a permanent >output of 13.5 v. >Additionally, the Dynon EFIS would not come on with the Master, but it >did come on with the EBus switched on (with the master also on). (When >testing during installation I noted previously the Dynon will come on >with the master if the battery is fully charged. When battery is not >fully charged the Master does not bring it on line but the EBus will.) Okay, you need to put a voltmeter on the AC input wires to the regulator with the engine running (yellow) and see what voltage you get there at moderate RPMs (don't need to run up to full throttle . . . just see that here's a substantial voltage there - 20 volts or more). I was able to get 20 v at 2600 RPM Do I presume correctly that you're wired per the latest verstion of Z-16? Is the relay closing (hear it 'click') when you move the master switch to full up position? You can do this while the engine is not running so you can listen. I have Revision 11, May 05. Yes, the battery relay closes (I can hear it click and the EIS, radio, etc comes on). If the regulator is still the same version I looked at some years ago, it depends on a GOOD ground between regulator case and your firewall ground bolt. Regulator is well grounded--bolted directly on firewall and check with Ohm meter = 0. Frank ________________________________________________________________________________
Date: Mar 21, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Radio aerial groundplane
>Hi Bob and list. > >Have been following list for some time, really excellent source of >information. > >I have a carbon fibre shell aircraft, Pioneer 300, can I use the carbon >fibre belly pan as a ground plane or should I fit a separate one. The carbon fiber is about 1000 times the sheet resistance of aluminum and does not make a good ground plane. You'll need to use "radials" on the comm antennas and either radials or a full disk ground plane on the transponder antenna. VOR and GPS antennas generally do not rely on groundplanes for proper operation. >The same question is asked about the transponder aerial, and how far from >the comms aerial should it be. As far as practical but certainly 36" is plenty. Don't loose any sleep over it if it's only 20". Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 21, 2007
Subject: Re: Extra credit quiz
From: "Matt Prather" <mprather(at)spro.net>
Erich, Your method of protecting the b-lead is correct as well. Minimum rating means that the manufacturer is telling you their product will produce at least a certain number of watts of electrical energy under certain conditions. Under more favorable conditions (cold temperature) the alternator likely is capable of producing more power. If you bought a 560Watt alternator (14V*40A) and it only produced 500Watts (while duplicating the test conditions), you'd be rightly disappointed. Regards, Matt- > > > Bob said "Did you spot any errors in simple ideas...?" > > Okay, now I see what you intended - should have paid more attention to the > thread subject line. > > Perusing the Kit Planes article once more, the information regarding the > correct size fuse or circuit breader for a 60-amp alternator doesnt sound > like what I thought I learned in the 'Connection. The article says use > 70 > or 80 amps to "prevent nuisance tripping because alternator ratings are > minimum ratings." I believe nuisance tripping on my Z-13/8 based system > with 40 amp alternator is handeled not by oversizing a fuse or breaker on > the alternator B-lead, but by using a 5-amp breaker on the alternator > field. My B-lead is protected with a 40 amp ANL current limiter which I > believe is the correct size for my alternator. > > Im also bothered by the "minimum rating" part of the statement, as this > would seem to imply that the alternator could easily produce that current > for long periods of time. We are supposed to be operating at about 75% of > the alternator rating, no? > > Is this more on track, or do I get the booby prize and have to go back and > read 'Connection yet again until it finally sinks in? > > Erich Weaver > This e-mail and any attachments are confidential. If you receive this > message in error or are not the intended recipient, you should not retain, > distribute, disclose or use any of this information and you should destroy > the e-mail and any attachments or copies. ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: XLR connectors
Date: Mar 21, 2007
Bob, Somewhere you had mentioned the use of XLR connectors as good parts to use as an external power port for charging aircraft batteries. These are made for audio applications and commonly found at radio Shack and other sound outlets. I would like to install one or two in my RV7A for maintaining the batteries whenever not flying (electrically dependant engine) to keep the batteries in full charge at all times and to supply power when "hangar flying" the EFIS and GPS as I learn how to use/program them. Now, several questions: Since these are audio products and not necessarily intended for sustained large current carrying capacity, max current are not likely published by the manufacturer. I have no specs here. Do you know the max DC current rating for these devices or have you tested one to destruction? If not, I could send you one for destructive testing. I could too for that matter, but my power supply only goes up to 25 amps at 12V. Maybe, I could use a car battery to supply more current. Any comments here? Would you recommend using the XLR port for ONLY "maintaining" battery levels and fused at some low value (if so what value would you recommend) or could these ports be used to "charge up" a depleted battery without current restrictions? Considering a dual battery system (probably Z-19) I assume two XLR ports would be required? I like these ports as they are small, lightweight, utilize chassis mount format, and have positive locking mechanism. A down side is they do not come with a cover to keep the weather out. I'm considering hiding them behind a small door near the aft mounted batteries. Any comments here? Bevan RV7A Finishing canopy Planning electrical install ________________________________________________________________________________
Date: Mar 21, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: XLR connectors
>Bob, > >Somewhere you had mentioned the use of XLR connectors as good parts to use >as an external power port for charging aircraft batteries. These are made >for audio applications and commonly found at radio Shack and other sound >outlets. I would like to install one or two in my RV7A for maintaining >the batteries whenever not flying (electrically dependant engine) to keep >the batteries in full charge at all times and to supply power when "hangar >flying" the EFIS and GPS as I learn how to use/program them. Now, several >questions: > >Since these are audio products and not necessarily intended for sustained >large current carrying capacity, max current are not likely published by >the manufacturer. I have no specs here. Do you know the max DC current >rating for these devices or have you tested one to destruction? The BEST application for these connectors is as cockpit power outlets for portable accessories. >If not, I could send you one for destructive testing. I could too for that >matter, but my power supply only goes up to 25 amps at 12V. Maybe, I >could use a car battery to supply more current. Any comments here? > >Would you recommend using the XLR port for ONLY "maintaining" battery >levels and fused at some low value (if so what value would you recommend) >or could these ports be used to "charge up" a depleted battery without >current restrictions? Yes . . . These can be used for a charger connection for a Battery Tender or Battery Minder. Perhaps even a small Schumacher smart charger rated at no more than 5A. >Considering a dual battery system (probably Z-19) I assume two XLR ports >would be required? Yeah . . . but you COULD use a single maintainer to do this through a single connector. The XLR connectors have 3 terminals. Use one for ground. Use the other two as feeders off the battery bus with 5A fuses. Then short these two pins together in the CHARGER side of the connection. This parallels the batteries only during the maintenance mode when the charger is plugged in. >I like these ports as they are small, lightweight, utilize chassis mount >format, and have positive locking mechanism. A down side is they do not >come with a cover to keep the weather out. I'm considering hiding them >behind a small door near the aft mounted batteries. Any comments here? Sounds like a plan. There are some flip-cover versions out there in the wild but they can be mounted in some handy but covered spot like on a bracket you can reach through the oil-check door. The only caveat is to limit total current through this connection to 5A or less. Bob . . . ________________________________________________________________________________
From: "Dennis Jones" <djones(at)northboone.net>
Subject: RF antenna connectors
Date: Mar 21, 2007
Bob I will box it up and send it on its way. Thank You Jonsey -----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 Sent: Tuesday, March 20, 2007 7:47 AM Subject: Re: AeroElectric-List: RF antenna connectors > > >Bob > >Do you or anyone else out there, have information on installing RF antenna >connectors for a tray mount to RG-400? I know the center conductor is >soldered to the center pin and the shield is soldered to the side >enterence. Does the shield go all the way to the enterence to the main >cup? Does the insullation go flush with enterance to the side entery? And >if so how would one get the sodder into the side enterence? How far does >the shield go inside? Is it flush with the inside of the cup? > >Jonsey If you'll send me your coax fitting I'll install what ever length of RG-400 you wish onto it and use the fitting to craft a comic-book on the subject for posting on my website. I've been wanting to do this article but haven't had access to the fitting. Bob . . . AeroElectric Connection 6936 Bainbridige Road Wichita, KS 67226 ________________________________________________________________________________
From: "Carlos Trigo" <trigo(at)mail.telepac.pt>
Subject: Re: XLR connectors
Date: Mar 21, 2007
XLR connectorsBevan Another electrically dependant Subbie guy here. I used a good "cigarrette lighter" socket in my panel, which will have dual function. One outlet, to power any handheld device, and the other as an inlet port to charge my 2 batteries. If you want to consider this solution, I will send you my schematic. Carlos RV-9A ----- Original Message ----- From: B Tomm To: aeroelectric-list(at)matronics.com Sent: Wednesday, March 21, 2007 5:56 PM Subject: AeroElectric-List: XLR connectors Bob, Somewhere you had mentioned the use of XLR connectors as good parts to use as an external power port for charging aircraft batteries. These are made for audio applications and commonly found at radio Shack and other sound outlets. I would like to install one or two in my RV7A for maintaining the batteries whenever not flying (electrically dependant engine) to keep the batteries in full charge at all times and to supply power when "hangar flying" the EFIS and GPS as I learn how to use/program them. Now, several questions: Since these are audio products and not necessarily intended for sustained large current carrying capacity, max current are not likely published by the manufacturer. I have no specs here. Do you know the max DC current rating for these devices or have you tested one to destruction? If not, I could send you one for destructive testing. I could too for that matter, but my power supply only goes up to 25 amps at 12V. Maybe, I could use a car battery to supply more current. Any comments here? Would you recommend using the XLR port for ONLY "maintaining" battery levels and fused at some low value (if so what value would you recommend) or could these ports be used to "charge up" a depleted battery without current restrictions? Considering a dual battery system (probably Z-19) I assume two XLR ports would be required? I like these ports as they are small, lightweight, utilize chassis mount format, and have positive locking mechanism. A down side is they do not come with a cover to keep the weather out. I'm considering hiding them behind a small door near the aft mounted batteries. Any comments here? Bevan RV7A Finishing canopy Planning electrical install ________________________________________________________________________________
Subject: Glideslope Antennas
Date: Mar 21, 2007
From: <longg(at)pjm.com>
I have found very little in the way of GS antennas on the market. I am looking for a solution for a fiberglass airplane. Perhaps one of you have crossed this path and found a good solution? I already have a built in VOR antenna in the wing, two COM dipole antennas attached internally to the fuselage, a transponder antenna through the floor and a beacon copper strip antenna on the floor. I would like to avoid the cat whisker arrangement found throughout GA aircraft. ________________________________________________________________________________
Subject: Glideslope Antennas
Date: Mar 21, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Why not use a splitter for your VOR antenna then you don't need a separate antenna or cable Frank -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Wednesday, March 21, 2007 12:23 PM Subject: AeroElectric-List: Glideslope Antennas I have found very little in the way of GS antennas on the market. I am looking for a solution for a fiberglass airplane. Perhaps one of you have crossed this path and found a good solution? I already have a built in VOR antenna in the wing, two COM dipole antennas attached internally to the fuselage, a transponder antenna through the floor and a beacon copper strip antenna on the floor. I would like to avoid the cat whisker arrangement found throughout GA aircraft. ________________________________________________________________________________
Date: Mar 21, 2007
From: <dsvs(at)ca.rr.com>
Subject: Re: XLR connectors
> > > Sounds like a plan. There are some flip-cover versions out > there in the wild but they can be mounted in some handy > but covered spot like on a bracket you can reach through > the oil-check door. The only caveat is to limit total > current through this connection to 5A or less. > > Bob . . . > > > Bob, These connectors are rated to higher current values and work in the cockpit as well as in the wild (the fully sealed units only) See www.powerletproducts.com/products/plugs_sockets.php > > > ________________________________________________________________________________
Subject: Glideslope Antennas
Date: Mar 21, 2007
From: <longg(at)pjm.com>
Frank, I thought about doing just that, however I only have one VOR antenna and two NAV radios. I have seen a splitter which will allow for both but I am hesitant to use it for fear of signal degradation. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Wednesday, March 21, 2007 3:50 PM Subject: RE: AeroElectric-List: Glideslope Antennas --> (Corvallis)" Why not use a splitter for your VOR antenna then you don't need a separate antenna or cable Frank -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Wednesday, March 21, 2007 12:23 PM Subject: AeroElectric-List: Glideslope Antennas I have found very little in the way of GS antennas on the market. I am looking for a solution for a fiberglass airplane. Perhaps one of you have crossed this path and found a good solution? I already have a built in VOR antenna in the wing, two COM dipole antennas attached internally to the fuselage, a transponder antenna through the floor and a beacon copper strip antenna on the floor. I would like to avoid the cat whisker arrangement found throughout GA aircraft. ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 21, 2007
Subject: Glideslope Antennas
Good Evening longg, I think you will find that at least ninety percent of the certified airplanes that have had a radio installation in the last twenty years will use one set of blades or a V antenna to feed two nav radios and two Glide Slope receivers. As 'Lectric Bob has noted, at the ranges we use, a wet string would probably be adequate. A set of blades is elegant and work very well, but even the cheapest V antenna when spilt with a four way splitter will give every bit of signal any modern receiver can use. Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 3/21/2007 4:07:43 P.M. Central Daylight Time, longg(at)pjm.com writes: Frank, I thought about doing just that, however I only have one VOR antenna and two NAV radios. I have seen a splitter which will allow for both but I am hesitant to use it for fear of signal degradation. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
Subject: Glideslope Antennas
Date: Mar 21, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
