AeroElectric-Archive.digest.vol-am

December 01, 2001 - December 28, 2001



      If it is critical, I think we find the current drain of each of the above.
      
      James
      RV6 ... Panel
      Patty
      RV6 ...Wingtips
      
      
      -----Original Message-----
From: owner-aeroelectric-list-server(at)matronics.com
[mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Ed Holyoke
Subject: Alternator size 40 or 60 amp?
I'm getting ready to engine my RV-6 and I'm trying to figure out how big an alternator I'll need. I'll be running all electric with : RC Allen horizon and DG, Navaid ap, EI ubg16, Matronics fuelscan, Van's gauges for about everything else, KMD 150 gps, KX 165 and indicator, and a transponder, 2 100watt landing lights (wigwag), whelen comet flash strobes, pitot heat, dual lightspeed ignitions and electric trim. The documentation that I've got doesn't tell me what the power consumption is on most of this stuff. I've tried to measure the amps on a gyro with my multimeter and got nowhere. Any ideas? Ed Holyoke RV-6 QB http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
Date: Dec 01, 2001
From: Matt Dralle <dralle(at)matronics.com>
Subject: Comments...
Listers, Below are some of the comments I've received just this week alone from members along with their Contributions to support the Lists! What can I say? Wow. I really appreciate the kind words and extremely positive feedback and I would encourage you to read over a few of comments below. I think they really say a mouthful... The last couple of days have seen a huge increase in support!! Thank you to all that have Contributed and to those that have rallied support for the Lists! Since the response has been so wonderful recently, I plan to delay the posting of the 2001 List of Contributors a few days to assure that everyone will be included! Won't you make your Contribution today to support the Lists? ------------------------------------------ The SSL Secure Web Site: http://www.matronics.com/contribution The US Mail Address: Matronics Email Lists c/o Matt Dralle PO Box 347 Livermore, CA 94550-7227 ------------------------------------------ Thank you to everyone for the kind words and support! Matt Dralle Email List Admin. ======== Some Great Comments on What The Lists Mean to its Members ========== ...great source of information, education, relaxation, frustration, and socialization. - John H. Can't imagine what it would be like building with out the Lists... - Steven E. Look forward to the list every day. - Parker T. I really enjoy reading the banter... - Wesley H. ...enjoy the patter on construction tips and possible problem areas. - Richard N. Couldn't have built my RV-4 without the List and archives!! - Warren M. I have found the list to be a great help, especially for a first time builder. - Peter D. I thoroughly enjoy the List. - Larry B. The List is a great resource. - Dennis K. The list is great entertainment. - Gary Z. Can't say enough about the good information that I have received from reading the List. - Robert C. ...it's the best! - Steve F. I'm addicted to the List! - Rodney B. The list has been a wonderful resource of knowledge. - Doug B. As a first time builder, the lists have been my most important source of information. - James V. It [read the List] is the first thing I do every day is see what's new. - Billie F. The information available through the List has made my flying safer... - Dave R. I get much more information about my plane from this List than from all of my aviation magazines combined. - Roger H. I love the list!!!! - Ken L. Much better value than a magazine subscription. - Ted M. ...found it very useful. - Allan J. ...this list has been a great service to me. - Peter F. I cannot express just how USEFUL the Lists are. - Geoff T. ...a tremendous help to my RV-8 project and a way to meet some of the best people going. - Steve G. The List is invaluable, and the best I've ever seen. - Ed C. Like another family for many of us. - John H. The lists have saved a bunch of calls to Van's for guidance. - James V. I think I'm addicted... - Terry C. Love it! - David W. The information really helps... - Jim P. ...I find [it] very informative. - Real D. ...List keeps me motivated... - Cliff M. The exchange of information is really helpful... - M.N. Lots of great info on the List. - Larry D. ________________________________________________________________________________
Date: Dec 01, 2001
From: "Mike & Lee Anne (mwiebe(at)sympatico.ca)" <mwiebe(at)sympatico.ca>
Subject: Re: Flap control
> Rob....sorry I can't help by directly answering your questions. However, that's why I said go see a Diamond Katana. They've done this and if you find someone nice, should be able to help with the details. Mike > > > I agree with your points here... > but - What kind of switch? How to include indicator? Circuit design? > These are the questions I have... as I already have a preference for a > system similar to your thoughts. > Robert > > Mike & Lee Anne (mwiebe(at)sympatico.ca) wrote: > > > > > > >Robert, here's something you might consider. It's a simplification (and in my opinion, > >an > >improvement) on the Cessna system. A little more difficult to construct, but elegantly > >simple to use. I first saw this in a Diamond Katana, so find a local dealer and check > >it out. > > ________________________________________________________________________________
From: "Gary Casey" <glcasey(at)gte.net>
Subject: air/fuel indicators
Date: Dec 01, 2001
>>The manual says the meter cannot be used with leaded fuels.<< The meter will work just fine - the sensor, though, will have a finite life running on leaded fuel. However, I have heard reports that they will last at least 200 hours and maybe more if protected from the direct exhaust stream. At $35 each, maybe that's acceptable. Also, note the previous response (excerpt below) that is correct: > HOWEVER, apparently, leaded gasoline DOES contaminate the sensor to > the point that it loses its ability to respond quickly enough to exhaust > changes > (milliseconds) to control an automobile Fuel management system (computer) > and prevent > those bad exhaust emissions. So for its intended purpose in an automobile > (emissions control), > it is essentially correct that leaded gas will degrade it. BUT, if you > simply want to use an O2 sensor in your exhaust to provide and indication of > relative fuel mixture, it will work fine using 100 LL for hundreds of hours. Also, another question was posted: >Would be interested in hearing of > > anyone's experience with this or any similar o2 > > sensor/indicator system. I don't know what JC Whitney sells, but I bought an Autometer unit from the local PAW speed shop for about the same price and it works great. The multi-LED display is a little more dramatic than it needs to be as one or two LED's would tell about the same story. It is not dimmable and not readable in direct sunlight. I have worked a little with the folks at Autometer since they are our customer for pressure sensors. Good company with high quality parts. Gary Casey ________________________________________________________________________________
From: "Gary Casey" <glcasey(at)gte.net>
Subject: flap position control
Date: Dec 01, 2001
>>I first saw this in a Diamond Katana, so find a local dealer and check >it out. >Flap switch is not a momentary contact switch like the days of old, but is simply a 3 >position >switch. Top position is cruise (flaps up), middle position is takeoff flaps, bottom >position is >landing flaps.<< I would like to do the same thing - I was thinking about a 3-position rotary switch with an indicator light(s). Turn to the position you want, a light comes on and then goes out when the flaps stop at that position. Anybody got a clever circuit design that would do that without too much complexity? Gary Casey Lancair ES project ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)qcbc.org>
Subject: Re: Alternator size 40 or 60 amp?
Date: Dec 01, 2001
I believe the FAA requirement is 80% of total load for power but if you look at your devices, seldom will all be one at one time, especially the landing lights if you are flying IFR. If the larger alternator doesn't have too big a weight penalty then it might be ok, but energy management is the key. Even with a 100 amp alternator you will not have enough charging capacity for extended taxi with every thing on. Alternators do not put out their rated capacity until you running the engine at cruise rpm so one must use only what is needed. Why do you think airliners turn off the cabin lights when landing? Pilot's can't see that light behind them. Cy Galley, TC - Chair, Emergency Aircraft Repair, Oshkosh Editor, EAA Safety Programs cgalley(at)qcbc.org or experimenter(at)eaa.org http://www.eaa.org for latest flying rules Always looking for articles for the Experimenter ----- Original Message ----- From: "James E. Clark" <jclark(at)conterra.com> Subject: RE: AeroElectric-List: Alternator size 40 or 60 amp? Ed, My partner and I are building an RV with a similr setup (without the electric RC Allens) Navaid AP EI UBG Van's Gauges KMD 150 GPS UPS SL40 (no indicator yet) KT76A Transponder 2 100 watt lights Whelen Strobes No Pitot heat (yet) Jeff Rose Electronic Ignition Manual Trim Turn Coordinator Electronic Compass Sony "Entertainment Subsystem" ;-) . We started out **thinking** that a 35 AMP alternator would work ...I don't think so! There is a scenario where the above adds up to over 50 AMPS! The more likely scenario can *probably* be covered with the 40. But even though my partner says she will never fly it at night, IFR, in a storm, over the mountains and that she KNOWS I won't either, we will most likely go with the 60. If it is critical, I think we find the current drain of each of the above. James RV6 ... Panel Patty RV6 ...Wingtips -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Ed Holyoke Subject: AeroElectric-List: Alternator size 40 or 60 amp? I'm getting ready to engine my RV-6 and I'm trying to figure out how big an alternator I'll need. I'll be running all electric with : RC Allen horizon and DG, Navaid ap, EI ubg16, Matronics fuelscan, Van's gauges for about everything else, KMD 150 gps, KX 165 and indicator, and a transponder, 2 100watt landing lights (wigwag), whelen comet flash strobes, pitot heat, dual lightspeed ignitions and electric trim. The documentation that I've got doesn't tell me what the power consumption is on most of this stuff. I've tried to measure the amps on a gyro with my multimeter and got nowhere. Any ideas? Ed Holyoke RV-6 QB http://www.matronics.com/browselist/aeroelectric-list http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
From: "Paul Besing" <azpilot(at)extremezone.com>
Subject: Re: flap position for RV
Date: Dec 01, 2001
Having flown my RV for about 60 hours now, and have most of my time in cessnas, I do not feel that I need stops in my flap deployment. Actually, it would hinder things a little. RV's in crosswinds can be tricky and sometimes you need to slow down a little bit, but don't want much flaps. I frequently use many different flap settings. It became a seat of the pants type of flying real quick. I have an indicator on the panel, but most of the time just look at the airspeed indicator and sometimes the flap itself and see where it is when I deploy it. You are creating too much work for yourself, in my opinion. RV's are so much more precise flying machines than Cessna aircraft and it is difficult to compare the two when considering flap deployment and other characteristics. Just put as much flaps in as you need to get your proper speeds relative to your flying conidtions. Paul Besing RV-6A N197AB Arizona http://www.lacodeworks.com/besing Flying Kitlog Pro Builder's Log Software http://www.kitlog.com ________________________________________________________________________________
Date: Dec 01, 2001
From: Finn Lassen <finnlassen(at)netzero.net>
Subject: EDO-AIRE RT-553 repair/parts
I'm trying to repair an EDO-AIRE RT-553 NAV/COM radio for a friend. Does anyone know where to get parts for these? I think I've traced it to a chip in the synthesizer: F 95H04DC (I assume an IC by Fairchild). Haven't been able to find it in any databook. Anybody know what it is and where I can get it? Finn ---------------------------------------------------- Sign Up for NetZero Platinum Today Only $9.95 per month! http://my.netzero.net/s/signup?r=platinum&refcd=PT97 ________________________________________________________________________________
Date: Dec 02, 2001
From: "Mike & Lee Anne (mwiebe(at)sympatico.ca)" <mwiebe(at)sympatico.ca>
Subject: Garmin connector
Hi all....just got my new 295 (sweet!) and am trying to figure out a mounting configuration. I need to use the external antenna, but would like to find a "shallow" coupler for it. That it, the BNC (I think?) connector sticks too far out to the rear of the unit for a reasonable surface "flush" mount. Simple BNC to R*-58 type 90 degree connectors I have locally, but the cable to the antenna is small diameter - not sure what it is. Any ideas for the connector of choice - ideally shallow mount and/or 90 degree bend. Also, any tricks to fastening this thin cable, before I cut the end off the existing connector? Thx in advance. Mike ________________________________________________________________________________
Date: Dec 02, 2001
From: Wes Knettle <wsknettl(at)centurytel.net>
Aviaiton Inspector , Beech-List Digest List , Denis M Arbeau , Engines-List Digest List , "North American Trainer Assc."