I have an Archer wingtip VOR antenna with a splitter and it works very well..Could you use a second wingtip job and split that signal instead, i.e two antennas and two splitters? I'm not sure how the signal would degrade if you used a single antenna to two radios? Frank -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Wednesday, March 21, 2007 2:00 PM Subject: RE: AeroElectric-List: Glideslope Antennas Frank, I thought about doing just that, however I only have one VOR antenna and two NAV radios. I have seen a splitter which will allow for both but I am hesitant to use it for fear of signal degradation. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Wednesday, March 21, 2007 3:50 PM Subject: RE: AeroElectric-List: Glideslope Antennas --> (Corvallis)" Why not use a splitter for your VOR antenna then you don't need a separate antenna or cable Frank -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of longg(at)pjm.com Sent: Wednesday, March 21, 2007 12:23 PM Subject: AeroElectric-List: Glideslope Antennas I have found very little in the way of GS antennas on the market. I am looking for a solution for a fiberglass airplane. Perhaps one of you have crossed this path and found a good solution? I already have a built in VOR antenna in the wing, two COM dipole antennas attached internally to the fuselage, a transponder antenna through the floor and a beacon copper strip antenna on the floor. I would like to avoid the cat whisker arrangement found throughout GA aircraft. ________________________________________________________________________________
Date: Mar 21, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Extra credit quiz
>Bob said "Did you spot any errors in simple ideas...?" > >Okay, now I see what you intended - should have paid more attention to the >thread subject line. > >Perusing the Kit Planes article once more, the information regarding the >correct size fuse or circuit breader for a 60-amp alternator doesnt sound >like what I thought I learned in the 'Connection. The article says >use 70 or 80 amps to "prevent nuisance tripping because alternator >ratings are minimum ratings." I believe nuisance tripping on my Z-13/8 >based system with 40 amp alternator is handeled not by oversizing a fuse >or breaker on the alternator B-lead, but by using a 5-amp breaker on the >alternator field. My B-lead is protected with a 40 amp ANL current >limiter which I believe is the correct size for my alternator. There's breakers, fuses and THEN there are current limiters. The ANL's trip characteristics are shown in . . . http://www.aeroelectric.com/Mfgr_Data/Fuses_and_Current_Limiters/Bussman/ANL_Specs.pdf There's no listing for the ANL40 but note that the ANL35 goes asymptotic to never-trips at about 90 amps! The ANL40 will be higher yet. Obviously, these critters are NOT intended to protect for wire overheat but HARD faults. You could use an ANL40 on a 60A alternator without nuisance tripping. You COULD go for an ANN40. See . . . http://www.aeroelectric.com/Mfgr_Data/Fuses_and_Current_Limiters/Bussman/ANN_Specs.pdf Here the device goes asymptotic to never-trips at 50A. An ANN40 would be solid at about 56A . . . still really good headroom for a 40A alternator. Let's consider a MAX40 for your 40A alternator. See . . . http://www.aeroelectric.com/Mfgr_Data/Fuses_and_Current_Limiters/Bussman/MAXI_Specs.pdf This device doesn't go asymptotic at under 100 seconds but still takes 60A to open it in about two minutes. But your 40A alternator will put out 50A or so when it's cold. Hmmmm . . . starting to push the limits. Lets look at a 40A breaker like . . . http://www.aeroelectric.com/Mfgr_Data/Breakers/Potter_Brumfield/W2331_DS.pdf Note in the calibration data we read: "Will carry 100% of rating but may trip between 101% and 134% of rating. Must trip within one hour at 135%." Things change pretty quickly in the range of 135 to 200% and drop to seconds of trip time. These are but a few examples of how much variability you can find in characteristics of the various circuit protection products when compared with their RATINGS. My writings have suggested the fast devices like fuses and breakers have healthy margins over the ratings of the alternator. Again, b-lead protection is for taming HARD faults (read many hundreds of amps) and not enduring low level overloads. Bottom line is that you probably can't have b-lead protection that is TOO big when selecting breakers and/or fuses. Anywhere from 1.5 to 3x the alternator rating would do the hard fault protection job and be free of nuisance tripping. On the other hand, current limiters are offered with those headrooms already built in. They're much more robust with respect to ratings than their faster cousins. >Im also bothered by the "minimum rating" part of the statement, as this >would seem to imply that the alternator could easily produce that current >for long periods of time. We are supposed to be operating at about 75% of >the alternator rating, no? You want to plan no more than 75% of rating for continuous loads by your ship's equipment as defined by the various operating conditions in your load analysis. See: http://www.aeroelectric.com/PPS/Load_Analysis/Revised%20%20load_analysis.xls or if you want to do one by hand see: http://www.aeroelectric.com/PPS/Load_Analysis/Blank_Form.pdf The idea behind alternator de-rating is to leave some stuff left over for RECHARGING the BATTERY. You don't want to launch in some condition that needs 100% of alternator output and leave your battery unattended. >Is this more on track, or do I get the booby prize and have to go back and >read 'Connection yet again until it finally sinks in? Hmmmm . . . here's a chance to redeem yourself. How accurate was he with respect to quotation of mile stones in voltage readings? Actually, his piece was pretty accurate for someone who is attempting a good critique of an activity that was not his particular field of experience. We romp along pretty fast in those seminars and we know it's tough to be 100% retentive in the best of circumstances. I'm working on the power point presentation for a seminar next Saturday in North Carolina. My seminar format is in transition in preparation for offing audio/slide and ultimately video versions off the website. This will allow us to reach many more individuals than those opportunities offered at 6-8 seminars a year. Bob . . . ________________________________________________________________________________
Date: Mar 21, 2007
From: "Stephen Reynolds" <stephen.j.reyn(at)gmail.com>
Subject: SD8 Connection queries
I have a SD8 standby alternator on my RV7 & am considering the various options for connecting it into the aircraft wiring. I have been looking at Bobs Z-8 diagram which uses an essential bus & cross tie. I would rather not have the essential bus & just have a way of connecting the both the SD8 & the battery into the main bus should the battery contactor fail as I see this as a single point of failure. Has anyone done something similar or is there another wiring diagram out there that shows another way of doing this. Thanks in advance Stephen RV7 N570Z Finish ________________________________________________________________________________
From: "John Burnaby" <jonlaury(at)impulse.net>
Subject: What did I do wrong?
Date: Mar 21, 2007
I am installing a flexible USB 5v, 50ma LED used on computers for cockpit/map light. To figure out which contacts light the LED, I soldered a 5.1v , 1 watt, Zener diode on to the positive lead of my power supply and went probing the contacts. The two outside contacts were the ones powering the LED. But the LED promptly fried. Obviously there's more to this than I thought. What do I need to do to here to keep my LED lights from burning up? Thanks, John ________________________________________________________________________________
Subject: Re: XLR connectors
From: "jetboy" <sanson.r(at)xtra.co.nz>
Date: Mar 22, 2007
Yes the XLR connector would be fine. There is also a 4 pin version used in the video industry extensively for 12V DC power on camera / recorder equipment. The pins are slightlly smaller dia. than the more common 3 pin audio connector, so the audio one may in fact have better current capability. both versions are very robust, cameramen and sound techs do not appreciate loosing their footage - as you will using the most horrid connector of all - the cigar lighter plug. these things are more likely to start a fire than the lighter itself - no disrespect to those that use them- please be wary of leaving them unattended and dont use for mission critical applications. A friend found the one in his Cherokee was not enough for all his gadgets so bought a 4 outlet box and slung it up behind the panel.... thereafter had to wiggle the plugs about to keep all his stuff online. It would be safer to cut all the plugs off and use a wire joiner - but can't do that in a cert. A/C Ralph -------- Ralph - CH701 / 2200a Read this topic online here: http://forums.matronics.com/viewtopic.php?p=102263#102263 ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: What did I do wrong?
>I am installing a flexible USB 5v, 50ma LED used on computers for >cockpit/map light. To figure out which contacts light the LED, I soldered >a 5.1v , 1 watt, Zener diode on to the positive lead of my power supply >and went probing the contacts. The two outside contacts were the ones >powering the LED. But the LED promptly fried. > >Obviously there's more to this than I thought. What do I need to do to >here to keep my LED lights from burning up? > >Thanks, >John adding a 5v zener in series with your powersupply only DROPS the supply voltage by 5v. Assuming a 12v supply, this leaves you 7v. Try hooking your lamp up with a series RESISTOR instead. Put a mulitmeter in series with your supply and adjust the resistor to get 30 milliamps of flow when pwered up. This is the operating point for most LEDs. White LEDs need about 4 volts to work so the 1v drop at .03 amps suggests a 33 ohm resistor inside the fixture. Applying 7 volts would have tripled the current trough the LED and probably induced the failure. If you don't have a tightly regulated 5v supply to run the light, then the series resistor is better. Try 200-270 ohms. A 1/2 watt resistor will do. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: CD version 10.1 is posted
The all inclusive data CD I've been offering on my website has been updated to version 10.1 I've posted it at: http://aeroelectric.com/CD Download the .zip file and unzip it to a CD or some dedicated directory on your hard drive. It's about 400M so expect 7-15 minutes depending on your service. Feel free to distribute this CD amongst your friends if they have an interest. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Subject: Re: What did I do wrong?
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Mar 22, 2007
> I am installing a flexible USB 5v, 50ma LED used on computers for cockpit/map light. To figure out which contacts light the LED, I soldered a 5.1v , 1 watt, Zener diode on to the positive lead of my power supply and went probing the contacts. The two outside contacts were the ones powering the LED. But the LED promptly fried. > > Obviously there's more to this than I thought. What do I need to do to here to keep my LED lights from burning up? John, A USB connection is nominally 5VDC current limited initially to 100 ma. So the LED assembly probably has inside it a current limiting resistor of R= (5V-Vf)/0.050 (You could assume it is about 47 ohms 1/4W) Diagnosing how you used the zener would complicate the issue. I suspect your assumption of how the zener works out needs some rethinking. But if you want to put this into your airplane on 14V add a series 470 ohm 1.5W resistor and be happy. Ring the bells that still can ring Forget your perfect offering There is a crack in everything That's how the light gets in. ---Leonard Cohen -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=102291#102291 ________________________________________________________________________________
Date: Mar 22, 2007
Subject: Re: What did I do wrong?
From: "Matt Prather" <mprather(at)spro.net>
Hey John, If I understand what you described, the zener would have only been capable of reducing the voltage seen by 5V. In other words, if the supply were set at 20V, the LED would see 15V... If the supply makes 12V, the LED sees 7V, etc. A way to make the LED see 5V is to connect the zener to ground, and then an appropriate resistor, and then to the positive lead of the power supply. Probe the LED from the node between the zener and the resistor. Matt- > I am installing a flexible USB 5v, 50ma LED used on computers for > cockpit/map light. To figure out which contacts light the LED, I soldered > a 5.1v , 1 watt, Zener diode on to the positive lead of my power supply > and went probing the contacts. The two outside contacts were the ones > powering the LED. But the LED promptly fried. > > Obviously there's more to this than I thought. What do I need to do to > here to keep my LED lights from burning up? > > Thanks, > John ________________________________________________________________________________
Date: Mar 22, 2007
From: "Larry James" <larry(at)ncproto.com>
Subject: ANR Headset Power without batteries - findings
Here is what I am learning on this subject: 1) My current Telex 50D headsets run on 8 - 28 vdc. Changing the cord / plugs will void the warranty. 2) The ANR headsets in my Flightsuits helmet are supplied by Headsets Inc. and run on 9 vdc. 3) The plug / connector that Headsets Inc. uses are Switchraft numbers 760 and 712A. 4) There does not seem to be any movement towards a single connector standard. The person at Telex indicated that their unit in this configuration was extremely low volume and there was no interest in putting any effort into improving it or talking with anyone about standardizing. 5) I flew again yesterday using my wife's Bose headset and the ear cups don't fit my (big??) ears that well. I don't want to convert back to Bose for myself (she continues to like them a lot). 6) This is what I am going to do: a. Install Headsets Inc. 9 vdc converter / power connector in the front seat of our Decathlon and both seats of the Rocket. b. Find a source to custom make very nice 3-plug cables; standard mic, standard headset, and the 760 power plugs. I'm looking for gold plated plug contacts, molded plug bodies, and a nicely molded 3-way "Y" where the 3 breakout. I'll buy a few of these and retrofit them to whatever I like. c. Retrofit this new cable to my Telex headsets (voiding the warranty). d. Retrofit this new cable to my helmet. e. Keep a couple of extra of these cables for future use. f. Headsets Inc. makes an auxiliary 9 vdc Battery Pack. I'll use this whenever I want to use any of "my" headsets in another aircraft. This is the most elegant solution I've been able to come up with ... And I'm open to suggestions. Larry E. James Bellevue, WA Super Decathlon Rocket (fuselage / systems) ________________________________________________________________________________
From: "Alan K. Adamson" <aadamson(at)highrf.com>
Subject: Wire size dilemma
Date: Mar 22, 2007
Ok, so I'm planning on a dual alt/batt 24v setup for a Lancair legacy. Batteries will be mounted behind the seats, a single 24v Concorde, and a backup B&C. I'm stuck on wire sizes to accommodate my goals. Wonder if anyone would care to comment. I had planned to run #2 between the starter contactor and the starter (both will be on the firewall). Then #4 between the Main alternator (a 100A 24v version) the starter contactor and the main batt contactor (which will be at the batteries about 5ft behind the firewall). Because the standby alternator is only 20A and a backup, was going to run #8 for it thru the firewall, to the battery contact/cross tie. Mine you, the cross tie will be "strap" connected so it won't actually be wire there. But after seeing a few larger airplanes, I started to re-think this plan. Perhaps I should use #2 for everything on the Main battery side, and stay either with #8 or go to #6 or #4 on the standby side. Trying to avoid losses over length, etc. I've looked thru everything I can find on Bob's site, but most of them are for 60A alternators on the main side and 12v, so I'm really not sure what to do. Any takers? To help with a little more placement info. The firewall will have the starter contactor only, the batteries are about 5-7 (wire feet) behind the firewall, the battery and cross tie contactors will be at the batteries. Thanks in advance, Alan ________________________________________________________________________________
Subject: Re:Extra credit quiz
From: Erich_Weaver(at)URSCorp.com
Date: Mar 22, 2007
Bob wrote: "Hmmmm . . . here's a chance to redeem yourself. How accurate was he with respect to quotation of mile stones in voltage readings?" Well that narrows it down quite a bit, ensuring complete and immediate public humiliation upon any further displays of my electrical ineptness : ) Then again, I didnt have far to go to reach that state anyway, so for t he purposes of List entertainment, I will go forward with my second answer to the quiz. The article states "A fully charged, healthy battery will show 12.5 vol tes, and a fully discharged battery will show 10.5 volts." Fair enough. B ut shortly thereafter, it goes on to state: "Where do you want to set you low voltage warning? How about 13.9 volts, which indicates hat the alterna tor isnt charging and you're running off the stored battery charge." Setting the warning at 13.9 volts seems a tad high to me - I would expe ct battery-only operations to exhibit a voltage significantly less than th is, especially if there was any load at all. Heck, voltage may well drop t o below this value just from going through the bridge rectifier to my e-b us. How about a setting more like 13.0 volts or so? Regardless of quiz results, I am so pleased to have been able to do my electrical wiring myself. I pretty much stuck with the Z-13/8 schematic , because time after time I have seen people overthinking it with "improvements" that just plain arent. Plus, even if I'm issing the nua nces of breakers vs. current limiters, Bob has my rear covered. Thanks for t he 'Connection and this list Bob. Erich Weaver This e-mail and any attachments are confidential. If you receive this message in error or are not the intended recipient, you should not retain, distribute, disclose or use any of this information and you should destroy the e-mail and any attachments or copies. ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Wire size dilemma
> > >Ok, so I'm planning on a dual alt/batt 24v setup for a Lancair legacy. >Batteries will be mounted behind the seats, a single 24v Concorde, and a >backup B&C. I'm stuck on wire sizes to accommodate my goals. Wonder if >anyone would care to comment. I had planned to run #2 between the starter >contactor and the starter (both will be on the firewall). Then #4 between >the Main alternator (a 100A 24v version) the starter contactor and the main >batt contactor (which will be at the batteries about 5ft behind the >firewall). Because the standby alternator is only 20A and a backup, was >going to run #8 for it thru the firewall, to the battery contact/cross tie. >Mine you, the cross tie will be "strap" connected so it won't actually be >wire there. > >But after seeing a few larger airplanes, I started to re-think this plan. >Perhaps I should use #2 for everything on the Main battery side, and stay >either with #8 or go to #6 or #4 on the standby side. > >Trying to avoid losses over length, etc. I've looked thru everything I can >find on Bob's site, but most of them are for 60A alternators on the main >side and 12v, so I'm really not sure what to do. > >Any takers? > >To help with a little more placement info. The firewall will have the >starter contactor only, the batteries are about 5-7 (wire feet) behind the >firewall, the battery and cross tie contactors will be at the batteries. I'd run a 2AWG ground for both batteries. Put crosstie contactor on firewall to use as fwd distribution point for the two systems. Run 2AWG for all fat wires on the main battery(+) side and 4AWG for fat wires on the auxiliary battery(+) side. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Wire size dilemma
> > >Ok, so I'm planning on a dual alt/batt 24v setup for a Lancair legacy. >Batteries will be mounted behind the seats, a single 24v Concorde, and a >backup B&C. I'm stuck on wire sizes to accommodate my goals. Wonder if >anyone would care to comment. I had planned to run #2 between the starter >contactor and the starter (both will be on the firewall). Then #4 between >the Main alternator (a 100A 24v version) the starter contactor and the main >batt contactor (which will be at the batteries about 5ft behind the >firewall). Because the standby alternator is only 20A and a backup, was >going to run #8 for it thru the firewall, to the battery contact/cross tie. >Mine you, the cross tie will be "strap" connected so it won't actually be >wire there. > >But after seeing a few larger airplanes, I started to re-think this plan. >Perhaps I should use #2 for everything on the Main battery side, and stay >either with #8 or go to #6 or #4 on the standby side. > >Trying to avoid losses over length, etc. I've looked thru everything I can >find on Bob's site, but most of them are for 60A alternators on the main >side and 12v, so I'm really not sure what to do. > >Any takers? > >To help with a little more placement info. The firewall will have the >starter contactor only, the batteries are about 5-7 (wire feet) behind the >firewall, the battery and cross tie contactors will be at the batteries. I'd run a 2AWG ground for both batteries. Put crosstie contactor on firewall to use as fwd distribution point for the two systems. Run 2AWG for all fat wires on the main battery(+) side and 4AWG for fat wires on the auxiliary battery(+) side. P.S. Use welding cable for jumpers from battery(-) terminals to common gnd and battery(+) terminals to their respective contactors. Use what ever style wire you like for other conductors. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re:Extra credit quiz
>Bob wrote: "Hmmmm . . . here's a chance to redeem yourself. How >accurate was he with respect to quotation of mile >stones in voltage readings?" > >Well that narrows it down quite a bit, ensuring complete and immediate >public humiliation upon any further displays of my electrical ineptness : ) > >Then again, I didnt have far to go to reach that state anyway, so for the >purposes of List entertainment, I will go forward with my second answer to >the quiz. > >The article states "A fully charged, healthy battery will show 12.5 >voltes, and a fully discharged battery will show 10.5 volts." Fair >enough. But shortly thereafter, it goes on to state: "Where do you want >to set you low voltage warning? How about 13.9 volts, which indicates hat >the alternator isnt charging and you're running off the stored battery charge." > >Setting the warning at 13.9 volts seems a tad high to me - I would expect >battery-only operations to exhibit a voltage significantly less than this, >especially if there was any load at all. Heck, voltage may well drop to >below this value just from going through the bridge rectifier to my >e-bus. How about a setting more like 13.0 volts or so? BINGO! You win the six pac . . . >Regardless of quiz results, I am so pleased to have been able to do my >electrical wiring myself. I pretty much stuck with the Z-13/8 schematic, >because time after time I have seen people overthinking it with >"improvements" that just plain arent. Plus, even if I'm issing the >nuances of breakers vs. current limiters, Bob has my rear covered. Thanks >for the 'Connection and this list Bob. You're most welcome. Couldn't do it if it wasn't fun. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Out of town for a couple of days
Dr. Dee and I are climbing aboard the heavy iron bird for the Winterville, North Carolina seminar next Saturday and Sunday. We'll be off line until Tuesday. If anyone wants to attend this presentation, you can just show up. You don't need a reservation. See: http://aeroelectric.com/seminars/Winterville.html Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: SD8 Connection queries
>I have a SD8 standby alternator on my RV7 & am considering the various >options for connecting it into the aircraft wiring. I have been looking at >Bobs Z-8 diagram which uses an essential bus & cross tie. I would rather >not have the essential bus & just have a way of connecting the both the >SD8 & the battery into the main bus should the battery contactor fail as I >see this as a single point of failure. Has anyone done something similar >or is there another wiring diagram out there that shows another way of >doing this. What's the heartburn with Z-13/8? What failure do you anticipate that the architecture won't cover? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 22, 2007
From: "Stephen Reynolds" <stephen.j.reyn(at)gmail.com>
Subject: Re: SD8 Connection queries
I wanted to get away from using the essential bus. If you were just going to use a common bus do you think it would be practical to have the SD8 & the battery feeding this via some sort of cross tie / switch. In the event of a alternator & main contactor failure you would then be able to supply the bus from a combination of the SD8 & the battery. In hindsight the chance of 2 components failing at the same time is statistically irrelevant, still I am planning some long flights so want the best system can devise. Regards Stephen RV7 N570Z wiring - quelle suprise On 22/03/07, Robert L. Nuckolls, III wrote: > > nuckollsr(at)cox.net> > > > >I have a SD8 standby alternator on my RV7 & am considering the various > >options for connecting it into the aircraft wiring. I have been looking > at > >Bobs Z-8 diagram which uses an essential bus & cross tie. I would rather > >not have the essential bus & just have a way of connecting the both the > >SD8 & the battery into the main bus should the battery contactor fail as > I > >see this as a single point of failure. Has anyone done something similar > >or is there another wiring diagram out there that shows another way of > >doing this. > > What's the heartburn with Z-13/8? What failure do you > anticipate that the architecture won't cover? > > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > > ________________________________________________________________________________
From: Bill Settle <billsettle(at)bellsouth.net>
Subject: Re: Out of town for a couple of days
Date: Mar 23, 2007
YEEHAAA!!!! Been looking forward to this. Can't wait! Bill Settle Winston-Salem, NC -8 Wings > > From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net> > Date: 2007/03/22 Thu PM 10:27:49 EST > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: Out of town for a couple of days > > > Dr. Dee and I are climbing aboard the heavy iron bird for > the Winterville, North Carolina seminar next Saturday and > Sunday. We'll be off line until Tuesday. If anyone wants > to attend this presentation, you can just show up. You don't > need a reservation. See: > > http://aeroelectric.com/seminars/Winterville.html > > > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > > > > > > ________________________________________________________________________________
Subject: Wire size dilemma
Date: Mar 23, 2007
From: <longg(at)pjm.com>
Alan, Also, if you have questions about impedance and length, take a look at and try one of the worksheets from Jim's engineering page. His worksheet takes out a lot of the guesswork. http://www.rst-engr.com/rst/jimsdata/index.html -----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 Sent: Thursday, March 22, 2007 11:24 PM Subject: Re: AeroElectric-List: Wire size dilemma --> > > >Ok, so I'm planning on a dual alt/batt 24v setup for a Lancair legacy. >Batteries will be mounted behind the seats, a single 24v Concorde, and >a backup B&C. I'm stuck on wire sizes to accommodate my goals. Wonder >if anyone would care to comment. I had planned to run #2 between the >starter contactor and the starter (both will be on the firewall). Then >#4 between the Main alternator (a 100A 24v version) the starter >contactor and the main batt contactor (which will be at the batteries >about 5ft behind the firewall). Because the standby alternator is only >20A and a backup, was going to run #8 for it thru the firewall, to the >battery contact/cross tie. Mine you, the cross tie will be "strap" >connected so it won't actually be wire there. > >But after seeing a few larger airplanes, I started to re-think this >plan. Perhaps I should use #2 for everything on the Main battery side, >and stay either with #8 or go to #6 or #4 on the standby side. > >Trying to avoid losses over length, etc. I've looked thru everything I >can find on Bob's site, but most of them are for 60A alternators on the >main side and 12v, so I'm really not sure what to do. > >Any takers? > >To help with a little more placement info. The firewall will have the >starter contactor only, the batteries are about 5-7 (wire feet) behind >the firewall, the battery and cross tie contactors will be at the >batteries. I'd run a 2AWG ground for both batteries. Put crosstie contactor on firewall to use as fwd distribution point for the two systems. Run 2AWG for all fat wires on the main battery(+) side and 4AWG for fat wires on the auxiliary battery(+) side. P.S. Use welding cable for jumpers from battery(-) terminals to common gnd and battery(+) terminals to their respective contactors. Use what ever style wire you like for other conductors. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Subject: Wire size dilemma
Date: Mar 23, 2007
From: <longg(at)pjm.com>
Alan, Just thought of something else. As Bob indicated (contactors on the firewall) Lancair sells a pre-built mountable package which includes the contactors, fuses etc. I assume you are using the Lyc 540? I am doing a similar thing with the Subaru engine except my two batteries will be supported by a single alternator for the electrically dependent engine. It still makes sense to keep the battery contactor near the batteries. For these glass boats we need to run a fat 02 ground from the engine back to the common ground behind the seat. Let me know what you work out for your battery boxes; I've not designed mine yet. -----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 Sent: Thursday, March 22, 2007 11:24 PM Subject: Re: AeroElectric-List: Wire size dilemma --> > > >Ok, so I'm planning on a dual alt/batt 24v setup for a Lancair legacy. >Batteries will be mounted behind the seats, a single 24v Concorde, and >a backup B&C. I'm stuck on wire sizes to accommodate my goals. Wonder >if anyone would care to comment. I had planned to run #2 between the >starter contactor and the starter (both will be on the firewall). Then >#4 between the Main alternator (a 100A 24v version) the starter >contactor and the main batt contactor (which will be at the batteries >about 5ft behind the firewall). Because the standby alternator is only >20A and a backup, was going to run #8 for it thru the firewall, to the >battery contact/cross tie. Mine you, the cross tie will be "strap" >connected so it won't actually be wire there. > >But after seeing a few larger airplanes, I started to re-think this >plan. Perhaps I should use #2 for everything on the Main battery side, >and stay either with #8 or go to #6 or #4 on the standby side. > >Trying to avoid losses over length, etc. I've looked thru everything I >can find on Bob's site, but most of them are for 60A alternators on the >main side and 12v, so I'm really not sure what to do. > >Any takers? > >To help with a little more placement info. The firewall will have the >starter contactor only, the batteries are about 5-7 (wire feet) behind >the firewall, the battery and cross tie contactors will be at the >batteries. I'd run a 2AWG ground for both batteries. Put crosstie contactor on firewall to use as fwd distribution point for the two systems. Run 2AWG for all fat wires on the main battery(+) side and 4AWG for fat wires on the auxiliary battery(+) side. P.S. Use welding cable for jumpers from battery(-) terminals to common gnd and battery(+) terminals to their respective contactors. Use what ever style wire you like for other conductors. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 24, 2007
From: Bill Bradburry <bbradburry(at)allvantage.com>
Subject: Low Voltage Warning/Aux Battery Management Module
I purchased the board from Bob's site and the components from Digikey. I then tried to assemble the module as per the instructions here... http://www.aeroelectric.com/articles/lvwarn/LVWarn-ABMM.pdf It looks like a simple board, so I thought that I could do it even with my skills??? Well, DUH!! When I turn on the master, the 3 amp fuse immediately blows! I have absolutely no idea how to go about trying to troubleshoot this board. Can some of you guys give me some leadership here? Please don't talk about testers more than a cheap volt/ohm meter and be pretty specific about how to use even that..:>) Thanks for your help. Bill B ________________________________________________________________________________
Date: Mar 25, 2007
From: Dennis Haverlah <clouduster(at)austin.rr.com>
Subject: Capacitors for Whelen strobe power supply
A friend gave me his Whelen strobe power supply. It was still cycling but not firing the strobes. Whelen will not repair it because they no longer support this unit. I checked the capacitors and found one of the two main capacitors has low resistance - partial short I believe. I'd like to try to make it work again for use in my RV 7A. The capacitors are 400UF - 300 VDC. They were manufactured by Sprague and have the # D77072 on the aluminum case. Also the numbers 7821L 19-03 are also on the case. Does anyone have a source I can purchase 2 from? I have looked on the web but don't know which capacitor design these are - aluminum, electroletic, etc. Thanks much, Dennis H. ________________________________________________________________________________
From: Speedy11(at)aol.com
Date: Mar 25, 2007
Subject: Good Deal on Power Guard
If anyone is interested, I have a 12V Composite Design Power Guard (see it at _http://www.compositedesigninc.com/Power_Guard.htm_ (http://www.compositedesigninc.com/Power_Guard.htm) ) that I don't need and I'll sell it at 40% off retail with free shipping. If you want photos send me a note off the list at speedy11 at aol.com. It is new, unused and never installed. It doesn't fit my needs but maybe someone on this list can use it. Stan Sutterfield ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: There is no 'ineptness'
Date: Mar 25, 2007
.......only ineptitude. Ferg Kyle ________________________________________________________________________________
From: "James Foerster" <jmfpublic(at)comcast.net>
Subject: re: Capacitors for Whelen strobe power supply
Date: Mar 25, 2007
Dennis, Digikey catalog lists 12 different capacitors, 9 of which are in stock, which would work for you if they fit mechanically. These are all 350v at 390UF units. You can use anything rated 300 volts or better, and the 400UF is rather approximate, as the electrolytics are rated + and - 20%. It seems that 390 UF is now commonly used. Prices run from the $5 to $7 range. I will try to send you the results of the search on the Digikey site privately. Below are 390UF at 350v units: Diameter(mm) Length(mm) P11920-ND 25 40 P11921-ND 30 30 P11790-ND 25 45 P11791-ND 30 30 There are others, but mainly the ratings differ for service life at rated temperature. The first two are 3000 hr at 85 degrees C, the next two are 2000 hr at 105 degrees C. Search for these part numbers on the Digikey site, and they will lead you to all the information. Jim Foerster J400 wiring-veerry sloooly ________________________________________________________________________________