Subject: Aeroshell Oil Recall
For those of you using Aeroshell products the code numbers of quart bottles and cases can be found on this site. http://www.cessna.org/aeroshell_recall.html Wes K ________________________________________________________________________________
Date: Dec 02, 2001
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: Garmin connector
"Mike & Lee Anne (mwiebe(at)sympatico.ca)" wrote: > > > Hi all....just got my new 295 (sweet!) and am trying to figure out a > mounting configuration. I need to use the external antenna, but would > like to find a "shallow" coupler for it. That it, the BNC (I think?) > connector sticks too far out to the rear of the unit for a reasonable > surface "flush" mount. Simple BNC to R*-58 type 90 degree connectors I > have locally, but the cable to the antenna is small diameter - not sure > what it is. Any ideas for the connector of choice - ideally shallow > mount and/or 90 degree bend. Also, any tricks to fastening this thin > cable, before I cut the end off the existing connector? > Thx in advance. > Mike > Have you seen the BNC 90 degree adaptors? BNC male > 90 degree turn > BNC female Any well stocked electronic supply house will have them & they won't stick out the back any further than a 90 degree connector. Nothing to cut, nothing to make, just plug & go. Charlie ________________________________________________________________________________
Date: Dec 02, 2001
From: tom sargent <sarg314(at)earthlink.net>
Subject: alternator field switch
Bob: Sorry if I'm the 10,000th guy to ask this, but on page 11-20 of your book you advise using a 2-3 switch to control battery master contactor AND alt. field current simultaneously, but you don't say why. It always made sense to me to be able to disconnect the alt. field coil separately in order to avoid wasting power into it when the alternator fails and you're running off the battery only. The Z-1 schematic shows the same switch. Are you depending on the B&C voltage regulator to not power the field coil when the alt. dies? -- Tom Sargent. ________________________________________________________________________________
Date: Dec 02, 2001
From: Charles Brame <charleyb(at)earthlink.net>
Subject: Alternator size 40 or 60 amp?
Just how much weight difference is there between the 40 Amp and the 60 Amp alternator? The answer does not appear to be on the website. Charlie Brame RV-6A QB N11CB (Res.) San Antonio ________________________________________________________________________________
From: BAKEROCB(at)aol.com
Date: Dec 02, 2001
Subject: Katana flap mechanism
12/1/01 Hello Robert Miller, I agree with Mike's recommendation below. Let me give you a bit of a head start from the Katana illustrated parts catalog. The flap control and indicator is in one box on the instrument panel. Part number is KLSTR-DV20A Flap Control The actuator is part number 22-2750-02-00 Actuator motor sub-assy, The position detection system is part number 20-2750-15-00 Position switch assy. This position detection system appears to contain two micro switches. This is not a simple system. Parts appear to be connected with a 3 pin and a 6 pin connector. If you'd like copies of the pertinent pages email me an address and I'll mail them to you. It would be interesting to learn how Diamond treats you. I considered using some of their parts in my airplane. Sometimes they treated me like a fellow airplane builder "we are all in this together". Other times they treated me as competitor to be stonewalled and as a tremedous potential liability if I crashed my plane and sued them because of the parts that they had sold me. Please keep us posted. 'OC' Baker, Builder of KIS TR-1 #116 4/14/97 - ?/?/? In a message dated 12/01/2001 2:52:38 AM Eastern Standard Time, Robert Miller writes: From: Robert Miller <rmiller3(at)earthlink.net> Subject: Re: AeroElectric-List: Re: flap position for RV I agree with your points here... but - What kind of switch? How to include indicator? Circuit design? These are the questions I have... as I already have a preference for a system similar to your thoughts. Robert Mike & Lee Anne (mwiebe(at)sympatico.ca) wrote: (mwiebe(at)sympatico.ca)" > > >Robert, here's something you might consider. It's a simplification (and in my opinion, >an >improvement) on the Cessna system. A little more difficult to construct, but elegantly >simple to use. I first saw this in a Diamond Katana, so find a local dealer and check >it out. >Flap switch is not a momentary contact switch like the days of old, but is simply a 3 >position >switch. Top position is cruise (flaps up), middle position is takeoff flaps, bottom >position is >landing flaps. No opportunity for screw ups in deployment. You do have to give up the >feeling that you "need" that infinite number of middle settings - sometimes a hard thing >for us >homebuilders to do, but in my opinion the right thing if you are really looking for >simplicity. After >a lot of discussion with the Diamond factory people about this, I am convinced. My next >airplane >will have this, but I haven't figured out the behind the scenes wiring to make it >happen. I'm >sure some listers here will know how, but it might be simpler to check with the Diamond >Aircraft folks. > >Mike > >> ________________________________________________________________________________
From: "David Swartzendruber" <dswartzendruber(at)earthlink.net>
Subject: Re: Alternator size 40 or 60 amp?
Date: Dec 02, 2001
I believe it's 8.3 lbs vs. 6.1 lbs. David Swartzendruber Wichita > Just how much weight difference is there between the 40 Amp and the 60 > Amp alternator? The answer does not appear to be on the website. > > Charlie Brame > RV-6A QB N11CB (Res.) > San Antonio ________________________________________________________________________________
Date: Dec 02, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: RE: Exhaust Gas Indicator
> > Do these O2 sensors work with leaded fuel? I've heard they get >contaminated and stop working but that could be old wife's tale. I've seen them produce satisfactory performance after hundreds of hours on 100LL. They get "slow" . . . too slow to work with electronic controlled fuel injection which needs to be tens-of-milliseconds fast . . . as a manual leaning aid, they seem to perform quite well. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 02, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: RE: Alternator size 40 or 60 amp - Load Analysis
> >Ed, > >My partner and I are building an RV with a similr setup (without the >electric RC Allens) >Navaid AP >EI UBG >Van's Gauges >KMD 150 GPS >UPS SL40 (no indicator yet) >KT76A Transponder >2 100 watt lights >Whelen Strobes >No Pitot heat (yet) >Jeff Rose Electronic Ignition >Manual Trim >Turn Coordinator >Electronic Compass >Sony "Entertainment Subsystem" ;-) . > >We started out **thinking** that a 35 AMP alternator would work ...I don't >think so! >There is a scenario where the above adds up to over 50 AMPS! > >The more likely scenario can *probably* be covered with the 40. But even >though my partner says she will never fly it at night, IFR, in a storm, over >the mountains and that she KNOWS I won't either, we will most likely go with >the 60. > >If it is critical, I think we find the current drain of each of the above. > >James >RV6 ... Panel >Patty >RV6 ...Wingtips And this note . . . > >I'm getting ready to engine my RV-6 and I'm trying to figure out how big >an alternator I'll need. I'll be running all electric with : >RC Allen horizon and DG, Navaid ap, EI ubg16, Matronics fuelscan, >Van's gauges for about everything else, KMD 150 gps, KX 165 and >indicator, and a transponder, 2 100watt landing lights (wigwag), whelen >comet flash strobes, pitot heat, dual lightspeed ignitions and electric >trim. >The documentation that I've got doesn't tell me what the power >consumption is on most of this stuff. I've tried to measure the amps on >a gyro with my multimeter and got nowhere. >Any ideas? I've yet to see a single engine airplane homebuilt that won't run well on a 40A machine. The largest full-up, night-ifr running load I've calculated so far is 27A which leaves 13A for battery support. The next new addition to the connection will be a chapter including a technique for load analysis . . . it is insufficient to ADD UP all the breakers, these don't represent RUNNING LOADS. It's equally insufficient to add up everything and assume that the alternator has to carry all those loads for any significant amount of time. Break down operations into phases of significant endurance and add up only those things which have continuous running loads during that phase. For example, pitot heat needs to be used in clouds, but all exterior lighting will be OFF. Landing gear, flap motors, landing lights are short duration, transient loads (unless you have wig wags where the average draw for the pair of lights is equal to one light) . . . make a chart of all goodies you plan to install and then columns of operation phases like taxi, takoff/departure, day cruise, night cruise, ifr cruise, approach to landing, and alternator-out ops (the current suppied by battery only to the essential bus). If anyone can come up with more than 27A in any of these phases, I'd like to see your analysis. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 02, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Alternator size 40 or 60 amp?