Date: Mar 26, 2007
From: Ken <klehman(at)albedo.net>
Subject: Re: re: Capacitors for Whelen strobe power supply
Careful guys. There is more to this. For proper performance and decent life you need "photoflash" capacitors specifically designed for fast high current discharge. They tend to be more difficult to find. Ken James Foerster wrote: > Dennis, > > Digikey catalog lists 12 different capacitors, 9 of which are in > stock, which would work for you if they fit mechanically. These are > all 350v at 390UF units. You can use anything rated 300 volts or > better, and the 400UF is rather approximate, as the electrolytics are > rated + and - 20%. It seems that 390 UF is now commonly used. Prices > run from the $5 to $7 range. I will try to send you the results of > the search on the Digikey site privately. Below are 390UF at 350v units: > > Diameter(mm) Length(mm) > P11920-ND 25 40 > P11921-ND 30 30 > P11790-ND 25 45 > P11791-ND 30 30 > > There are others, but mainly the ratings differ for service life > at rated temperature. The first two are 3000 hr at 85 degrees C, the > next two are 2000 hr at 105 degrees C. > > Search for these part numbers on the Digikey site, and they will lead > you to all the information. > > Jim Foerster J400 wiring-veerry sloooly ________________________________________________________________________________
Subject: Good Deal on Power Guard
Date: Mar 26, 2007
From: <longg(at)pjm.com>
Looks interesting. How would this interact with Bob's design for a electrically dependent engine? Does it buy anything over what Bob's schematic is doing? Glenn -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Speedy11(at)aol.com Sent: Sunday, March 25, 2007 9:46 PM To: aeroelectric-list(at)matronics.com Subject: [Probable SPAM] AeroElectric-List: Good Deal on Power Guard If anyone is interested, I have a 12V Composite Design Power Guard (see it at http://www.compositedesigninc.com/Power_Guard.htm) that I don't need and I'll sell it at 40% off retail with free shipping. If you want photos send me a note off the list at speedy11 at aol.com. It is new, unused and never installed. It doesn't fit my needs but maybe someone on this list can use it. Stan Sutterfield ________________________________ AOL.com. ________________________________________________________________________________
From: "JOHN TIPTON" <jmtipton(at)btopenworld.com>
Subject: Earth return
Date: Mar 26, 2007
Hi Guys Can you please confirm that it is good (aircraft) practice to have in addition to an earth return wire to the main earth 'bus' a local earth connection, for example, at the wing tip for the navigation and landing lights. Best regards - John ________________________________________________________________________________
Subject: Earth return
Date: Mar 26, 2007
From: "George, Neal E Capt MIL USAF 605TES/TSI" <Neal.George(at)hurlburt.af.mil>
John - Bob has often suggested that simple resistive loads such as lights and pitot heat are perfect candidates for local airframe grounding - and that's exactly what I did. Neal George RV-7 N8ZG (Contemplating the Cowling) Z13-8 (Do we ever really finish wiring ?) --> Hi Guys Can you please confirm that it is good (aircraft) practice to have in addition to an earth return wire to the main earth 'bus' a local earth connection, for example, at the wing tip for the navigation and landing lights. Best regards - John ________________________________________________________________________________
From: "Alex" <alex157(at)pwhome.com>
Subject: Current Sensor Placement
Date: Mar 26, 2007
I have a dual alternator / dual battery setup- my question is can I somehow just use the single hall effect current sensor I have to determine output of either/or alternator or do I need to get 2 of them and use a toggle? I was thinking that possibly I could pass both alternator output wires through the ring and then it would measure all current passing through regardless of where it was coming from, but I am not sure if it will work this way, or is there another solution- maybe put the sensor on the single ground cable that goes to both batteries? ________________________________________________________________________________
Subject: Re: Current Sensor Placement
Date: Mar 26, 2007
From: "Glaeser, Dennis A" <dennis.glaeser(at)eds.com>
Hall effect sensors work just fine with multiple wires running through them. The reported current is the total what is running through all of the wires. In fact, you can loop the same wire through the sensor to get higher readings. If you want independent readings, you need independent sensors. Hooking 2 sensors to the same display, or EIS/EFIS input with a toggle means they have to be calibrated the same (or at least close enough :-) Dennis Glaeser ------------------------------------------------------------------------ ----- From:Alex I have a dual alternator / dual battery setup- my question is can I somehow just use the single hall effect current sensor I have to determine output of either/or alternator or do I need to get 2 of them and use a toggle? I was thinking that possibly I could pass both alternator output wires through the ring and then it would measure all current passing through regardless of where it was coming from, but I am not sure if it will work this way, or is there another solution- maybe put the sensor on the single ground cable that goes to both batteries? ________________________________________________________________________________
Date: Mar 26, 2007
From: Leo Holler <leoh(at)gci.net>
Subject: Double row breaker panel
Anyone have experience (or comments) with installing a two-row breaker panel. My application would fit nice if I could put my main bus over my endurance bus, using Klixon 7277's or similar (all of the same exterior dimensions) and using no more than 2.25" to 2.5" total vertical space. The panel would unscrew from the instrument panel and could be worked on on one's lap. I have plenty of space for extra wire behind the panel. Am I dreaming or can it be done? I fully appreciate the benefits of using a fuse panel instead, but this is a certified ship and soon to be sold. In my area IA's are not very inclined toward fuses but they are very involved with the sale of an aircraft, thus the use of breakers. Thanks for any comments/suggestions. Leo Holler leoh(at)gci.net PA-22/20 Alaska ________________________________________________________________________________
Date: Mar 26, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Low Voltage Warning/Aux Battery Management Module
> > >I purchased the board from Bob's site and the components from Digikey. I >then tried to assemble the module as per the instructions here... > >http://www.aeroelectric.com/articles/lvwarn/LVWarn-ABMM.pdf > >It looks like a simple board, so I thought that I could do it even with my >skills??? Well, DUH!! > >When I turn on the master, the 3 amp fuse immediately blows! I have >absolutely no idea how to go about trying to troubleshoot this board. > >Can some of you guys give me some leadership here? Please don't talk >about testers more than a cheap volt/ohm meter and be pretty specific >about how to use even that..:>) > >Thanks for your help. > >Bill B Drop it to me in the mail and I'll trouble shoot it, fix it and tell you what I found and how I found it. I've built a couple hundred of these critters and can probably find it pretty quick. On the other hand, if it's blowing fuses, it sounds like a hard short. Check for solder splashes on the connector pins. I can't think of any component placement error that would draw that much current. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 26, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: re: Capacitors for Whelen strobe power supply
> >Careful guys. There is more to this. >For proper performance and decent life you need "photoflash" capacitors >specifically designed for fast high current discharge. >They tend to be more difficult to find. >Ken yeah . . . but I've had pretty good luck with plain-vanilla replacements. The cost is sure right and if you're willing to replace the first set of bad ones at all, then the idea of putting a new set in every couple of years is probably not repulsive either. I never got a report back from the owners that I serviced with non-specialty caps many moons ago. I presume they offered satisfactory service for awhile. It would be interesting to see how long the PV caps last got someone who hangs out here on the list. Bob . . . ________________________________________________________________________________
Date: Mar 26, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Double row breaker panel
>Anyone have experience (or comments) with installing a two-row breaker >panel. My application would fit nice if I could put my main bus over my >endurance bus, using Klixon 7277's or similar (all of the same exterior >dimensions) and using no more than 2.25" to 2.5" total vertical space. The >panel would unscrew from the instrument panel and could be worked on on >one's lap. I have plenty of space for extra wire behind the panel. Am I >dreaming or can it be done? > >I fully appreciate the benefits of using a fuse panel instead, but this is >a certified ship and soon to be sold. In my area IA's are not very >inclined toward fuses but they are very involved with the sale of an >aircraft, thus the use of breakers. That will work and it's been done. Would they be more receptive if you had a copy of a 337 where the fuseblocks were installed on a Grumman Tiger? Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: "Jim Baker" <jlbaker(at)msbit.net>
Date: Mar 26, 2007
Subject: Re: Double row breaker panel
X-mailer: Pegasus Mail for Windows (4.41) > >Anyone have experience (or comments) with installing a two-row breaker > >panel. > That will work and it's been done. Would they > be more receptive if you had a copy of a 337 where > the fuseblocks were installed on a Grumman Tiger? > > Bob . . . My Bellanca Viking has a dual row breaker set-up......ask me again how easy it is to work on that top row....go ahead, just ask! If you could make a removable access panel it might work.... Jim Baker 580.788.2779 Elmore City, OK ________________________________________________________________________________
Date: Mar 27, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Fwd: Re: re: Capacitors for Whelen strobe power supply
Here's a note I received on one fellows success with replacing flash-rated capacitors with plain-vanilla electrolytics. His confirmation of my past experiences suggests that the experiment is worth repeating. >Hey, Bob, I'm just a lurker in the archives, but I have replaced the >electrolytics in two Whelen strobe supplies.... Worked fine then and is >working fine now. Some spray-on conformal coating helps cut down on the >high-voltage corrosion in the units. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 27, 2007
From: Bill Bradburry <bbradburry(at)allvantage.com>
Subject: Low Voltage Warning/Aux Battery Management Module
Thanks, Bob! My buddy at the airport has offered to look at the board. He has it now. If he comes up empty handed...(not likely :>)) I will take you up on the offer. Bill B > From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net> > Subject: Re: AeroElectric-List: Low Voltage Warning/Aux Battery Management Module > > > >> > >> > >> >I purchased the board from Bob's site and the components from Digikey. I >> >then tried to assemble the module as per the instructions here... >> > >> >http://www.aeroelectric.com/articles/lvwarn/LVWarn-ABMM.pdf >> > >> >It looks like a simple board, so I thought that I could do it even with my >> >skills??? Well, DUH!! >> > >> >When I turn on the master, the 3 amp fuse immediately blows! I have >> >absolutely no idea how to go about trying to troubleshoot this board. >> > >> >Can some of you guys give me some leadership here? Please don't talk >> >about testers more than a cheap volt/ohm meter and be pretty specific >> >about how to use even that..:>) >> > >> >Thanks for your help. >> > >> >Bill B > > Drop it to me in the mail and I'll trouble shoot > it, fix it and tell you what I found and how I > found it. > > I've built a couple hundred of these critters > and can probably find it pretty quick. > > On the other hand, if it's blowing fuses, it sounds > like a hard short. Check for solder splashes on the > connector pins. I can't think of any component placement > error that would draw that much current. > > Bob . . . ________________________________________________________________________________
Subject: Re: Fwd: Re: re: Capacitors for Whelen strobe power
supply
Date: Mar 27, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Yes I did the same, I had a pair of Aeroflash units in my old Zodiac. Standard repair for each Aeroflash was $50. Standard capacitor was $10 and 10 minutes with a soldering iron. I only used to get a couple of years per capacitor but that seemed no worse than the Caps the Aeroflashers came with. Cheers Frank -----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 Sent: Tuesday, March 27, 2007 7:55 AM Subject: AeroElectric-List: Fwd: Re: re: Capacitors for Whelen strobe power supply --> Here's a note I received on one fellows success with replacing flash-rated capacitors with plain-vanilla electrolytics. His confirmation of my past experiences suggests that the experiment is worth repeating. >Hey, Bob, I'm just a lurker in the archives, but I have replaced the >electrolytics in two Whelen strobe supplies.... Worked fine then and is >working fine now. Some spray-on conformal coating helps cut down on >the high-voltage corrosion in the units. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: Speedy11(at)aol.com
Date: Mar 27, 2007
Subject: Re: Good Deal on Power Guard
I understand from the manufacturer that it does the same thing as Bob's concept. It's designed around having two alternators. I don't believe it adds anything beyond Bob's concept except that it is ready to mount and connect. Send a note to the builder (via his web site) and ask about the operation. I bought it before I had settled on my final electric plan and I've decided to use two batteries instead of two alternators. Stan Sutterfield Looks interesting. How would this interact with Bob's design for a electrically dependent engine? Does it buy anything over what Bob's schematic is doing? Glenn If anyone is interested, I have a 12V Composite Design Power Guard (see it at http://www.compositedesigninc.com/Power_Guard.htm) that I don't need and I'll sell it at 40% off retail with free shipping. If you want photos send me a note off the list at speedy11 at aol.com. It is new, unused and never installed. It doesn't fit my needs but maybe someone on this list can use it. Stan Sutterfield ________________________________________________________________________________
From: "Keith Hallsten" <KeithHallsten(at)quiknet.com>
Subject: RE: Earth return
Date: Mar 27, 2007
John, Each circuit needs only one ground. The advantage of using a local (airframe) ground in a metal airplane is that a separate ground wire need not be threaded through the structure. If you elect to use a separate ground wire then there is no advantage to using a local ground. In fact, there may be a disadvantage because the possibility of ground loops would then exist. Regards, Keith Hallsten Roseville, CA John Tipton wrote: Hi Guys Can you please confirm that it is good (aircraft) practice to have in addition to an earth return wire to the main earth 'bus' a local earth connection, for example, at the wing tip for the navigation and landing lights. Best regards - John ________________________________________________________________________________
Date: Mar 27, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Low Voltage Warning/Aux Battery Management Module
> > >Thanks, Bob! My buddy at the airport has offered to look at the >board. He has it now. If he comes up empty handed...(not likely :>)) >I will take you up on the offer. Very well. Holler if we can help! Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 27, 2007
From: Todd Heffley <list(at)toddheffley.com>
Subject: Re: Double row breaker panel
I have done this many times. Here is the secret. All of the wires..... and I mean ALL OF THE WIRES must go to one side of the breaker panel. This allows the panel to be angled 90 degrees out from the panel for very easy service. No need for a silly 2 foot long service loop. Did I mention that ALL OF THE WIRES MUST EXIT TO ONE SIDE? Avionics Installer hell is where removeable service panels have wires run willy nilly in all directions, so that the panel cannot be moved away from the instrument panel. Todd ________________________________________________________________________________
Date: Mar 27, 2007
From: frequent flyer <jdhcv(at)yahoo.com>
Subject: Lightspeed Electronic Ignition
I have one of the original ignition systems from Lightspeed which was purchased in 1992 by a friend who is now deceased. I am going to install it on my IO-360 but am missing the manual. I have the newer manual but it doesn't answer all my questions. If any of you have the manual for the Model CD 4 CYL AEI 42 which was discontinued in 1995 I'd sure appreciate a copy of it. Thanks, Jack In AZ --------------------------------- TV dinner still cooling? Check out "Tonight's Picks" on Yahoo! TV. ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: RE: Earth return
>John, > >Each circuit needs only one ground. The advantage of using a local >(airframe) ground in a metal airplane is that a separate ground wire need >not be threaded through the structure. If you elect to use a separate >ground wire then there is no advantage to using a local ground. In fact, >there may be a disadvantage because the possibility of ground loops would >then exist. > >Regards, > >Keith Hallsten Good catch Keith. I'd missed the "in addition" phrase in his query. Bob . . . >Roseville, CA > >John Tipton wrote: > >Hi Guys > >Can you please confirm that it is good (aircraft) practice to have in > >addition to an earth return wire to the main earth 'bus' a local earth > >connection, for example, at the wing tip for the navigation and landing > >lights. > >Best regards - John ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Rear Mounted Batteries in Z-14
>Comments/Questions: Bob, > >First, thank you for all you do and have done to support the Experimental >Aircraft community over the years. I have had your materials and >reference your web site on a VERY frequent basisgreat stuff! Thank you for the kind words . . . > I am now building an RV-10, and plan on using the Z-14 dual battery > configuration. I am pretty much decided on using two of the 600 amp > Odyssey batteries, mounted side by side in the standard rear tailcone > configuration. > > From a configuration perspective, Is it acceptable to locate both battery > contactor relays near the rear mounted batteries? That's where they're supposed to go. Battery contactors and battery busses are mounted adjacent to their respective batteries. Irrespective of what kind of wire you use for other "fat wires" in the airplane, consider the use of 4AWG, welding cable jumpers from battery(+) and battery(-) terminals to their local attach points. >Assuming the foregoing is acceptable, is it sufficient for me to use one >#4 wire from the positive side of each contactor forward to the starter >contactor and cross-feed contactor appropriately? I think this will be fine. >Is it OK to use one wire for the battery ground from the rear batteries >forward to the firewall? By that I mean can I use a single say #2 wire to >bring the ground forward to the firewall ground bus locations? Ground batteries locally, each to a separate tab riveted to most robust structure available. See: http://aeroelectric.com/articles/Battery_Grounds/Battery_Grounds.html >You recommend the main battery bus connection to the main battery >contactor (usually a #10 wire) be kept less than 6 inches. Obviously if >the battery contactor is located aft, that is not possible. Do I need to >fuse-protect the line, or increase the wire size? It IS possible because the always hot busses are located next to their respective batteries. >Bob, Thank you again in advance! My pleasure sir! Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
From: "David Lamphere" <lamphere(at)earthlink.net>
Subject: Re: Rear Mounted Batteries - more questions
Date: Mar 28, 2007
Bob, Now you are confusing me.. Yes, I did look at the link you provided. Using the generic aircraft - single battery schematic for schematic on metal tube frame. Battery (Odyssey 680) and contactor will be located under baggage compartment floor behind seat backs. I thought we were supposed to run a ground wire from the battery to the brass ground bus plate (with all the quick connect tabs on it) which was to be mounted on the firewall. Isn't using the airframe for ground now generating two paths for ground - hence possible problems? I'm about ready to wire in my rear mounted battery (before covering). I will use flexible wire for the battery terminal connections (and to the local ground if that's what I am supposed to do). No problem attaching ground leads to the frame if a good idea. It would eliminate an extra wire to top and bottom strobes and tail position light... but I was already resolved to run + and gnd to each (using a small local-next to battery version of the brass ground bus with quick disconnects like in the front) I'd appreciate your input. Thanks, Dave ----- Original Message ----- From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net> Sent: Wednesday, March 28, 2007 7:38 AM Subject: AeroElectric-List: Rear Mounted Batteries in Z-14 > > > >Comments/Questions: Bob, > > > >First, thank you for all you do and have done to support the Experimental > >Aircraft community over the years. I have had your materials and > >reference your web site on a VERY frequent basisgreat stuff! > > Thank you for the kind words . . . > > > > I am now building an RV-10, and plan on using the Z-14 dual battery > > configuration. I am pretty much decided on using two of the 600 amp > > Odyssey batteries, mounted side by side in the standard rear tailcone > > configuration. > > > > From a configuration perspective, Is it acceptable to locate both battery > > contactor relays near the rear mounted batteries? > > That's where they're supposed to go. Battery contactors and battery > busses are mounted adjacent to their respective batteries. Irrespective > of what kind of wire you use for other "fat wires" in the airplane, > consider the use of 4AWG, welding cable jumpers from battery(+) and > battery(-) terminals to their local attach points. > > >Assuming the foregoing is acceptable, is it sufficient for me to use one > >#4 wire from the positive side of each contactor forward to the starter > >contactor and cross-feed contactor appropriately? > > I think this will be fine. > > >Is it OK to use one wire for the battery ground from the rear batteries > >forward to the firewall? By that I mean can I use a single say #2 wire to > >bring the ground forward to the firewall ground bus locations? > > Ground batteries locally, each to a separate tab riveted > to most robust structure available. See: > > http://aeroelectric.com/articles/Battery_Grounds/Battery_Grounds.html > > > >You recommend the main battery bus connection to the main battery > >contactor (usually a #10 wire) be kept less than 6 inches. Obviously if > >the battery contactor is located aft, that is not possible. Do I need to > >fuse-protect the line, or increase the wire size? > > It IS possible because the always hot busses are located > next to their respective batteries. > > > >Bob, Thank you again in advance! > > My pleasure sir! > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > ________________________________________________________________________________
Date: Mar 28, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: Double row breaker panel
Todd Heffley wrote: > > Did I mention that ALL OF THE WIRES MUST EXIT TO ONE SIDE? > > Avionics Installer hell is where removeable service panels have wires > run willy nilly in all directions, so that the panel cannot be moved > away from the instrument panel. > > > Todd Todd, thank you. Some ideas are so fundamental, useful, and obvious...AFTER they are pointed out to you. (Excuse me while I go re-route a few wires.) -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: Rear Mounted Batteries - more questions
> > >Bob, > >Now you are confusing me.. > >Yes, I did look at the link you provided. > >Using the generic aircraft - single battery schematic for schematic on >metal tube frame. >Battery (Odyssey 680) and contactor will be located under baggage >compartment floor behind seat backs. > >I thought we were supposed to run a ground wire from the battery to the >brass ground bus plate (with all the quick connect tabs on it) which was >to be mounted on the firewall. Isn't using the airframe for ground now >generating two paths for ground - hence possible problems? Local grounds in all metal airplanes can practically depart from "ideal" for the following: Batteries, strobe supplies, landing/taxi lights, pitot heaters, position lights, hydraulic pumps for landing gear (because they're intermittent) but not for air-conditioning compressors (because they're continuous). >I'm about ready to wire in my rear mounted battery (before covering). I >will use flexible wire for the battery terminal connections (and to the >local ground if that's what I am supposed to do). No problem attaching >ground leads to the frame if a good idea. It would eliminate an extra wire >to top and bottom strobes and tail position light... but I was already >resolved to run + and gnd to each (using a small local-next to battery >version of the brass ground bus with quick disconnects like in the front) > >I'd appreciate your input. It's never 'bad' to run all electro-whizzies to a single point ground but if one wishes to take advantage of the ground-friendly, all-metal airplane with the cited compromises, there's no risk of having an unhappy noise moment. It's most important to pay attention to grounding potential victims such as avionics and instrumentation. These should return to the firewall ground point per Z-15. I'll add some notes to Z-15 next revision to clarify this point. Bob . . . ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: SD8 Connection queries
>I wanted to get away from using the essential bus. If you were just going >to use a common bus do you think it would be practical to have the SD8 & >the battery feeding this via some sort of cross tie / switch. In the event >of a alternator & main contactor failure you would then be able to supply >the bus from a combination of the SD8 & the battery. In hindsight the >chance of 2 components failing at the same time is statistically >irrelevant, still I am planning some long flights so want the best >system can devise. Just tie the SD-8 to the downstream side of the downstream side of the battery contactor instead of the upstream side and leave the e-bus off. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: SD8 Connection queries
>I have a SD8 standby alternator on my RV7 & am considering the various >options for connecting it into the aircraft wiring. I have been looking at >Bobs Z-8 diagram which uses an essential bus & cross tie. I would rather >not have the essential bus & just have a way of connecting the both the >SD8 & the battery into the main bus should the battery contactor fail as I >see this as a single point of failure. Has anyone done something similar >or is there another wiring diagram out there that shows another way of >doing this. Wire the SD-8 for self excitation and it will run without a battery. If you're worried about the battery contactor then dual battery contactors would fix that one. But then, that's heavier than an e-bus. I don't understand what optimization you perceive over Z-13/8 as published. Bob . . . ---------------------------------------- ( IF one aspires to be "world class", ) ( what ever you do must be exercised ) ( EVERY day . . . ) ( R. L. Nuckolls III ) ---------------------------------------- ________________________________________________________________________________
Subject: Rear Mounted Batteries - more questions
Date: Mar 28, 2007
From: <longg(at)pjm.com>
Wednesday battery installation tip. I am relatively new to this wiring stuff, but I have had the experience of replacing all of the battery, starter etc cables in a Piper 67' PA140. Believe it or not, they had a pretty good setup for a rear mounted battery. They had a really silly set of jumpers wires connected/welded to the battery box and routed through grommets on the box to the battery (eliminated by Aircraft Spruce upgrade kit), but the layout will provide anyone hoping to install rear mounted batteries with a very clear picture of how things are done. Visit your FBO and ask someone to let you look under the rear seat (there's always a 140 around). Take a picture of the layout. One note about their setup is that they installed the starter contactor on firewall and run a #6? from the rear up the left side, through the firewall to the contactor and then to the starter which is up front on the Lycoming. I was very proud of my first wiring job and gladly threw that old stuff in the trash. The engine turned over 3x faster with the new cables etc. I am installing dual batteries rear of the rear bulkhead in my new Legacy and will use the pictures I took to help with the layout. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of David Lamphere Sent: Wednesday, March 28, 2007 9:19 AM Subject: Re: AeroElectric-List: Rear Mounted Batteries - more questions --> Bob, Now you are confusing me.. Yes, I did look at the link you provided. Using the generic aircraft - single battery schematic for schematic on metal tube frame. Battery (Odyssey 680) and contactor will be located under baggage compartment floor behind seat backs. I thought we were supposed to run a ground wire from the battery to the brass ground bus plate (with all the quick connect tabs on it) which was to be mounted on the firewall. Isn't using the airframe for ground now generating two paths for ground - hence possible problems? I'm about ready to wire in my rear mounted battery (before covering). I will use flexible wire for the battery terminal connections (and to the local ground if that's what I am supposed to do). No problem attaching ground leads to the frame if a good idea. It would eliminate an extra wire to top and bottom strobes and tail position light... but I was already resolved to run + and gnd to each (using a small local-next to battery version of the brass ground bus with quick disconnects like in the front) I'd appreciate your input. Thanks, Dave ----- Original Message ----- From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net> Sent: Wednesday, March 28, 2007 7:38 AM Subject: AeroElectric-List: Rear Mounted Batteries in Z-14 > --> > > > >Comments/Questions: Bob, > > > >First, thank you for all you do and have done to support the > >Experimental > >Aircraft community over the years. I have had your materials and > >reference your web site on a VERY frequent basis...great stuff! > > Thank you for the kind words . . . > > > > I am now building an RV-10, and plan on using the Z-14 dual battery > > configuration. I am pretty much decided on using two of the 600 amp > > Odyssey batteries, mounted side by side in the standard rear tailcone > > configuration. > > > > From a configuration perspective, Is it acceptable to locate both > > battery > > contactor relays near the rear mounted batteries? > > That's where they're supposed to go. Battery contactors and battery > busses are mounted adjacent to their respective batteries. Irrespective > of what kind of wire you use for other "fat wires" in the airplane, > consider the use of 4AWG, welding cable jumpers from battery(+) and > battery(-) terminals to their local attach points. > > >Assuming the foregoing is acceptable, is it sufficient for me to use > >one > >#4 wire from the positive side of each contactor forward to the starter > >contactor and cross-feed contactor appropriately? > > I think this will be fine. > > >Is it OK to use one wire for the battery ground from the rear > >batteries > >forward to the firewall? By that I mean can I use a single say #2 wire to > >bring the ground forward to the firewall ground bus locations? > > Ground batteries locally, each to a separate tab riveted > to most robust structure available. See: > > http://aeroelectric.com/articles/Battery_Grounds/Battery_Grounds.html > > > >You recommend the main battery bus connection to the main battery > >contactor (usually a #10 wire) be kept less than 6 inches. Obviously if > >the battery contactor is located aft, that is not possible. Do I need to > >fuse-protect the line, or increase the wire size? > > It IS possible because the always hot busses are located > next to their respective batteries. > > > >Bob, Thank you again in advance! > > My pleasure sir! > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > ________________________________________________________________________________
Date: Mar 28, 2007
From: Dennis Haverlah <clouduster(at)austin.rr.com>
Subject: Re: Fwd: Re: re: Capacitors for Whelen strobe power
supply I want to thank everyone for the information on strobe capacitors. I have ordered some from Digi-key and will let the list know how they work. Dennis H. Robert L. Nuckolls, III wrote: > > > Here's a note I received on one fellows success with > replacing flash-rated capacitors with plain-vanilla > electrolytics. > > His confirmation of my past experiences suggests that > the experiment is worth repeating. > > >> Hey, Bob, I'm just a lurker in the archives, but I have replaced the >> electrolytics in two Whelen strobe supplies.... Worked fine then and >> is working fine now. Some spray-on conformal coating helps cut down >> on the high-voltage corrosion in the units. > > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > > ________________________________________________________________________________
From: "John Burnaby" <jonlaury(at)impulse.net>
Subject: Re: Lightspeed Electronic Ignition
Date: Mar 28, 2007
Did you talk to Klaus about getting a manual or an upgrade to the unit to match the newer manual? LSE @ (805) 933-3299 ________________________________________________________________________________
Date: Mar 28, 2007
From: Cleone Markwell <cleone(at)rr1.net>
Subject: New question