> >I believe the FAA requirement is 80% of total load for power but if you look >at your devices, seldom will all be one at one time, especially the landing >lights if you are flying IFR. Please try to eliminate the phrase "FAA requirement" from the lexicon of modern, owner built airplane-speak. There are NO requirements applicable to what we're doing here. Let's pick an alternator because we understand what it does for us and how we need to use it. > If the larger alternator doesn't have too big >a weight penalty then it might be ok, but energy management is the key. >Even with a 100 amp alternator you will not have enough charging capacity >for extended taxi with every thing on. What kind of airplane are we talking about here? Electrically heated prop? Windshield? Toe warmers? . . . The biggest taxi loads are presented by killer lighting of some kind. Most of the airplanes I fly don't exceed 100W for taxi lamps (8.5A) . . . after that, it falls rapidly from there. I suspect none exceed 20A during night taxi. The way we recommend belting a B&C alternator (leave the stock small pulley on), you'll have FULL output available from the alternator at taxi RPMS. > Alternators do not put out their >rated capacity until you running the engine at cruise rpm so one must use >only what is needed. Why do you think airliners turn off the cabin lights >when landing? Pilot's can't see that light behind them. Because they fly certified airplanes that may or may not be operated with any need to satisfy the physics of the matter. I don't know of any Raytheon product that can't get LOTS of snort out of engine driven power sources even at flight idle . . . and they never get that slow in normal ops. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 03, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Garmin connector
> >Hi all....just got my new 295 (sweet!) and am trying to figure out a >mounting configuration. I need to use the external antenna, but would >like to find a "shallow" coupler for it. That it, the BNC (I think?) >connector sticks too far out to the rear of the unit for a reasonable >surface "flush" mount. Simple BNC to R*-58 type 90 degree connectors I >have locally, but the cable to the antenna is small diameter - not sure >what it is. Any ideas for the connector of choice - ideally shallow >mount and/or 90 degree bend. Also, any tricks to fastening this thin >cable, before I cut the end off the existing connector? >Thx in advance. >Mike There are right angle connectors for use with the miniature coax. Check out http://www.kingselectronics.com/ and search on p/n KC-59-109. This is a typical product for one series of 50-ohm miniature coaxes. You need to make sure we're talking about BNC and what coax is involved. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 03, 2001
From: klehman <klehman(at)albedo.net>
Subject: Alternator size 40 or 60 amp?
I'm sure you are kidding here cause the cabin lighting load is almost insignificant on airliners with mutiple 100kw (or larger) generators. The feds do seem to want your eyes adjusted for night vision though in case of an 'incident'. Ken > Alternators do not put out their >rated capacity until you running the engine at cruise rpm so one must use >only what is needed. Why do you think airliners turn off the cabin lights >when landing? Pilot's can't see that light behind them. ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Dec 03, 2001
Subject: Re: Ring Terminal Sizes
Bob: I am trying to hook up some 14-16 gauge wires to the larger terminals at solenoid area. I find the large S812 series terminals on your site but what I need is the large ring for the stud but small crimp area for 16 guage wire. Is there such an animal? Len Leggette RV-8A N901LL (res) Greensboro, N.C. Hanger # 23 at INT ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Lightspeed Headsets
Date: Dec 03, 2001
I am looking to buy a set of Lightspeed headsets for my RV6A. The three available are: 25XL $500 25-28db of active cancellation 20XL $400 22-24db of active cancellation 15XL $300 16-18db of active cancellation There seems to be quite a difference between the 15XL and the 20XL that is probably worth the $100. What I am wondering about is if the $100 for the 3db difference is "worth it." They are identical other wise except for the inclusion of an extra "ultrasoft" earcup for the 25XL. Comments? Ross Mickey ________________________________________________________________________________
Date: Dec 03, 2001
From: Jaye and Scott Jackson <jayeandscott(at)shaw.ca>
Subject: Re: Alternator size 40 or 60 amp?
> >only what is needed. Why do you think airliners turn off the cabin lights > >when landing? Pilot's can't see that light behind them. > I thought they turned off the cabin lights to allow the passengers night vision to adjust should there be a need for an emergency evacuation on landing. It certainly has nothing to do with the pilot's vision or the electrical loads. Scott in Vancouver > ================================= > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Ed Perry" <eperry(at)san.rr.com>
Subject: Re: Lightspeed Headsets
Date: Dec 03, 2001
Hi Ross, I have the 20K and am very happy with it. What a difference ANR makes. I seriously doubt that you can tell the 3db difference between the 20 and 25XL. Anyway....If you are looking to save some cash I would not hesitate to bid on ebay. I have enclosed a couple of current links to give you an idea on price. I got one from the RV-list for $260 and a new in the box off ebay for $225. http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1671563825 http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1670756232 Ed Perry eperry(at)san.rr.com ----- Original Message ----- From: "Ross Mickey" <rmickey(at)ix.netcom.com> Subject: AeroElectric-List: Lightspeed Headsets > > I am looking to buy a set of Lightspeed headsets for my RV6A. The three > available are: > > 25XL $500 25-28db of active cancellation > 20XL $400 22-24db of active cancellation > 15XL $300 16-18db of active cancellation > > There seems to be quite a difference between the 15XL and the 20XL that is > probably worth the $100. What I am wondering about is if the $100 for the > 3db difference is "worth it." They are identical other wise except for the > inclusion of an extra "ultrasoft" earcup for the 25XL. > > Comments? > > Ross Mickey > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
Date: Dec 03, 2001
From: "Boyd C. Braem" <bcbraem(at)home.com>
Subject: Re: Lightspeed Headsets
Ross-- Decibels are plotted on a logarithmic curve, meaning that a 3 dB increase is a doubling of acoustic power or sound pressure (10 log 2 3.01). At conversational frequencies (1 - 3 kHz) a 3 dB change is just noticeable as a change in volume. A 10 dB change is noted by most subjects as a doubling (or halving) in volume. Thus, across most of the frequecies that you'll be hearing, the noise reduction in the 25XL will be subjectively twice as great as that of the 15XL. See if you can get the frequency response curve for the headsets--if the noise reduction is greatest in the 1 - 5 kHz range, then that's something you will notice (3 - 5 kHz is above normal conversation but accounts for a lot of the "hiss" that you hear). The sensitivity of the ear to changes in low frequency sounds falls off quite a bit (find something called the Fletcher-Munson frequency curves and then invert the curves to find out where noise reduction will be most beneficial), so noise reductiion in this area is not as critical. A very truncated discussion of psychoacoustics. Boyd Ross Mickey wrote: > > > I am looking to buy a set of Lightspeed headsets for my RV6A. The three > available are: > > 25XL $500 25-28db of active cancellation > 20XL $400 22-24db of active cancellation > 15XL $300 16-18db of active cancellation > > There seems to be quite a difference between the 15XL and the 20XL that is > probably worth the $100. What I am wondering about is if the $100 for the > 3db difference is "worth it." They are identical other wise except for the > inclusion of an extra "ultrasoft" earcup for the 25XL. > > Comments? > > Ross Mickey > ________________________________________________________________________________
Date: Dec 03, 2001
From: "Boyd C. Braem" <bcbraem(at)home.com>
Subject: Re: Lightspeed Headsets
I forgot. The acid test is to try them in your plane with your intercom. If you like 'em, then throw out all those frequency curves and fly on. But it does explain why a "high-frequency wife" gets cancelled out but not the teen-age drummer--be lucky the other sibling is not a bass player. "Boyd C. Braem" wrote: > > > Ross-- > > Decibels are plotted on a logarithmic curve, meaning that a 3 dB > increase is a doubling of acoustic power or sound pressure (10 log 2 > 3.01). At conversational frequencies (1 - 3 kHz) a 3 dB change is just > noticeable as a change in volume. A 10 dB change is noted by most > subjects as a doubling (or halving) in volume. > > Thus, across most of the frequecies that you'll be hearing, the noise > reduction in the 25XL will be subjectively twice as great as that of the > 15XL. See if you can get the frequency response curve for the > headsets--if the noise reduction is greatest in the 1 - 5 kHz range, > then that's something you will notice (3 - 5 kHz is above normal > conversation but accounts for a lot of the "hiss" that you hear). The > sensitivity of the ear to changes in low frequency sounds falls off > quite a bit (find something called the Fletcher-Munson frequency curves > and then invert the curves to find out where noise reduction will be > most beneficial), so noise reductiion in this area is not as critical. > > A very truncated discussion of psychoacoustics. > > Boyd > > Ross Mickey wrote: > > > > > > I am looking to buy a set of Lightspeed headsets for my RV6A. The three > > available are: > > > > 25XL $500 25-28db of active cancellation > > 20XL $400 22-24db of active cancellation > > 15XL $300 16-18db of active cancellation > > > > There seems to be quite a difference between the 15XL and the 20XL that is > > probably worth the $100. What I am wondering about is if the $100 for the > > 3db difference is "worth it." They are identical other wise except for the > > inclusion of an extra "ultrasoft" earcup for the 25XL. > > > > Comments? > > > > Ross Mickey > > > ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: Lightspeed Headsets
Date: Dec 03, 2001
Thanks so much. I will keep looking at ebay. Ross ----- Original Message ----- From: "Ed Perry" <eperry(at)san.rr.com> Subject: Re: AeroElectric-List: Lightspeed Headsets > > Hi Ross, > > I have the 20K and am very happy with it. What a difference ANR makes. I > seriously doubt that you can tell the 3db difference between the 20 and > 25XL. Anyway....If you are looking to save some cash I would not hesitate to > bid on ebay. I have enclosed a couple of current links to give you an idea > on price. I got one from the RV-list for $260 and a new in the box off ebay > for $225. > http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1671563825 > http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1670756232 > > Ed Perry > eperry(at)san.rr.com > ----- Original Message ----- > From: "Ross Mickey" <rmickey(at)ix.netcom.com> > To: > Subject: AeroElectric-List: Lightspeed Headsets > > > > > > > I am looking to buy a set of Lightspeed headsets for my RV6A. The three > > available are: > > > > 25XL $500 25-28db of active cancellation > > 20XL $400 22-24db of active cancellation > > 15XL $300 16-18db of active cancellation > > > > There seems to be quite a difference between the 15XL and the 20XL that is > > probably worth the $100. What I am wondering about is if the $100 for the > > 3db difference is "worth it." They are identical other wise except for > the > > inclusion of an extra "ultrasoft" earcup for the 25XL. > > > > Comments? > > > > Ross Mickey > > > > > > > > > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: Lightspeed Headsets
Date: Dec 03, 2001
----- Original Message ----- From: "Boyd C. Braem" <bcbraem(at)home.com> > See if you can get the frequency response curve for the > headsets--if the noise reduction is greatest in the 1 - 5 kHz range, > then that's something you will notice (3 - 5 kHz is above normal > conversation but accounts for a lot of the "hiss" that you hear). Boyd, A curve is shown on the Lightspeed website but I can't decipher it. http://www.anrheadsets.com/products25xl.html Ross ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Lightspeed Headsets
Date: Dec 03, 201
Boyd C. Braem wrote: > > > A very truncated discussion of psychoacoustics. > *** Here's another consideration - Lightspeed headsets are not the most mechanically robust. I have a pair of 25K's - they're literally falling apart. Lightspeed support is very good - they fix'em for free - but I can't quite bring myself to send mine away :). - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 03, 2001
From: efortner <efortner(at)vnet.net>
Subject: Re: Lightspeed Headsets