Glad that you are back. Always interested in what you have to say. While reconsidering my over voltage circuit I wondered about breaking one of the ac wires from the alternator (John Deer, same as Mark Langford) as a means of shutting down the alternator when the crowbar actuates the relay. What are your thoughts about this? Thanks, Cleone t 07:40 PM 3/27/2007, you wrote: > > > >> >> >>Thanks, Bob! My buddy at the airport has offered to look at the >>board. He has it now. If he comes up empty handed...(not likely :>)) >>I will take you up on the offer. > > Very well. Holler if we can help! > > Bob . . . > > ---------------------------------------- > ( IF one aspires to be "world class", ) > ( what ever you do must be exercised ) > ( EVERY day . . . ) > ( R. L. Nuckolls III ) > ---------------------------------------- > > ________________________________________________________________________________
Date: Mar 28, 2007
Subject: Re: Lightspeed Electronic Ignition
From: "Matt Prather" <mprather(at)spro.net>
Hi Jack, I think I have that model of ignition on my O-200 powered Varieze. It's the one with the small LSE box plus a red MSD box. I'll try to remember to grab the manual for it when I'm at the hangar tonight. Matt- > I have one of the original ignition systems from Lightspeed which was > purchased in 1992 by a friend who is now deceased. I am going to install > it on my IO-360 but am missing the manual. I have the newer manual but it > doesn't answer all my questions. If any of you have the manual for the > Model CD 4 CYL AEI 42 which was discontinued in 1995 I'd sure appreciate > a copy of it. > > Thanks, Jack In AZ > > > --------------------------------- > TV dinner still cooling? > Check out "Tonight's Picks" on Yahoo! TV. ________________________________________________________________________________
Date: Mar 28, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: New question
> >Glad that you are back. Always interested in what you have to say. While >reconsidering my over voltage circuit I wondered about breaking one of the >ac wires from the alternator (John Deer, same as Mark Langford) as a >means of shutting down the alternator when the crowbar actuates the >relay. What are your thoughts about this? Thanks, Cleone Revision 11J to Figure Z-16 does exactly that. I'm going to modify all the AC dynamo systems to do the same thing on Revision 12. Bob . . . ________________________________________________________________________________
Date: Mar 29, 2007
From: Ralph Hoover <hooverra(at)verizon.net>
Subject: DIY engine monitor
Try Rocky Mountain Instruments ( http://www.rkymtn.com/Home.htm -- Ralph C. Hoover RV7A hooverra at verizon dot net ________________________________________________________________________________
Date: Mar 29, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: DIY engine monitor
raymondj wrote: > >Greetings listers, > > I am looking at the possibility of making my own engine monitor. I would >like 6 CHT and 2 EGT. Any info on kits or plans would be appreciated. > > > You can get a Megaview kit to add to the Megasquirt DIY engine controller. http://www.megasquirt.org -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
From: "Ed Holyoke" <bicyclop(at)pacbell.net>
Subject: Lightspeed Electronic Ignition
Date: Mar 29, 2007
We've got an original Plasma ignition in our 6a. Apparently, the power supply transformers that he used in those run hotter than the ones he uses now. We had him replace ours after about 600 hours and it was pretty blackened. We also increased the size of the air port and hooked up an avionics fan to it to keep it cool. I'd give Klaus a call and talk it over with him. Have the serial # in your hand when you call. Pax, Ed Holyoke -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of frequent flyer Sent: Tuesday, March 27, 2007 7:47 PM Subject: AeroElectric-List: Lightspeed Electronic Ignition I have one of the original ignition systems from Lightspeed which was purchased in 1992 by a friend who is now deceased. I am going to install it on my IO-360 but am missing the manual. I have the newer manual but it doesn't answer all my questions. If any of you have the manual for the Model CD 4 CYL AEI 42 which was discontinued in 1995 I'd sure appreciate a copy of it. Thanks, Jack In AZ _____ TV dinner still cooling? Check out <http://us.rd.yahoo.com/evt=49979/*http:/tv.yahoo.com/> "Tonight's Picks" on Yahoo! TV. ________________________________________________________________________________
From: <bakerocb(at)cox.net>
Subject: Avionics Mounting
Date: Mar 30, 2007
3/30/2007 Hello Greg, Check out a not-so-cheap solution here http://www.radiorax.com/ and also to get some idea of what is involved in installing a stack of avionics. OC -- The best investment we can make is the effort to gather and understand knowledge. PS: That is a great selection of equipment. From: "Greg Vouga" <gmvouga(at)hotmail.com> Subject: Avionics-List: Avionics Mounting Hi All, I am hoping to get some info on mounting a stack of Garmin equipment in my RV-7A. I just received a GMA-340, GNS-430W, SL-30, and GTX-327 with mounting trays. I'm told that the rest of the mounting hardware such as screws, brackets, etc. are not included. I can start looking for low profile screws and fabricate brackets, but I don't want to re-invent the wheel if it's not necessary. Are there reasonably priced installation kits out there? How have others handled this? Thanks in advance, Greg gvouga(at)gmail.com ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 30, 2007
Subject: Re: Avionics Mounting
In a message dated 3/30/2007 8:01:56 A.M. Central Daylight Time, bakerocb(at)cox.net writes: Hello Greg, Check out a not-so-cheap solution here http://www.radiorax.com/ and also to get some idea of what is involved in installing a stack of avionics. Good Morning OC, For What It Is Worth; I installed a set of the RadioRax in my Bonanza a few years ago. They aren't cheap, but they sure work nice and the assistance from the manufacturer was terrific. Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
Date: Mar 30, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: Avionics Mounting
I have the same radio stack, just used .250 AL bar, and taped the holes for #8 screws. I also added 1 support in the rear of the stack. bakerocb(at)cox.net wrote: > > 3/30/2007 > > Hello Greg, Check out a not-so-cheap solution here > > http://www.radiorax.com/ > > and also to get some idea of what is involved in installing a stack of > avionics. > > OC -- The best investment we can make is the effort to gather and > understand knowledge. > > PS: That is a great selection of equipment. > > From: "Greg Vouga" <gmvouga(at)hotmail.com> > Subject: Avionics-List: Avionics Mounting > > Hi All, I am hoping to get some info on mounting a stack of Garmin > equipment in my > RV-7A. I just received a GMA-340, GNS-430W, SL-30, and GTX-327 with > mounting trays. I'm told that the rest of the mounting hardware such as > screws, brackets, etc. are not included. > > I can start looking for low profile screws and fabricate brackets, but I > don't want to re-invent the wheel if it's not necessary. Are there > reasonably priced installation kits out there? How have others handled > this? > > Thanks in advance, > > Greg > gvouga(at)gmail.com > > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 30, 2007
Subject: Re: Avionics Mounting
In a message dated 3/30/2007 8:39:20 A.M. Central Daylight Time, sam(at)fr8dog.net writes: I have the same radio stack, just used .250 AL bar, and taped the holes for #8 screws. I also added 1 support in the rear of the stack. Good Morning Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 30, 2007
Subject: Avionics Mounting
Good Morning Sam, The advantage (if there is any) to the RadioRax is that they are infinitely adjustable. If you want to rearrange or add anything to the stack, there is no need to drill new holes. With any of the more conventional strips, the new holes often conflict with old holes which will then require that a new support bar be fabricated and installed. If you are absolutely certain you will never want to change anything, there is little advantage to the RadioRax system. Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8 In a message dated 3/30/2007 8:39:20 A.M. Central Daylight Time, sam(at)fr8dog.net writes: I have the same radio stack, just used .250 AL bar, and taped the holes for #8 screws. I also added 1 support in the rear of the stack. 503 ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
From: "raymondj" <raymondj(at)frontiernet.net>
Subject: DIY engine monitor
Date: Mar 30, 2007
My apologies! I accidentally moved this discussion off list. This post brings it back to the list with no lost information. Raymond Julian Kettle River, MN archive -----Original Message----- From: BobsV35B(at)aol.com [mailto:BobsV35B(at)aol.com] Sent: Friday, March 30, 2007 8:13 AM Subject: OFF AeroElectric-List: DIY engine monitor In a message dated 3/30/2007 1:15:53 A.M. Central Daylight Time, raymondj(at)frontiernet.net writes: Greetings Bob, I am slightly familiar with GAMI's work on lean of peak operation and dispelling other OWTs as they call them. I haven't gone to deeply into their work because I will not have injectors. I was not familiar with the "lean test". If my understanding of the "lean test" is correct, when you fall over, you "leaned" too far. But seriously, if my understanding of the "lean test" is correct it will tell me the "spread" on my cylinders, indicating unequal distribution of fuel from the carb. The only way I can think of to change that would be to modify the intake manifold. This test will give useful info during R&D of the intake manifold, and I will use it then, but I can't think of any other time when I would apply it. If there is another application of this test I would like to learn of it. I appreciate your input. Thanks, Raymond Julian Kettle River, MN Good Morning Raymond, Your thought about using the information during R&D is dead on, but it is even more useful to check for changes that are occurring during normal operations. There is nothing I am aware of that works as well as fuel injection to attain an even mixture to all cylinders, but there are lot's of techniques that were used before fuel injection became common. The major problem has always been getting the same amount of air into each cylinder. The second challenge is getting the same amount of fuel in every parcel of air! The shape and length of intake tubes is one aspect. Leaks are a major problem. There is a potential for a change in the balance due to RPM and even the amount of manifold pressure available. In high performance automobile engines, the big boys claim that tuned intake and exhaust pipes can make a difference as to how much air gets into each cylinder. That is probably less of a factor in our low RPM engines, but Continental has made an effort in that direction with their newer top mounted intake pipe arrangement. Lycoming attacked the exhaust portion in the fifties with their crossover exhaust. Outside of the leaks, not much we can do there, but it is worth keeping in mind. Getting an even amount of fuel into each parcel of air is a bit easier. Introducing turbulence into the airflow can help whatever fuel is added to be distributed evenly throughout the air that does make it into the cylinder. Unfortunately, that same turbulence can interfere with the amount of air that flows! The temperature of the air will also affect the fuel distribution. Most of my experimentation has been with the six cylinder horizontally opposed Continentals that have been used in the Bonanzas. I bought my first one in 1954. It was a very old airplane at the time. Seven years old which we consider to be an antique on it's last legs, but it was all a poor young copilot could afford. Things sure have changed! Since I had just been to school on the latest, finest, and fastest airliner in the skies, the Douglas DC-7 with a Wright Turbo Compound engine, I was all up to date on the benefits of lean side operations. I started to seriously investigate the possibility of operating my Bonanza on the lean side of best power. The first order of business was to check the mixture distribution. My method was to slowly lean the engine and monitor the engine RPM. Since the early Bonanza was equipped with an electric controllable pitch propellor, it was a fixed pitch propellor when I was not actually changing the pitch by operating the pitch change system. As the mixture was leaned, the RPM would increase, then slowly start to decrease. I had read all of Charles Lindbergh's writings and that is the method he had used to determine the balance of his distribution. Peak RPM was peak power and anything beyond peak RPM placed the engine on the lean side. Lindbergh had mentioned that he normally leaned the Challenger engine for about a fifty RPM drop, though the precise RPM used was a number that had been given to him by a professor at the New York City University who had developed precise data for his use. I found that, on that first Bonanza, I could lean and the engine would smoothly drop until it finally quit. The engine never got rough at all. I had lucked out and had a distribution that was almost perfect at the RPM and manifold pressure being used. My next Bonanza had nowhere near as good distribution and got rough before the RPM even peaked! Why do I bore you with all this information? Because there are many things that can affect the distribution and a good engine monitor can be of great value in trouble shooting the imbalance. Sometimes I found that merely changing the RPM by fifty to one hundred RPM made things better. Other times, I could throttle back until I could see the very first indication of manifold pressure reduction and find the balance to be better. As I am sure you are aware, the last little bit of throttle movement does not open the throttle valve any further (it is already full open), but it does add more fuel via the enrichment valve or whatever arrangement is on that particular fuel delivery system. Throttling back in that manner probably improved things by changing the mixture flow just a bit or it may have been because the throttle valve has moved far enough to introduce a bit of turbulence. I even found that I could affect mixture balance by things as basic as getting better alignment of intake tubes. I also messed around with polishing the small brass tubes within the carburetor through which the fuel flowed. All of my random experimentation would have been much more productive if I had been equipped with a modern engine monitor and if I had thought about doing a lean test. To me, the data presented by GAMI is the first really useful knowledge given us about how to operate our engines since that nameless college professor explained it to Lindbergh in 1927. Do the GAMI lean test during the R&D phase for the educational virtues and to figure out how to improve things. Follow that with checks during normal operation to catch things that change! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 ---------------------------------------------------------------------------- ---- See what's free at AOL.com. ________________________________________________________________________________
From: "RV_10" <john_rv10(at)yahoo.com>
Subject: Avionics Mounting
Date: Mar 31, 2007
Hi Bob, Do you have any photos of your install that you could send to me? Thank you, John Cleary _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of BobsV35B(at)aol.com Sent: Saturday, 31 March 2007 1:56 AM Subject: Re: AeroElectric-List: Avionics Mounting In a message dated 3/30/2007 8:39:20 A.M. Central Daylight Time, sam(at)fr8dog.net writes: I have the same radio stack, just used .250 AL bar, and taped the holes for #8 screws. I also added 1 support in the rear of the stack. Good Morning Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 _____ See what's free at AOL.com <http://www.aol.com?ncid=AOLAOF00020000000503> . ________________________________________________________________________________
From: "Greg Vouga" <gmvouga(at)hotmail.com>
Subject: Avionics Mounting
Date: Mar 30, 2007
All, Due to the large amount of responses, I can't respond to everyone individually. However, rest assured that all of the responses were read and very much appreciated. What did people do 20 years ago wthout a resource such as this? Anyways, i've decided to move forward with the simple Aluminum angle technique. It's cheap and i have the stuff to complete it tomorrow. Thanks again to everyone that responded. Greg _________________________________________________________________ Interest Rates near 39yr lows! $430,000 Mortgage for $1,399/mo - Calculate new payment ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 31, 2007
Subject: Avionics Mounting
Good Evening John, I remember that I did document the installation quite thoroughly, but I can't find the pictures! May I suggest that you check the RadioRax website to see what they look like? _www.radiorax.com_ (http://www.radiorax.com/) Meanwhile, I will try to have one of my children help me find the lost images! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 3/30/2007 4:49:57 P.M. Central Daylight Time, john_rv10(at)yahoo.com writes: Hi Bob, Do you have any photos of your install that you could send to me? Thank you, John Cleary ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
Date: Mar 31, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: the battery dragon . . .