I have the 25XL and am very pleased with it; howevery it failed after about 15 minutes of use. It was returned for repair and turnaround was quick. They said it had a broken wire. I have had it for over a year now with no further problems. Earl RV4 Ed Perry wrote: > > Hi Ross, > > I have the 20K and am very happy with it. What a difference ANR makes. I > seriously doubt that you can tell the 3db difference between the 20 and > 25XL. Anyway....If you are looking to save some cash I would not hesitate to > bid on ebay. I have enclosed a couple of current links to give you an idea > on price. I got one from the RV-list for $260 and a new in the box off ebay > for $225. > http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1671563825 > http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1670756232 > > Ed Perry > eperry(at)san.rr.com > ----- Original Message ----- > From: "Ross Mickey" <rmickey(at)ix.netcom.com> > To: > Subject: AeroElectric-List: Lightspeed Headsets > > > > > > I am looking to buy a set of Lightspeed headsets for my RV6A. The three > > available are: > > > > 25XL $500 25-28db of active cancellation > > 20XL $400 22-24db of active cancellation > > 15XL $300 16-18db of active cancellation > > > > There seems to be quite a difference between the 15XL and the 20XL that is > > probably worth the $100. What I am wondering about is if the $100 for the > > 3db difference is "worth it." They are identical other wise except for > the > > inclusion of an extra "ultrasoft" earcup for the 25XL. > > > > Comments? > > > > Ross Mickey > > > > > > > > > ________________________________________________________________________________
Date: Dec 03, 2001
From: "Richard V. Reynolds" <rvreynolds(at)macs.net>
Subject: Re: Ring Terminal Sizes
Lenleg(at)aol.com wrote: I am trying to hook up some 14-16 gauge wires to the larger terminals at solenoid area. I find the large S812 series terminals on your site but what I need is the large ring for the stud but small crimp area for 16 guage wire. Is there such an animal? Go to your local West Marine or BOAT US store. ANCOR makes a good terminal in most every size. Richard Reynolds ________________________________________________________________________________
From: "Sam Chambers" <schamber@glasgow-ky.com>
Subject: Re: Redundant systems
Date: Dec 03, 2001
Pat, Sorry for the long delay in responding to this. I found the same information in the manual that you mentioned and did not see anything about the failure annunciation. Maybe I either dreamed it or Ron Roberts told me on the phone about some indication of failure of one ignition system. I haven't had a chance to check through my lengthy notes yet but a call to Ron may be in order here. Sorry for the apparent false information, if I find out anything different, I will let you know. Sam Chambers Long-EZ N775AM ----- Original Message ----- From: "pat_hatch" <pat_hatch(at)email.msn.com> Subject: Re: AeroElectric-List: Redundant systems > > Sam, > > Could you elaborate on how the Electronics Internationals tach monitors both > ignition systems? I have their R-1 gauge with dual electronic ignitions and > I have read through their manual and cannot find any reference to this. It > does say that during the "mag" check you will see a large drop in RPM for 1 > sec when switching from BOTH to LEFT mag while the microprocessor switches > to the other mag. My gauge has no annunciator that I can see that would > indicate a failure. Is there a more recent mod to the gauge perhaps? I > recently had my R-1 modified by E.I. for the electronic ignition and larger > numbers, but they did not mention anything about this. > > Pat Hatch > RV-4, N17PH @ VRB, 700 hours TT > O-320, Hartzell C/S > RV-6, Fuselage > O-360, Hartzell C/S > > ----- Original Message ----- > From: "Sam Chambers" <schamber@glasgow-ky.com> > To: > Subject: Re: AeroElectric-List: Redundant systems > > > <schamber@glasgow-ky.com> > > > > Electronics International's tach monitors both ingition systems and > > annunciates a failure. They can and will custom tailor the signal > > conditioning to whatever your system needs. > > > > Sam Chambers > > Long-EZ N775AM > > ----- Original Message ----- > > From: "Gary Casey" <glcasey(at)gte.net> > > To: > > Subject: AeroElectric-List: Redundant systems > > > > > > > > > > >> I did have an electronic ignition failure while in flight. (the mag > > > saved > > > my butt). Turns out the inductive pickup went intermittent. But as > you've > > > stated, the chances of a failure are very slim if everything has been > > > installed correctly. Having two systems fail at the same time (assuming > no > > > power loss) is almost impossible....<< > > > > > > I've been thinking about the discussion of "redundancy" with regard to > one > > > electronic/one mag ignition. The previous posts imply that the mag can > > fail > > > undetected because of the timing difference between the electronic > system > > > and the mag. This then fails one of the tests for redundancy. For > > > instance, assume that the mag fails early in a long flight - over > hostile > > > terrain of course. That means that you are going to make the whole > flight > > > without a backup ignition and not know it. This is what brought down > the > > > 737's a while back - the backup hydraulic system would fail and there > > wasn't > > > a good way to detect it until the primary also failed. The idea of a > > > "single failure mode" being all that is necessary to worry about only > > works > > > if you can detect that failure. Am I worrying about nothing? One > > previous > > > post said the mag is much more likely to fail than the electronic system > > and > > > another reported on an electronic system failure. The population of > > > electronic systems is very small so one known failure is a lot. Sounds > > like > > > an ignition monitoring system might be worthwhile. > > > > > > Gary Casey > > > C177RG > > > > > > > > > > > > ________________________________________________________________________________
Date: Dec 03, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Ring Terminal Sizes
> > >Lenleg(at)aol.com wrote: > >I am trying to hook up some 14-16 gauge wires to the larger terminals at >solenoid area. I find the large S812 series terminals on your site but what I >need is the large ring for the stud but small crimp area for 16 guage wire. Is >there such an animal? Sure . . . from our website catalog at: http://www.aeroelectric.com/Catalog/BCcatalog.html where you'll find an S814B38 which is a blue insulator (14-16AWG) and 3/8" stud and an S814B31 which fits a 5/16" stud. >Go to your local West Marine or BOAT US store. ANCOR makes a good terminal in >most every size. BE WARY OF STORES BEARING TERMINALS . . . not all terminals are the same. See: http://209.134.106.21/articles/terminal.pdf Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 03, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: alternator field switch
> >Bob: > Sorry if I'm the 10,000th guy to ask this, but on page 11-20 of your >book you advise using a 2-3 switch to control battery master contactor >AND alt. field current simultaneously, but you don't say why. It always >made sense to me to be able to disconnect the alt. field coil separately >in order to avoid wasting power into it when the alternator fails and >you're running off the battery only. The Z-1 schematic shows the same >switch. when most of the folks building MODERN single engine airplanes have an essential bus that is powered independently of the main bus. If the alternator fails, one wants to shut down the main bus which takes care of the alternator field loads -AND- battery contactor. If there's a need to keep the main bus up via the battery contactor, then you can pull the alternator field breaker while leaving the DC power master switch ON. This is most often done during maintenance ops on the ground to minimize battery loads. Another option is to wire the DC POWER MASTER with an S700-2-10 switch - two pole, three position, progressive transfer. With this switch, one can emulate the features of the mystical-magic split-rocker switch that's found on many certified ships and too many homebuilts. The lower position is OFF, first position is BATTERY only, the second position adds the ALT FIELD. This is the switch shown in the latest incarnations of the 'Connections power distribution diagrams at: http://209.134.106.21/articles/Rev10/z10.pdf >Are you depending on the B&C voltage regulator to not power the field >coil when the alt. dies? Nope, it's all done with switches as described above. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: "Richard Sipp" <rsipp(at)earthlink.net>
Subject: Load Analysis
Date: Dec 03, 2001
> I've yet to see a single engine airplane homebuilt that won't > run well on a 40A machine. The largest full-up, night-ifr running > load I've calculated so far is 27A which leaves 13A for battery > support. Bob: This certainly agrees with a normal "everything on" load of about 15 amps for my airplane. Using the above logic, the Z appendix drawings that call for awg 4 or 5 wire for the alternator output seems to be more than required. Assuming even a 100% increase in load for a short battery charging period, would not awg 8 be adequate? An informal eyeball survey on my local ramp seems to show smaller than awg 4 wires on the alternator supply leads. Do you recommend the larger wire and 80 amp in line fuse to protect against a potential battery feed short in this wire? Dick Sipp RV4 250DS ________________________________________________________________________________
From: "Rick" <turboflyer(at)mediaone.net>
Subject: Lightspeed Headsets
Date: Dec 03, 2001
If its just the U shapes part that holds the ear cups, they will send you the parts, easy fix. Rick -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of jerry(at)tr2.com Subject: Re: AeroElectric-List: Lightspeed Headsets Boyd C. Braem wrote: > > > A very truncated discussion of psychoacoustics. > *** Here's another consideration - Lightspeed headsets are not the most mechanically robust. I have a pair of 25K's - they're literally falling apart. Lightspeed support is very good - they fix'em for free - but I can't quite bring myself to send mine away :). - Jerry Kaidor ( jerry(at)tr2.com ) http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
From: jerry(at)tr2.com
Subject:
Date: Dec 03, 201
Rick wrote: > > > If its just the U shapes part that holds the ear cups, they will send you > the parts, easy fix. *** Stirrups? Already replaced those twice. They're OK for the moment. * One of the "cups" that form the outside of the earpieces has fallen apart, a big chunk fell out. * The headband has developed some cracks at its stress points. * The electronics box broke at one side - I taped it together. * The R/H pot slider doohicky broke - that side is stuck at full volume. * One of the foam surrounds keeps coming unglued. ...But electrically, it's a fantastic headset. And I know Lightspeed will fix it all, no problem. Just can't stand to take even one flight without that cushy feel & ANR. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Subject: Interconnection
Date: Dec 04, 2001
From: "Mike Gray" <mgray(at)graymatter.org>
In reading the list over the last few months - and at the same time trying to decide which aircraft to build I haven't seen much discussion on avionics installation issues. Nowdays there is little need for the old vacuum instruments as more and more manufacturers are coming up with the most sophisticated EFIS type instrumentation - much of which has been discussed on this list. Use of this new technology dramatically increases the complexity of panel wiring while reducing the plumbing. I really do not want to build a harness that may have as many as 15 plugs on it each with cables running from different plugs, sometimes with joins to multiple connectors. In trying to come up with a simple avionics wiring system I thought about using commonly available computer type DB9 / DB25 cables and - for lack of a better word - an "interface box". My theory is this - matching connectors on the avionics - for example a DB15F on the Microair 760 would interface through a computer type DB15 F - M cable to a DB15M on the "interface box". All wiring - from for example the headphone out (pin 14 on the Microair) to a COM1 position on the audio selector would be made inside this box eliminating the need for a complex harness which would have to be hand made in the traditional method. At the worst case the substitution of the Microair for another make of radio would simply require one custom cable DB15F on the interface box to whatever the pin was on the new radio. In many cases simple IDC (insulation displacement) style connectors and the appropriate connector would suffice. However I am not sure if the use of this non-aviation cable (behind the firewall) would be permitted. Obviously the box would be screened and the odd cable would have to be hand made (mainly to overcome problems of interference and crosstalk where the maker has routed mic level and speaker outs together on one DB connector). An additional possibility is that the box could contain a 12V 4Ah NiCad which would trickle charge from the Avionics buss and provide a final emergency backup for several instruments. Does this make sense to those far more experienced than myself? Mike Gray ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Terminal terminals
Date: Dec 03, 2001
>Go to your local West Marine or BOAT US store. ANCOR makes a good terminal in>most every size. BE WARY OF STORES BEARING TERMINALS . . . not all terminals are the same. See: http://209.134.106.21/articles/terminal.pdf Bob . . . Cheers, I'll second that! I'm sitting here slowly cooling off because the pressure switch which enables the gas burner in my furnace has a broken ring connector hanging off it. VIBRATION broke its neck. I am at the computor, so I can welcome the warrantee man who is coming with the right unit. Ferg Europa A064 ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Cabin lights
Date: Dec 03, 2001
Why do you think airliners turn off the cabin lights when landing? Pilot's can't see that light behind them. I think they used to turn them off to prepare passengers for landing - mentally. Matching the lights to the environment is one way. Turning off the movie is another. Setting the cabin staff in their seats is another. However, some manufacturers have decided to 'automate' the decision or have left it to the cabin folk. Bad move. Ferg DC3,DC4M2,Visc,Vang,L1049,DC8,DC9,L10,L1011,B767 ________________________________________________________________________________
Date: Dec 04, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Load Analysis
> > >> I've yet to see a single engine airplane homebuilt that won't >> run well on a 40A machine. The largest full-up, night-ifr running >> load I've calculated so far is 27A which leaves 13A for battery >> support. > >Bob: > >This certainly agrees with a normal "everything on" load of about 15 amps >for my airplane. Using the above logic, the Z appendix drawings that call >for awg 4 or 5 wire for the alternator output seems to be more than >required. Assuming even a 100% increase in load for a short battery >charging period, would not awg 8 be adequate? An informal eyeball survey on >my local ramp seems to show smaller than awg 4 wires on the alternator >supply leads. Do you recommend the larger wire and 80 amp in line fuse to >protect against a potential battery feed short in this wire? 4AWG was a one-size-fits all that was mated with the terminals supplied in our b-lead fuse kit of some years past. It wasn't that 4AWG was necessary, just that it didn't hurt anything and will mate with the hardware in the kit. 8AWG would be fine too. I'm going to be taking the b-lead fuse kit off the website catalog and replacing it with ANL current limiters and the appropriate mounting base. When this is done, customers will supply their own terminals to attach to the mounting base and can size the alternator b-lead accordingly. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Interconnection
Date: Dec 04, 201
Mike Gray wrote: > > > the most sophisticated EFIS type instrumentation - much of which has > been discussed on this list. Use of this new technology dramatically > increases the complexity of panel wiring while reducing the plumbing. I > really do not want to build a harness that may have as many as 15 plugs > joins to multiple connectors. In trying to come up with a simple > avionics wiring system I thought about using commonly available computer > My theory is this - matching connectors on the avionics - for example a > DB15F on the Microair 760 would interface through a computer type DB15 F > - M cable to a DB15M on the "interface box". All wiring - from for > example the headphone out (pin 14 on the Microair) to a COM1 position on > the audio selector would be made inside this box eliminating the need > for a complex harness which would have to be hand made in the *** How about making the big central box ( BCB ) standardized? With little individual boxes for the radios and instruments, converting them to a standard? That way, if a navcom broke or became obsolete, you would be able to plug in any other navcom that fit in the hole. Another issue is ease of maintenance. The coolest BCB would open up and swing out. Every single signal would be available as a test point. It might even have a trouble light built into the top! The perimeter of the BCB might be populated with DB25's. Each DB25 would have a standardized internal "patch board" that could be freely wired to other stuff inside the BCB. So you set up a little photographic circuit board foundry - make up a bunch of these patch boards - or have them made up. Each board would take a PC-mount DB25. The DB25 solders into the patch board, and mounts to the edge of the BCB with screws. There's your support for the patch board, too. One key to making something like this work, is not to use the frame of the BCB as a ground. Have one ground buss inside the BCB for power, another one for signal, tie the two together at one point, and tie that point to the main ground of the airplane. Peripheral Adaptor Boxes ( PABs ) would consist of a little plastic case containing a single DB25 with a patch board, same as the ones inside the BCB. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 04, 2001
From: "Boyd C. Braem" <bcbraem(at)home.com>
Subject: Re: Lightspeed Headsets
What they're showing in the graph (tho I can't read what's represented in the left-hand scale) is a bandpass filter allowing the speech frequencies centered on 1 kHz to come thru and then attenuating the frequencies above and below by either -6/-12 dB per octave. This allows your (male) voice to go thru but blocks the frequencies on either side of it. A female with a voice an octave higher (a musical note is an octave higher if it is double the frequency of the lower note) might get cut out a bit, here (ie, there's a real sharp cut at 2 kHz). If the ANR only occurs thru the mic-to-headphone circuit then you shouldn't notice any difference in the music you hear coming out of the intercom--you'll notice that there's quite a difference between the frequency response of the mic compared to the earphones. Boyd Ross Mickey wrote: > > > ----- Original Message ----- > From: "Boyd C. Braem" <bcbraem(at)home.com> > > > See if you can get the frequency response curve for the > > headsets--if the noise reduction is greatest in the 1 - 5 kHz range, > > then that's something you will notice (3 - 5 kHz is above normal > > conversation but accounts for a lot of the "hiss" that you hear). > > Boyd, > > A curve is shown on the Lightspeed website but I can't decipher it. > http://www.anrheadsets.com/products25xl.html > > Ross > ________________________________________________________________________________
Subject: measuring RPM from a mag
Date: Dec 04, 2001
From: "Bob Japundza" <Bob.Japundza(at)realmed.com>
Hi Guys, I am wanting to monitor RPM with an engine monitor of my own creation via the p-lead off of a magneto. My plan is to use a NTE3090 optoisolator and a 10K resistor from the p-lead to get TTL pulses which if I'm thinking correctly will be two pulses per revolution. Will this work? Bob Japundza RV-6 N244BJ O-360C/S flying 252 hours ________________________________________________________________________________
Date: Dec 04, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Interconnection
> >In reading the list over the last few months - and at the same time >trying to decide which aircraft to build I haven't seen much discussion >on avionics installation issues. Nowdays there is little need for the >old vacuum instruments as more and more manufacturers are coming up with >the most sophisticated EFIS type instrumentation - much of which has >been discussed on this list. Use of this new technology dramatically >increases the complexity of panel wiring while reducing the plumbing. I >really do not want to build a harness that may have as many as 15 plugs >on it each with cables running from different plugs, sometimes with >joins to multiple connectors. In trying to come up with a simple >avionics wiring system I thought about using commonly available computer >type DB9 / DB25 cables and - for lack of a better word - an "interface >box". Airplanes have used these since WWII . . . I helped design, install and document a really fat on for the military version of a Cessna 337 (The O-2A featured in numerous Vietnam movies). EVERYTHING went through that box. Really friendly for installing the various systems on the line but there was probably as much labor in building the box as their was in all the rest of the harnesses that connected to it. >My theory is this - matching connectors on the avionics - for example a >DB15F on the Microair 760 would interface through a computer type DB15 F >- M cable to a DB15M on the "interface box". All wiring - from for >example the headphone out (pin 14 on the Microair) to a COM1 position on >the audio selector would be made inside this box eliminating the need >for a complex harness which would have to be hand made in the >traditional method. At the worst case the substitution of the Microair >for another make of radio would simply require one custom cable DB15F on >the interface box to whatever the pin was on the new radio. In many >cases simple IDC (insulation displacement) style connectors and the >appropriate connector would suffice. However I am not sure if the use of >this non-aviation cable (behind the firewall) would be permitted. You can use any kind of connectors you want to . . . nobody's permission is necessary. What you seem to be describing is a multi-system junction box . . . widely used in past designs to facilitate a production situation where hundreds or thousands of airplanes needed to be assembled. The j-box permits slicing installations up into discrete harness assemblies that go into the airplane like tinker-toy parts. >Obviously the box would be screened and the odd cable would have to be >hand made (mainly to overcome problems of interference and crosstalk >where the maker has routed mic level and speaker outs together on one DB >connector). An additional possibility is that the box could contain a >12V 4Ah NiCad which would trickle charge from the Avionics buss and >provide a final emergency backup for several instruments. > >Does this make sense to those far more experienced than myself? In spite of an increase in capability and greater integration of functionality of current products and things coming over the hill, the number of wires in the system continue to go DOWN. We're making more use of serial data communication and integrating more functions into fewer black boxes. If you were going to build hundreds of cookie-cutter airplanes, pre-assembled harnesses and junction boxes might make sense but the ultimate goal is to minimize the total number of joints in every conductor. J-boxes take us in the wrong direction. I'll venture to say that assembling the full avionics package of a modern light plane will have less than half the number of black boxes, 1/4th the wire and give more capability than similar full-up systems of 30 years ago. I'd look VERY carefully at including any kind of j-box. I helped a guy put one in his Velocity project about 10 years ago. It sure LOOKED neat but it had to more than double the time to put the system together. Bob . . . ________________________________________________________________________________
From: "John Anderson" <janderson412(at)hotmail.com>
Subject: Re: Cabin lights
Date: Dec 05, 2001
Good point Ferg, I've often wondered. John A. ----- Original Message ----- From: Fergus Kyle Subject: AeroElectric-List: Cabin lights Why do you think airliners turn off the cabin lights when landing? Pilot's can't see that light behind them. I think they used to turn them off to prepare passengers for landing - mentally. Matching the lights to the environment is one way. Turning off the movie is another. Setting the cabin staff in their seats is another. However, some manufacturers have decided to 'automate' the decision or have left it to the cabin folk. Bad move. Ferg DC3,DC4M2,Visc,Vang,L1049,DC8,DC9,L10,L1011,B767 = = = = c-list = Get mor ________________________________________________________________________________
From: "Ronnie Brown" <romott(at)adelphia.net>
Subject: Re: Lightspeed Headsets
Date: Dec 04, 2001
And the 15K's are well worth the money too! I have two of them - had them for several years. I haven't had ANY problems with them. And they work as well as a friend's $1000 Bose. GREAT Value Ronnie ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: oil switch
Date: Dec 04, 2001
I know this has been a topic before and I have searched the archives but didn't find the answer. I have two of the oil switches from B&C. I would think that I would get continuity between the common pole and the normally closed pole, but I don't on either switch. I am testing them on my bench with a meter. What am I not seeing here?? Jerry Calvert Edmond Ok -6 ________________________________________________________________________________
From: "David Swartzendruber" <dswartzendruber(at)earthlink.net>
Subject: Re: Interconnection
Date: Dec 04, 2001