>Comments/Questions: I am building a Jabiru J430 and plan to include your >crowbar overvoltage system and low voltage detector. I am planning on a >dual battery where the second battery supports the main bus but not the >starter motor. The plan is to put a power diode between the bus and the >main battery. This means that that both batteries will charge from the >regulator but the second battery will not contribute to starting and >provide a sink to the bus to ensure voltage is maintained to the bus even >during starting. The idea is for the second battery to keep the electics >going in the event of main battery failure. Do you think this make sense? Unless you're planning not to maintain your battery, then 'battery failure' is exceedingly remote. The battery can be the most reliable source of power in the airplane. Since you've expressed a concern for keeping certain electro-whizzies operating under battery-only operations, (1) WHICH devices are the most useful, how much (2) CURRENT do they need and for (3) HOW LONG? After you've deduced these answers, what is your (4) PLAN for making sure that the battery in your airplane is up to the task? There are two qualifying tests of a battery. (5) LOAD testing proves the battery's ability to carry high loads such as starting the engine. This is the kind of test a service station operator puts on your car battery using a device similar to this one from Harbor Freight: http://www.aeroelectric.com/Pictures/Tools/HF91129_4.jpg Passing this test simply says the battery contains sufficient ENERGY delivered through a sufficiently LOW INTERNAL RESISTANCE to start the engine. The second test is a measure of (6) CAPACITY. This proves the battery's ability to perform under conditions (1), (2) and (3) above. It matters not how many batteries you install or how you wire them if you do not craft a preventative maintenance (a) PLAN to make sure your design goals for battery only endurance are met. The fact that you can get the engine started is but one of the two features that need monitoring. Further, unless you choose to meet an endurance load goal of a hand-full of minutes (like the FAA's favorite 30), then you'll need to establish some protocol for seeing that your goals are met throughout your ownership of the airplane. This will involve either (b) periodic replacement of what appears to be a perfectly good battery - cause it started the engine or (c) periodic CAPACITY TESTING against your personalized design goals defined by (1), (2) and (3) above. This can be easily accomplished with one battery but it does commit you to deciding which protocol offers the lowest cost of ownership. (b) throw a new $50 battery in every annual or (c) acquire the $tools$ and spend the $time$ to track your battery's condition such that design goals for battery only operations are consistently met. What you've proposed in your query does not make sense under the protocols established to operate your airplane at all times confident that the battery is going to be there to do the task you've established for it. The thing you need to do is establish PLAN (a) that will embrace the philosophy of (b) or (c) and then stick to it. If you do not have a copy of the 'Connection, I'll suggest you acquire or borrow one and review chapter 17 on system reliability. Join the AeroElectric-List and avail yourself of the knowledge, experience and understanding of dozens of folks who have slain the dragons you're concerned with. It doesn't need to be expensive or heavy. Bob . . . ________________________________________________________________________________
From: "Joe & Jan Connell" <jconnell(at)rconnect.com>
Subject: DIY engine monitor
Date: Mar 31, 2007
Guys, Some of the postings on this topic have discussed the work done by GAMI in regards to lean of peak. I might be incorrect but the GAMI folks are usually working with fuel injection, not carburetors. Please correct me if I'm wrong... Joe Connell ________________________________________________________________________________
From: "RV_10" <john_rv10(at)yahoo.com>
Subject: Rear Mounted Batteries - more questions
Date: Apr 01, 2007
Hello 'Lectric Bob, Thank you for all the fantastic effort you put into this group. It is extremely helpful to those of us with zero earlier experience in this area. I have read the Connection a couple of times and I have been pondering the whole issue of batteries and locations and fat wires etc. Attached is a schematic of a Z-14, architecture for rear batteries. This is not your current Z-14, and I don't know now where I got this from, but it very specifically states that the Aft Ground Buss is NOT Grounded to the airframe. My wife and I are building an RV-10. We are planning an all electric IFR panel and a two PC625 battery, two alternator electrical system. Would you please make your comments specific to this setup? Am I correct in assuming that there is an ideal setup for a two rear battery, two alternator system, which is the Z-14 attached, and then there is a more practical setup, which has the batteries grounded at the rear. Is this correct? Would you please comment on the relative merits of these two different approaches, and especially comment on any downside of both approaches? If you ground both rear batteries as suggested down the back to the airframe, do you then set up your avionics ground bus at the panel simply by connecting it to the firewall Ground? Are there any issues or concerns with doing this? >From a purely electrical perspective, would it be preferable in our situation (ignoring weight and balance questions for the moment) to have either battery situated up the front somewhere? If yes, which would be preferable to put up the front, and why? I also have a couple of other questions on the attached Figure Z-14. Does the single ground lead from both batteries to the front provide a single source of total failure? And lastly, why have you specified the copper/brass strap on the power side of the main battery in the attached Z-14? Thank you once again for all your very generous input. John Cleary -----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 Sent: Thursday, 29 March 2007 12:28 AM Subject: Re: AeroElectric-List: Rear Mounted Batteries - more questions > > >Bob, > >Now you are confusing me.. > >Yes, I did look at the link you provided. > >Using the generic aircraft - single battery schematic for schematic on >metal tube frame. >Battery (Odyssey 680) and contactor will be located under baggage >compartment floor behind seat backs. > >I thought we were supposed to run a ground wire from the battery to the >brass ground bus plate (with all the quick connect tabs on it) which was >to be mounted on the firewall. Isn't using the airframe for ground now >generating two paths for ground - hence possible problems? Local grounds in all metal airplanes can practically depart from "ideal" for the following: Batteries, strobe supplies, landing/taxi lights, pitot heaters, position lights, hydraulic pumps for landing gear (because they're intermittent) but not for air-conditioning compressors (because they're continuous). >I'm about ready to wire in my rear mounted battery (before covering). I >will use flexible wire for the battery terminal connections (and to the >local ground if that's what I am supposed to do). No problem attaching >ground leads to the frame if a good idea. It would eliminate an extra wire >to top and bottom strobes and tail position light... but I was already >resolved to run + and gnd to each (using a small local-next to battery >version of the brass ground bus with quick disconnects like in the front) > >I'd appreciate your input. It's never 'bad' to run all electro-whizzies to a single point ground but if one wishes to take advantage of the ground-friendly, all-metal airplane with the cited compromises, there's no risk of having an unhappy noise moment. It's most important to pay attention to grounding potential victims such as avionics and instrumentation. These should return to the firewall ground point per Z-15. I'll add some notes to Z-15 next revision to clarify this point. Bob . . . ________________________________________________________________________________
From: "David M." <ainut(at)hiwaay.net>
Subject: OT: looking for ride
Date: Mar 31, 2007
Will share fuel and flying for our leg, at least. My wife and I would like to get from the Houston, Texas area to Huntsville, Alabama (preferably to 3M5, Moontown Airport) around April 17 or so. We have a car here in Houston so we can drive a couple of hours to an airport, then we'll ride our bikes back to Houston. Thanks, David M. ________________________________________________________________________________
Date: Apr 01, 2007
Subject: Re: OT: looking for ride
From: Dj Merrill <deej(at)deej.net>
John Burnaby wrote: > I have often thought about this very subject, aircraft ride sharing, and > thought that, surely, there must be an aviation "Ride Board" > somewhere??? Did a cursory Google and got nothing except one site that > is trying to middleman($$) flyers and riders, but the site was down. > John > Hi John, Try this site: <http://www.pilotsharetheride.com/> -Dj -- Dj Merrill Sportsman 2+2 Builder #7118 http://econ.duke.edu/~deej/sportsman/ "TSA: Totally Screwing Aviation" ________________________________________________________________________________
From: "Eric Parlow" <ericparlow(at)hotmail.com>
Subject: PMA-8000-SR Audio Panel Connections
Date: Apr 01, 2007
Looking for suggestions on connecting the PMA-8000-SR It has an input for DME, what goes in here? The internal Sirius radio can be routed internally or externally to Crew Audio and Pass Audio. If external they recommend a STDP switch to be able to connect another audio input. Does an audio jack exist that will do the switching when the plug is inserted? For the "Un-switched Audio 1,2,3,4" will an input such as an iPod be able to drive 4 head sets? In other words, is the input amplified in any way? Understanding that the volume will be controlled by the input signal. And, how could a handheld radio (ICOM A23) be wired in as a Com 3 or the like? Can it go in as an "Aux Receiver"? We have the following components to connect: GNS 430W SL-30 GTX 327 ICOM A23 (handheld) BMA EFIS/One & Autopilot(disconnect & stall) Garmin 396 with XM weather & radio DVD player/Laptop audio IPOD for rear pass. Cell Phone ________________________________________________________________________________
From: "Todd Archer" <archerw(at)ubtanet.com>
Subject: OT: looking for ride
Date: Apr 01, 2007
http://www.sun-n-fun.org/content/flyin/posts.asp?type=0§ion=flyin&body=s hareaflight I have often thought about this very subject, aircraft ride sharing, and thought that, surely, there must be an aviation "Ride Board" somewhere??? Did a cursory Google and got nothing except one site that is trying to middleman($$) flyers and riders, but the site was down. John ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Apr 01, 2007
Subject: Re: PMA-8000-SR Audio Panel Connections
In a message dated 4/1/2007 12:46:22 P.M. Central Daylight Time, ericparlow(at)hotmail.com writes: It has an input for DME, what goes in here? DME Audio so you can properly identify the station being received Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
Date: Apr 02, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: Avionics Mounting
I'll work on that today. Sam Marlow RV_10 wrote: > > Hi Bob, > > > > Do you have any photos of your install that you could send to me? > > > > Thank you, > > John Cleary > > > > ------------------------------------------------------------------------ > > *From:* owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of > *BobsV35B(at)aol.com > *Sent:* Saturday, 31 March 2007 1:56 AM > *To:* aeroelectric-list(at)matronics.com > *Subject:* Re: AeroElectric-List: Avionics Mounting > > > > In a message dated 3/30/2007 8:39:20 A.M. Central Daylight Time, > sam(at)fr8dog.net writes: > > I have the same radio stack, just used .250 AL bar, and taped the > holes for #8 screws. I also added 1 support in the rear of the stack. > > Good Morning > > > > Happy Skies, > > Old Bob > AKA > Bob Siegfried > Ancient Aviator > Stearman N3977A > Brookeridge Air Park LL22 > Downers Grove, IL 60516 > 630 985-8503 > > > ------------------------------------------------------------------------ > > See what's free at AOL.com > <http://www.aol.com?ncid=AOLAOF00020000000503>. > > * * > * * > ** > ** > ** > ** > ** > ** > * * > * > > > * ________________________________________________________________________________
Date: Apr 02, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: Avionics Mounting
Yes that's very true, but I can just build another AL bar rack before UPS can deliver a made to order unit. It's simple and cheap, from your Lowe's aviation department! BobsV35B(at)aol.com wrote: > Good Morning Sam, > > The advantage (if there is any) to the RadioRax is that they are > infinitely adjustable. If you want to rearrange or add anything to the > stack, there is no need to drill new holes. With any of the more > conventional strips, the new holes often conflict with old holes which > will then require that a new support bar be fabricated and installed. > > If you are absolutely certain you will never want to change anything, > there is little advantage to the RadioRax system. > > Happy Skies, > > Old Bob > AKA > Bob Siegfried > Ancient Aviator > Stearman N3977A > Brookeridge Air Park LL22 > Downers Grove, IL 60516 > 630 985-8 > > In a message dated 3/30/2007 8:39:20 A.M. Central Daylight Time, > sam(at)fr8dog.net writes: > > I have the same radio stack, just used .250 AL bar, and taped the > holes for #8 screws. I also added 1 support in the rear of the stack. > > 503 > > > ------------------------------------------------------------------------ > See what's free at AOL.com > <http://www.aol.com?ncid=AOLAOF00020000000503>. > * > > > * ________________________________________________________________________________
Date: Apr 02, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: DIY engine monitor