How about a J-box that interconnected everything with a printed circuit board and connectors that soldered directly to the board and poked out through the box? David Swartzendruber Wichita > > In spite of an increase in capability and greater integration > of functionality of current products and things coming over the > hill, the number of wires in the system continue to go DOWN. > We're making more use of serial data communication and integrating > more functions into fewer black boxes. If you were going to > build hundreds of cookie-cutter airplanes, pre-assembled harnesses > and junction boxes might make sense but the ultimate goal is to > minimize the total number of joints in every conductor. J-boxes > take us in the wrong direction. > > I'll venture to say that assembling the full avionics package > of a modern light plane will have less than half the number of > black boxes, 1/4th the wire and give more capability than > similar full-up systems of 30 years ago. I'd look VERY carefully > at including any kind of j-box. I helped a guy put one in his > Velocity project about 10 years ago. It sure LOOKED neat but it > had to more than double the time to put the system together. > > Bob . . . > ________________________________________________________________________________
From: W4PPN(at)aol.com
Date: Dec 04, 2001
Subject: Re: oil switch
Jerry they are supposed to close under pressure. When you have oil pressure the switch closes and applies 12 Volts to a Hobbs meter and it starts counting the time you have run the engine. Of course there are switches that are closed until you apply oil pressure and then they open. I bought one that does both so I can incorporate it into my system. One side will run the hobbs meter when I have oil pressure and the other side will either turn a light on to let me know that the Master Switch is still on after the engine has shut down, or I can hook it up to a buzzer that will let me know that the Master Sw is still on. Howard 1/2 of an RV-8 project. Mooresville, NC ________________________________________________________________________________
Date: Dec 04, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: measuring RPM from a mag
> >Hi Guys, > >I am wanting to monitor RPM with an engine monitor of my own creation >via the p-lead off of a magneto. My plan is to use a NTE3090 >optoisolator and a 10K resistor from the p-lead to get TTL pulses which >if I'm thinking correctly will be two pulses per revolution. Will this >work? last time I 'scoped a p-lead, it had LOTS of trash that included ringing with excursions above and below ground. I ended up using the the first excursion to trigger a one- shot multivibrator with a time constant long enough to ignore the rest of the trash. That was part of a prop-synchronizer system I was working on for the Cessna light twins about 25 years ago. Haven't had occasion to look at one since. I suspect it's STILL quite trashy and will need some kind of filter philosophy to avoid multiple triggers of a single point opening. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 04, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Interconnection
> >*** How about making the big central box ( BCB ) standardized? With little >individual boxes for the radios and instruments, converting them to a >standard? That way, if a navcom broke or became obsolete, you would be >able to plug in any other navcom that fit in the hole. > > Another issue is ease of maintenance. The coolest BCB would open up and >swing out. Every single signal would be available as a test point. It >might even have a trouble light built into the top! > > The perimeter of the BCB might be populated with DB25's. Each DB25 would >have a standardized internal "patch board" that could be freely wired to >other stuff inside the BCB. So you set up a little photographic circuit >board foundry - make up a bunch of these patch boards - or have them made >up. Each board would take a PC-mount DB25. The DB25 solders into the >patch board, and mounts to the edge of the BCB with screws. There's your >support for the patch board, too. > > One key to making something like this work, is not to use the frame of >the BCB as a ground. Have one ground buss inside the BCB for power, another >one for signal, tie the two together at one point, and tie that point to the >main ground of the airplane. > > Peripheral Adaptor Boxes ( PABs ) would consist of a little plastic case >containing a single DB25 with a patch board, same as the ones inside the >BCB. > > - Jerry Kaidor ( jerry(at)tr2.com ) Sheesh! How many new joints and connectors would this add to all the wires? I was just setting here figuring out my fondest wishes instrument panel. Garmin GPS/Nav/Com, transponder, encoder (this will go away soon . . . transponders will get built in encoders). The only place components of this system touch each other is panel lighting and power supplies. Hmmm . . . how about a poor mans system. Microair transceiver, some superwhippy panel mount GPS, transponder, encoder. Maybe some alarm tones to the headsets and a stereo system. Again, power and lighting commonality but with some audio added . . . nothing that the po'man's audio distribution amplifier couldn't handle. See http://209.134.106.21/articles/audio/760v4.pdf If I had a j-box mounted somewhere, I cannot figure out what I would what to run through it and in particular, how the installation would be any simpler/easier by running any wires through a j-box. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: oil switch
Date: Dec 05, 2001
The switch you are refering to is what I have. The switch has 3 connections. A common pole, a normally open pole, and a normally closed pole. When there is no pressure in the switch, I would think the common pole and the normally closed pole would make a complete circuit, but neither switch do. This confuses me. Thanks for the reply, Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: <W4PPN(at)aol.com> Subject: Re: AeroElectric-List: oil switch > > Jerry they are supposed to close under pressure. When you have oil pressure > the switch closes and applies 12 Volts to a Hobbs meter and it starts > counting the time you have run the engine. > > Of course there are switches that are closed until you apply oil pressure and > then they open. > > I bought one that does both so I can incorporate it into my system. One side > will run the hobbs meter when I have oil pressure and the other side will > either turn a light on to let me know that the Master Switch is still on > after the engine has shut down, or I can hook it up to a buzzer that will let > me know that the Master Sw is still on. > > Howard > 1/2 of an RV-8 project. > Mooresville, NC > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: Re: Interconnection
Date: Dec 05, 2001
----- Original Message ----- From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> > I was just setting here figuring out my fondest wishes instrument panel. > Garmin GPS/Nav/Com, transponder, encoder (this will go away soon . . . transponders > will get built in encoders). Bob: A couple of years ago when Upsat introduced their new transponder I gave them particular hell for not including an encoder in the new design. I did this more than once. What I got for response was a rather lame "Well, we probably couldn't get it in our 1.3" box," to which I suggested that maybe this fixation on a standard box was just flat wrong. Then they said that they expected their new txp to go into aircraft that already had encoders. When asked if they just figured to blow off the new aircraft part of the market the conversation just died away. I believe it just never occured to them to combine the two functions. Now you come up with the above comment. Do you know for a fact that this will happen, and who will be the first to do it? Gordon Comfort N363GC ________________________________________________________________________________
Subject: measuring RPM from a mag
Date: Dec 05, 2001
From: "Bob Japundza" <Bob.Japundza(at)realmed.com>
> last time I 'scoped a p-lead, it had LOTS of trash that > included ringing with excursions above and below ground. > I ended up using the the first excursion to trigger a one- > shot multivibrator with a time constant long enough to ignore > the rest of the trash. That was part of a prop-synchronizer > system I was working on for the Cessna light twins about > 25 years ago. Haven't had occasion to look at one since. > I suspect it's STILL quite trashy and will need some kind > of filter philosophy to avoid multiple triggers of a single > point opening. > > I was afraid of that. I'm certain I can take care of that in my code, by ignoring any other pulses for a few uS after the first pulse. At this point the question in my mind is how much variation in voltage I'll see in the pulses to effectively trigger the pulse output of the optoisolator. Bob Japundza RV-6 N244BJ O-360C/S flying ________________________________________________________________________________
Date: Dec 05, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: RE: measuring RPM from a mag
> >> last time I 'scoped a p-lead, it had LOTS of trash that >> included ringing with excursions above and below ground. >> I ended up using the the first excursion to trigger a one- >> shot multivibrator with a time constant long enough to ignore >> the rest of the trash. That was part of a prop-synchronizer >> system I was working on for the Cessna light twins about >> 25 years ago. Haven't had occasion to look at one since. >> I suspect it's STILL quite trashy and will need some kind >> of filter philosophy to avoid multiple triggers of a single >> point opening. >> >> > >I was afraid of that. I'm certain I can take care of that in my code, >by ignoring any other pulses for a few uS after the first pulse. At >this point the question in my mind is how much variation in voltage I'll >see in the pulses to effectively trigger the pulse output of the >optoisolator. The "signal" (if you want to call it that) has a peak amplitude in the several hundreds of volts . . . about 300 as I recall. This is why poking 'round the p-lead connections behind the panel with the engine running is fraught with surprises. Only got "bit" once . . . learned very quickly. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 05, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Interconnection
> > >----- Original Message ----- >From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> >> I was just setting here figuring out my fondest wishes instrument >panel. >> Garmin GPS/Nav/Com, transponder, encoder (this will go away soon . . . >transponders >> will get built in encoders). > >Bob: A couple of years ago when Upsat introduced their new transponder I >gave them particular hell for not including an encoder in the new design. I >did this more than once. What I got for response was a rather lame "Well, >we probably couldn't get it in our 1.3" box," to which I suggested that >maybe this fixation on a standard box was just flat wrong. Then they said >that they expected their new txp to go into aircraft that already had >encoders. When asked if they just figured to blow off the new aircraft part >of the market the conversation just died away. I believe it just never >occured to them to combine the two functions. Now you come up with the >above comment. Do you know for a fact that this will happen, and who will >be the first to do it? > >Gordon Comfort >N363GC\ Nope. I've talked to a couple of folks. They all see 5-7 cubic inches of volume when they close their eyes and imagine an encoder. I've been telling folks that 1.0 to 1.2 cubic inches is closer. I told them how to do it . . . haven't heard back. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 05, 2001
Subject: Re: oil switch
From: <racker(at)rmci.net>
Jerry, According to Bob's diagram (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), there should be continuity between leads "P" and "S" with no oil pressure (i.e. oil pressure idiot light/buzzer circuit), and leads "P" and "I" with oil pressure (i.e hobbs meter circuit). I'll check my switch tonight at home. Rob Acker (RV-6). > > > The switch you are refering to is what I have. The switch has 3 > connections. A common pole, a normally open pole, and a normally > closed pole. When there is no pressure in the switch, I would think > the common pole and the normally closed pole would make a complete > circuit, but neither switch do. This confuses me. > > Thanks for the reply, > Jerry Calvert > Edmond Ok -6 > ----- Original Message ----- > From: <W4PPN(at)aol.com> > To: > Subject: Re: AeroElectric-List: oil switch > > >> >> Jerry they are supposed to close under pressure. When you have oil > pressure >> the switch closes and applies 12 Volts to a Hobbs meter and it starts >> counting the time you have run the engine. >> >> Of course there are switches that are closed until you apply oil >> pressure > and >> then they open. >> >> I bought one that does both so I can incorporate it into my system. >> One > side >> will run the hobbs meter when I have oil pressure and the other side >> will either turn a light on to let me know that the Master Switch is >> still on after the engine has shut down, or I can hook it up to a >> buzzer that will > let >> me know that the Master Sw is still on. >> >> Howard >> 1/2 of an RV-8 project. >> Mooresville, NC >> >> >> >> > > > generous support! http://www.matronics.com/contribution > direct advertising on the Matronics Forums. > Engine: http://www.matronics.com/search > Other Lists: http://www.matronics.com/emaillists ________________________________________________________________________________
From: Don Hyde <DonH(at)axonn.com>
Subject: Re: Interconnection
Date: Dec 05, 2001
A couple of years ago I wired up an altimeter/airspeed indicator using a microcontroller and solid-state pressure sensors. On the breadboard with wires hanging out and no attempt at packaging, it is less than 5 cu. in. SMT, with only one sensor for altitude, 1 cu.in. easy. And parts cost under $20 also easy. > -----Original Message----- > From: Robert L. Nuckolls, III [mailto:nuckolls(at)aeroelectric.com] > Sent: Wednesday, December 05, 2001 9:31 AM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: Re: Interconnection > > > III" > > Comfort" > > > > > >----- Original Message ----- > >From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> > >> I was just setting here figuring out my fondest wishes > instrument > >panel. > >> Garmin GPS/Nav/Com, transponder, encoder (this will go > away soon . . . > >transponders > >> will get built in encoders). > > > >Bob: A couple of years ago when Upsat introduced their new > transponder I > >gave them particular hell for not including an encoder in > the new design. I > >did this more than once. What I got for response was a > rather lame "Well, > >we probably couldn't get it in our 1.3" box," to which I > suggested that > >maybe this fixation on a standard box was just flat wrong. > Then they said > >that they expected their new txp to go into aircraft that already had > >encoders. When asked if they just figured to blow off the > new aircraft part > >of the market the conversation just died away. I believe it > just never > >occured to them to combine the two functions. Now you come > up with the > >above comment. Do you know for a fact that this will > happen, and who will > >be the first to do it? > > > >Gordon Comfort > >N363GC\ > > Nope. I've talked to a couple of folks. They all see 5-7 cubic > inches of volume when they close their eyes and imagine an > encoder. I've been telling folks that 1.0 to 1.2 cubic inches > is closer. I told them how to do it . . . haven't heard back. > > > Bob . . . > > //// > (o o) > ===========o00o=(_)=o00o========= > < Go ahead, make my day . . . > > < show me where I'm wrong. > > ================================= > > > ============ > =========== > =========== > =========== > =========== > > > > ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Interconnection
Date: Dec 05, 201
Robert L. Nuckolls, III wrote: > > Sheesh! How many new joints and connectors would this add to all the wires? *** Yeah you're right, Bob. In the case of aircraft wiring, less is definitely more. My main desire would be to facilitate troubleshooting anyway. How about a set of radio/instrument extender/breakout cables, fabricated at the same time that the panel was put together? Then kept in storage. - Jerry ________________________________________________________________________________
From: "Gary K" <flyink(at)efortress.com>
Subject: Re: Interconnection
Date: Dec 05, 2001
> How about a set of radio/instrument extender/breakout cables, fabricated > at the same time that the panel was put together? Then kept in storage. That's my approach. I'm using the AMP CPC connectors with the machined pins, I love these things. The connectors are only a few bucks and I bought extra so I can make a breakout cable and check signals coming out and also send stuff into the electronics to check and calibrate the system. I like it so far, nice and clean and "modular". Thru the firewall I have a 9-pin for "control" signals and a 28-pin for "sensors". On my PC box I have another 9-pin for power and control and a 28-pin connector for the data coming in. Connectors are sometimes unreliable but I like to be able to plug stuff in and out easily. For anything critical, I have either redundancy or single wires from source to destination. These connectors and pins with a nice crimper work very well and are a pleasure to work with. Wiring has been very easy so far. I just have a list of signals for each connector, then route and cut the wires, then crimp and snap them into the connector. I'm using the spiral wrap for harnesses and so far so good, I never thought it would be this easy. Gary K., fun with wiring ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: oil switch
Date: Dec 05, 2001
Rob, That's my thoughts too, but both switchs have no continuity at any lead. One switch is over 6 months old and the other I just received. I thought the old one was defective so I ordered another one last week when I ordered my coax. I just don's see how my "master left on" buzzer will work. Thanks and let me know what you determine. Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: <racker(at)rmci.net> Subject: Re: AeroElectric-List: oil switch > > Jerry, > > According to Bob's diagram > (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), there should be > continuity between leads "P" and "S" with no oil pressure (i.e. oil > pressure idiot light/buzzer circuit), and leads "P" and "I" with oil > pressure (i.e hobbs meter circuit). > > I'll check my switch tonight at home. > > Rob Acker (RV-6). > > > > > > > > The switch you are refering to is what I have. The switch has 3 > > connections. A common pole, a normally open pole, and a normally > > closed pole. When there is no pressure in the switch, I would think > > the common pole and the normally closed pole would make a complete > > circuit, but neither switch do. This confuses me. > > > > Thanks for the reply, > > Jerry Calvert > > Edmond Ok -6 > > ----- Original Message ----- > > From: <W4PPN(at)aol.com> > > To: > > Subject: Re: AeroElectric-List: oil switch > > > > > >> > >> Jerry they are supposed to close under pressure. When you have oil > > pressure > >> the switch closes and applies 12 Volts to a Hobbs meter and it starts > >> counting the time you have run the engine. > >> > >> Of course there are switches that are closed until you apply oil > >> pressure > > and > >> then they open. > >> > >> I bought one that does both so I can incorporate it into my system. > >> One > > side > >> will run the hobbs meter when I have oil pressure and the other side > >> will either turn a light on to let me know that the Master Switch is > >> still on after the engine has shut down, or I can hook it up to a > >> buzzer that will > > let > >> me know that the Master Sw is still on. > >> > >> Howard > >> 1/2 of an RV-8 project. > >> Mooresville, NC > >> > >> > >> > >> > > > > > > generous support! http://www.matronics.com/contribution > > direct advertising on the Matronics Forums. > > Engine: http://www.matronics.com/search > > Other Lists: http://www.matronics.com/emaillists > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Paul Messinger" <paulm(at)tenforward.com>
Subject: oil switch
Date: Dec 05, 2001
Before you give up try a light and 12V battery. Ohmmeters use very low voltage these days and might not break down any oxide. I had the same concern with a similar switch a few years ago and it ohm'ed open but worked fine with 12V and some current. Paul -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Jerry Calvert Subject: Re: AeroElectric-List: oil switch Rob, That's my thoughts too, but both switchs have no continuity at any lead. One switch is over 6 months old and the other I just received. I thought the old one was defective so I ordered another one last week when I ordered my coax. I just don's see how my "master left on" buzzer will work. Thanks and let me know what you determine. Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: <racker(at)rmci.net> Subject: Re: AeroElectric-List: oil switch > > Jerry, > > According to Bob's diagram > (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), there should be > continuity between leads "P" and "S" with no oil pressure (i.e. oil > pressure idiot light/buzzer circuit), and leads "P" and "I" with oil > pressure (i.e hobbs meter circuit). > > I'll check my switch tonight at home. > > Rob Acker (RV-6). > > > > > > > > The switch you are refering to is what I have. The switch has 3 > > connections. A common pole, a normally open pole, and a normally > > closed pole. When there is no pressure in the switch, I would think > > the common pole and the normally closed pole would make a complete > > circuit, but neither switch do. This confuses me. > > > > Thanks for the reply, > > Jerry Calvert > > Edmond Ok -6 > > ----- Original Message ----- > > From: <W4PPN(at)aol.com> > > To: > > Subject: Re: AeroElectric-List: oil switch > > > > > >> > >> Jerry they are supposed to close under pressure. When you have oil > > pressure > >> the switch closes and applies 12 Volts to a Hobbs meter and it starts > >> counting the time you have run the engine. > >> > >> Of course there are switches that are closed until you apply oil > >> pressure > > and > >> then they open. > >> > >> I bought one that does both so I can incorporate it into my system. > >> One > > side > >> will run the hobbs meter when I have oil pressure and the other side > >> will either turn a light on to let me know that the Master Switch is > >> still on after the engine has shut down, or I can hook it up to a > >> buzzer that will > > let > >> me know that the Master Sw is still on. > >> > >> Howard > >> 1/2 of an RV-8 project. > >> Mooresville, NC > >> > >> > >> > >> > > > > > > generous support! http://www.matronics.com/contribution > > direct advertising on the Matronics Forums. > > Engine: http://www.matronics.com/search > > Other Lists: http://www.matronics.com/emaillists > > http://www.matronics.com/browselist/aeroelectric-list > > http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: oil switch
Date: Dec 05, 2001
Paul, I will give it a try and post the results. Thanks, Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: Paul Messinger <paulm(at)tenforward.com> Subject: RE: AeroElectric-List: oil switch > > Before you give up try a light and 12V battery. Ohmmeters use very low > voltage these days and might not break down any oxide. I had the same > concern with a similar switch a few years ago and it ohm'ed open but worked > fine with 12V and some current. > > Paul > > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Jerry > Calvert > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: oil switch > > > > Rob, > > That's my thoughts too, but both switchs have no continuity at any lead. > One switch is over 6 months old and the other I just received. I thought > the old one was defective so I ordered another one last week when I ordered > my coax. > I just don's see how my "master left on" buzzer will work. > > Thanks and let me know what you determine. > > Jerry Calvert > Edmond Ok -6 > ----- Original Message ----- > From: <racker(at)rmci.net> > To: > Subject: Re: AeroElectric-List: oil switch > > > > > > Jerry, > > > > According to Bob's diagram > > (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), there should be > > continuity between leads "P" and "S" with no oil pressure (i.e. oil > > pressure idiot light/buzzer circuit), and leads "P" and "I" with oil > > pressure (i.e hobbs meter circuit). > > > > I'll check my switch tonight at home. > > > > Rob Acker (RV-6). > > > > > > > > > > > > > The switch you are refering to is what I have. The switch has 3 > > > connections. A common pole, a normally open pole, and a normally > > > closed pole. When there is no pressure in the switch, I would think > > > the common pole and the normally closed pole would make a complete > > > circuit, but neither switch do. This confuses me. > > > > > > Thanks for the reply, > > > Jerry Calvert > > > Edmond Ok -6 > > > ----- Original Message ----- > > > From: <W4PPN(at)aol.com> > > > To: > > > Subject: Re: AeroElectric-List: oil switch > > > > > > > > >> > > >> Jerry they are supposed to close under pressure. When you have oil > > > pressure > > >> the switch closes and applies 12 Volts to a Hobbs meter and it starts > > >> counting the time you have run the engine. > > >> > > >> Of course there are switches that are closed until you apply oil > > >> pressure > > > and > > >> then they open. > > >> > > >> I bought one that does both so I can incorporate it into my system. > > >> One > > > side > > >> will run the hobbs meter when I have oil pressure and the other side > > >> will either turn a light on to let me know that the Master Switch is > > >> still on after the engine has shut down, or I can hook it up to a > > >> buzzer that will > > > let > > >> me know that the Master Sw is still on. > > >> > > >> Howard > > >> 1/2 of an RV-8 project. > > >> Mooresville, NC > > >> > > >> > > >> > > >> > > > > > > > > > generous support! http://www.matronics.com/contribution > > > direct advertising on the Matronics Forums. > > > Engine: http://www.matronics.com/search > > > Other Lists: http://www.matronics.com/emaillists > > > > > > > > > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Oil Switch problem resolved!