Joe & Jan Connell wrote: > Guys, > > Some of the postings on this topic have discussed the work > done by GAMI in regards to lean of peak. I might be incorrect > but the GAMI folks are usually working with fuel injection, not > carburetors. Please correct me if I'm wrong... > > Joe Connell I think the thrust of your question is that GAMI is an authority on injectors, but are not in a position to authoritatively discuss carburated engines. It's a valid point. If someone claims to be an authority, the need to show from where that claim derives. I've seen some of their work as it relates to instrumenting an engine cylinder to collect data. Most of it as related by John Deakins in his Avweb column. I rank it highly and trust it, because the explanations provided break the cylinder combustion process down to basic principles of physics and remove a lot of the black majic and handwaving. The sort that you'll get a lot of around a racetrack or other such place where people think they know what is happening, but haven't actually instrumented a cylinder to find out. Once the cylinder is instrumented, it is a simple matter to swap the engine to be carburated. If I was going to attempt to compete in this arena, I most certainly would do that. It would be plain silly not to. No, I haven't seen any data they've collected from a carburated engine, and they mostly concentrate on promoting *balanced* injectors; however, the statements they've made about carburated engines corresponds to every statement I've heard from any other authority (including my high school physics teacher.) -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Date: Apr 02, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Rear Mounted Batteries - more questions
>Hello 'Lectric Bob, > >Thank you for all the fantastic effort you put into this group. It is >extremely helpful to those of us with zero earlier experience in this area. > >I have read the Connection a couple of times and I have been pondering the >whole issue of batteries and locations and fat wires etc. > >Attached is a schematic of a Z-14, architecture for rear batteries. This is >not your current Z-14, and I don't know now where I got this from, but it >very specifically states that the Aft Ground Buss is NOT Grounded to the >airframe. > >My wife and I are building an RV-10. We are planning an all electric IFR >panel and a two PC625 battery, two alternator electrical system. Would you >please make your comments specific to this setup? > >Am I correct in assuming that there is an ideal setup for a two rear >battery, two alternator system, which is the Z-14 attached, and then there >is a more practical setup, which has the batteries grounded at the rear. Is >this correct? Essentially yes. If one were building a composite aircraft, then a fat feeder for battery(-) leads to the firewall is REQUIRED. But in a metal airplane, one has the option of crafting a pristine system depicted in the sketch -or- taking advantage of the airframe as a power return for devices that are NOT potential victims to ground loop conducted noises. >Would you please comment on the relative merits of these two different >approaches, and especially comment on any downside of both approaches? > >If you ground both rear batteries as suggested down the back to the >airframe, do you then set up your avionics ground bus at the panel simply by >connecting it to the firewall Ground? Are there any issues or concerns with >doing this? Nope. Your engine straps to the bolt at this ground also. > >From a purely electrical perspective, would it be preferable in our >situation (ignoring weight and balance questions for the moment) to have >either battery situated up the front somewhere? If yes, which would be >preferable to put up the front, and why? Batteries are the ultimate mitigator of CG problems. From the electrical perspective, we'd like to have all the starters, alternators and batteries be grouped together in something under 2 cubic feet of common volume. As a practical matter, batteries are placed where they need to go to accommodate other airframe design goals. As a major component of weight and volume, batteries are among the very few items where performance is not seriously compromised by moving them around. >I also have a couple of other questions on the attached Figure Z-14. Does >the single ground lead from both batteries to the front provide a single >source of total failure? And lastly, why have you specified the copper/brass >strap on the power side of the main battery in the attached Z-14? The crossfeed contactor, starter contactor and current limiter block can be mounted within inches of each other and "wired" with flat strap like the pictures found in this directory . . . http://www.aeroelectric.com/Pictures/Wiring_Technique/ The short straps are much easier to fabricate and install than very short hunks of fat wire with terminals. Bob . . . ________________________________________________________________________________
Date: Apr 02, 2007
From: "Robert L. Nuckolls, III" <nuckollsr(at)cox.net>
Subject: Re: the battery dragon . . .
> > > >>Comments/Questions: I am building a Jabiru J430 and plan to include your >>crowbar overvoltage system and low voltage detector. I am planning on a >>dual battery where the second battery supports the main bus but not the >>starter motor. The plan is to put a power diode between the bus and the >>main battery. This means that that both batteries will charge from the >>regulator but the second battery will not contribute to starting and >>provide a sink to the bus to ensure voltage is maintained to the bus even >>during starting. The idea is for the second battery to keep the electics >>going in the event of main battery failure. Do you think this make sense? > > Unless you're planning not to maintain your battery, then > 'battery failure' is exceedingly remote. The battery can > be the most reliable source of power in the airplane. I missed an important part of this guy's questions 'bout brownout protection. I'm crafting an article to cover both the brownout free bus (BOF-Bus) and battery failures. It's about done and will be published to the website this evening. Bob . . . ________________________________________________________________________________
Date: Apr 02, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: Avionics Mounting
BobsV35B(at)aol.com wrote: > Good Morning Sam, > > But you can't make and install a new bar in the time it takes me to > loosen a screw and slide the radio sleeve up or down an eighth of an > inch. There is no need to ever touch the mounting bars once they are > installed. The placement of all fastenings is infinitely adjustable > forever! > > Why do you feel it would be necessary to wait for a made to order unit? > Why wouldn't you just cut slots instead of tapped holes in the Lowe's Aviation angle? It's not infinitely adjustable, but there's plenty for what's necessary. -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
Date: Apr 02, 2007
From: Sam Marlow <sam(at)fr8dog.net>
Subject: Re: Avionics Mounting
I'm a little close on room, my panel is full. Ernest Christley wrote: > > > BobsV35B(at)aol.com wrote: > >> Good Morning Sam, >> >> But you can't make and install a new bar in the time it takes me to >> loosen a screw and slide the radio sleeve up or down an eighth of an >> inch. There is no need to ever touch the mounting bars once they are >> installed. The placement of all fastenings is infinitely adjustable >> forever! >> >> Why do you feel it would be necessary to wait for a made to order unit? >> > > > Why wouldn't you just cut slots instead of tapped holes in the Lowe's > Aviation angle? It's not infinitely adjustable, but there's plenty > for what's necessary. > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Apr 02, 2007
Subject: Avionics Mounting
Good Morning Ernest, Given adequate machining capability, you could produce almost anything you wanted to produce. I was merely commenting that I like the way RadioRax work and I wish I would have thought of it! You can manufacture your own engine if you want to. I tend to buy my engines already built and I also buy other products that are beyond my capability of producing economically. Whatever works! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 4/2/2007 9:08:03 A.M. Central Daylight Time, echristley(at)nc.rr.com writes: Why wouldn't you just cut slots instead of tapped holes in the Lowe's Aviation angle? It's not infinitely adjustable, but there's plenty for what's necessary. ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
Date: Apr 02, 2007
From: Ernest Christley <echristley(at)nc.rr.com>
Subject: Re: Avionics Mounting
BobsV35B(at)aol.com wrote: > Good Morning Ernest, > > Given adequate machining capability, you could produce almost anything > you wanted to produce. > > I was merely commenting that I like the way RadioRax work and I wish I > would have thought of it! > > You can manufacture your own engine if you want to. I tend to buy my > engines already built and I also buy other products that are beyond my > capability of producing economically. > > Whatever works! > For a cheap slotted hole, you can buy a rotary saw. Looks like a drill bit with a serated edge. To cut aluminum, wax up both sides real good with a candle. Scrape a little on the bit, too. For a really straight slot, clamp a fence to your drill press table (or a friends table if you don't have one, and he ain't lookin'). Drop the bit through at the start of the slot and push the piece through to the end of it. The fence would be a chunk of 2x4, another piece of angle, or any other straight object of suitable length. It's easier if you can find a suitable helper, as it's best to have two hands on the workpiece if possible. If it isn't possible, clamp a fence on both sides of the angle so it can't spin on you. Maybe I should take some pictures of the process and send it in to the new guy doing home machine shop articles in Kitplanes. -- ,|"|"|, Ernest Christley | ----===<{{(oQo)}}>===---- Dyke Delta Builder | o| d |o http://ernest.isa-geek.org | ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Apr 02, 2007
Subject: Avionics Mounting
Good Afternoon Ernest, In my opinion, the article produced would still have no where near the capability of the RadioRax. I think it is wonderful that you and others have the freedom to make and use whatever you want on your airplane. I also have a choice. Given the choice between anything I have yet manufactured and the readily available manufactured items, I will take the readily available RadioRax! Maybe I remove and add components to my radio stack a lot more often than do most others, but drilling new holes and slots in an existing piece of aluminum is not as pleasurable to me as is just loosening a binding screw and moving the radio sleeves wherever I want them to be. A little extra effort during the original installation saves me hours of work every time thereafter that a radio needs to be moved or replaced. Happy Skies, Do Not Archive Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 4/2/2007 1:20:37 P.M. Central Daylight Time, echristley(at)nc.rr.com writes: For a cheap slotted hole, you can buy a rotary saw. Looks like a drill bit with a serated edge. To cut aluminum, wax up both sides real good with a candle. Scrape a little on the bit, too. ************************************** See what's free at http://www.aol.com. ________________________________________________________________________________
Date: Apr 02, 2007
From: Dennis Haverlah <clouduster(at)austin.rr.com>
Subject: Re: Fwd: Re: re: Capacitors for Whelen strobe power
supply I was asked how the repair of the Whelen strobe power supply has gone. The strobe is Model A413A,HDA-DF-14 The power supply is working but it took some luck. I'm pretty much an amateur when it comes to electronics. I used the P11920-ND capacitors from DigiKey. These were recommended by James Foerster - Thanks James! The capacitors are the correct electrical size but are much smaller physically than the original caps. After installing the new capacitors, the strobe flashed erratically and the large transistor mounted on the aluminum heat sink got quite hot. I believe the transistor controls the high voltage transformer primary windings but I'm not sure. I would discharge the capacitors with an insulated screwdriver before inspecting the unit. Only one cap. had a charge. A test with a voltmeter showed the second cap. was not getting any voltage. The high voltage windings on the transformer charging the caps. is a center-tap winding. The center tap is connected to the + on one cap. and the - on the other. I disconnected the dead winding output wire (read cut it off 1 inch from the circuit board with a dike) and hooked it to my Harbor Freight $4.00 volt meter. Powered up, it had several hundred volts A/C so I assumed the transformer was OK! That was good news because if the transformer was bad I'd give up. I looked at the circuit board and the next component on the board where the transformer wire connected was a diode - marked EDA - BR8M5. I tested it with the HF meter and it was open!! I could not find any data on the BR8M5 diode but I had a pack of RadioShack IN 5404 diodes rated at 400 V. Soldered one in and the power supply came alive - And the transistor is now running Cool! Hope this helps someone else rejuvenate a strobe power supply. I hate to see them thrown away! PS: If you want to get your Grand kids attention - discharge one of the capacitors while they are watching! Dennis Haverlah wrote: > > > I want to thank everyone for the information on strobe capacitors. I > have ordered some from Digi-key and will let the list know how they work. > > Dennis H. > > Robert L. Nuckolls, III wrote: > >> >> >> Here's a note I received on one fellows success with >> replacing flash-rated capacitors with plain-vanilla >> electrolytics. >> >> His confirmation of my past experiences suggests that >> the experiment is worth repeating. >> >> >> >>> Hey, Bob, I'm just a lurker in the archives, but I have replaced the >>> electrolytics in two Whelen strobe supplies.... Worked fine then and >>> is working fine now. Some spray-on conformal coating helps cut down >>> on the high-voltage corrosion in the units. >> >> >> >> Bob . . . >> >> ---------------------------------------- >> ( IF one aspires to be "world class", ) >> ( what ever you do must be exercised ) >> ( EVERY day . . . ) >> ( R. L. Nuckolls III ) >> ----------------------------------------


March 13, 2007 - April 02, 2007

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