Date: Dec 05, 2001
Paul Messinger suggested testing the oil switch continuity with a light and 12v battery. The ohm meter doesn't have enough voltage to get through the slight oxidation on the contacts. This suggestion wins the prize! The 12v testing method proves that the normally closed contact is definately closed in the natural state. Thanks Paul. Jerry Calvert Edmond Ok -6 ________________________________________________________________________________
From: "dave ford" <dford(at)michweb.net>
Subject: fuse link
Date: Dec 05, 2001
Bob, Your drawings show from the main bus to the master switch alternator side a fusible link then routing through a circuit breaker to the alternator field. Is the double protection necessary or is the fusible link suggested as an option? Dave Ford RV6 ________________________________________________________________________________
From: "Rob A" <racker(at)rmci.net>
Subject: oil switch
Date: Dec 05, 2001
Jerry, My switch ohm'ed out correctly. No idea what's up with *both* of yours...sure you have the right pins you are trying to measure (P to S continuity, P to I no continuity w/o pressure)? Rob. > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Jerry > Calvert > Sent: Wednesday, December 05, 2001 4:39 PM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: oil switch > > > > > Rob, > > That's my thoughts too, but both switchs have no continuity at any lead. > One switch is over 6 months old and the other I just received. I thought > the old one was defective so I ordered another one last week when > I ordered > my coax. > I just don's see how my "master left on" buzzer will work. > > Thanks and let me know what you determine. > > Jerry Calvert > Edmond Ok -6 > ----- Original Message ----- > From: <racker(at)rmci.net> > To: > Subject: Re: AeroElectric-List: oil switch > > > > > > Jerry, > > > > According to Bob's diagram > > (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), > there should be > > continuity between leads "P" and "S" with no oil pressure (i.e. oil > > pressure idiot light/buzzer circuit), and leads "P" and "I" with oil > > pressure (i.e hobbs meter circuit). > > > > I'll check my switch tonight at home. > > > > Rob Acker (RV-6). > ________________________________________________________________________________
Date: Dec 06, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: fuse link
> > Bob, > >Your drawings show from the main bus to the master switch alternator >side a fusible link then routing through a circuit breaker to the >alternator field. Is the double protection necessary or is the fusible >link suggested as an option? > >Dave Ford >RV6 protection for a wire needs to be AT THE BUS. If you're using a fuseblock mounted away from the panel, then there's an unprotected wire that runs from the main bus up to the DC MASTER and ALT FIELD circuit breaker. Using a fusible link at the bus takes care of the short wire, the c/b takes care of the ov protection and downstream wiring. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: oil switch
Date: Dec 06, 2001
Rob, I checked again with a 12v battery and light. I checks out Ok now. My ohm meter isn't putting out enough power to get through the oxidation on the contacts. Thanks for checking it out. Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: Rob A <racker(at)rmci.net> Subject: RE: AeroElectric-List: oil switch > > Jerry, > > My switch ohm'ed out correctly. No idea what's up with *both* of > yours...sure you have the right pins you are trying to measure (P to S > continuity, P to I no continuity w/o pressure)? > > Rob. > > > -----Original Message----- > > From: owner-aeroelectric-list-server(at)matronics.com > > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Jerry > > Calvert > > Sent: Wednesday, December 05, 2001 4:39 PM > > To: aeroelectric-list(at)matronics.com > > Subject: Re: AeroElectric-List: oil switch > > > > > > > > > > Rob, > > > > That's my thoughts too, but both switchs have no continuity at any lead. > > One switch is over 6 months old and the other I just received. I thought > > the old one was defective so I ordered another one last week when > > I ordered > > my coax. > > I just don's see how my "master left on" buzzer will work. > > > > Thanks and let me know what you determine. > > > > Jerry Calvert > > Edmond Ok -6 > > ----- Original Message ----- > > From: <racker(at)rmci.net> > > To: > > Subject: Re: AeroElectric-List: oil switch > > > > > > > > > > Jerry, > > > > > > According to Bob's diagram > > > (http://www.aeroelectric.com/Catalog/switch/oilpwarn.pdf), > > there should be > > > continuity between leads "P" and "S" with no oil pressure (i.e. oil > > > pressure idiot light/buzzer circuit), and leads "P" and "I" with oil > > > pressure (i.e hobbs meter circuit). > > > > > > I'll check my switch tonight at home. > > > > > > Rob Acker (RV-6). > > > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Gary K" <flyink(at)efortress.com>
Subject: ig/fp switches
Date: Dec 06, 2001
I'm hoping to get some opinions on the layout of switches for my panel. I have a Stratus subaru with dual fuel pumps, dual ignition and dual batteries. I have a starter switch that has an accessory contact that I plan on using for the primary fuel pump and ignition, and a master toggle for the main battery and alternator. So the start procedure would be flip up master and turn the key to start. For the backup pump and ignition (for takeoff/landing and primary system failure), I am planning on having one of these options; - one off/on/on toggle to switch on the pump, then pump and ig on using the backup battery (simplest) - two off/on/on toggles, one each for the pump and ig, switching between off, main battery and backup battery (most flexible) - two on/off switches, one each for the pump and ig to switch off/on from the backup battery. - break out the primary pump and ignition from the starter switch and have separate switches for each (real messy but then maybe a push button starter) I know it's hard enough to build your own system, much less take an interest in someone else's, but there's a lot of experienced builders and pilots here that can provide some valuable opinions. I guess it's mostly preference anyway but I was having last minute thoughts before installing. Thanks for any comments, Gary K. ________________________________________________________________________________
Date: Dec 06, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Interconnection
> >Robert L. Nuckolls, III wrote: >> >> Sheesh! How many new joints and connectors would this add to all the wires? > >*** Yeah you're right, Bob. In the case of aircraft wiring, less is >definitely more. My main desire would be to facilitate troubleshooting >anyway. > > How about a set of radio/instrument extender/breakout cables, fabricated >at the same time that the panel was put together? Then kept in storage. Extension cables, and "breakout" boxes are most valuable tools for technicians. I have my own set of harnesses with mating connectors and intermediate panel boxes with tip jacks that sample every wire through the harness. Got tired of trying to chase down common tools at RAC and built my own. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 06, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Dry Cell Batteries
>Hi Bob, > >I would like to know your opinion on dry cell rechargeable batteries that some guys are putting in their aircraft in place of the regular wet cell or RC batteries. Aircraft Spruce and Van's sell them. > >Thanks, > >Mike Hepperlen These are STILL RG batteries . . . they're playing on words a tad to make them appear different. The Odyssey battery is an excellent RG product from Hawker . . . they've been enhanced for deep discharge service (not particularly important to airplane folks). See: http://www.odysseyfactory.com/ Bob . . . ________________________________________________________________________________
From: "Paul Messinger" <paulm(at)tenforward.com>
Subject: Oil Switch problem resolved!
Date: Dec 06, 2001
TX. This list has helped me many times, glad to be of help. Paul -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Jerry Calvert Subject: AeroElectric-List: Oil Switch problem resolved! Paul Messinger suggested testing the oil switch continuity with a light and 12v battery. The ohm meter doesn't have enough voltage to get through the slight oxidation on the contacts. This suggestion wins the prize! The 12v testing method proves that the normally closed contact is definately closed in the natural state. Thanks Paul. Jerry Calvert Edmond Ok -6 http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
Date: Dec 06, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Interconnection
> >How about a J-box that interconnected everything with a printed circuit >board and connectors that soldered directly to the board and poked out >through the box? > >David Swartzendruber >Wichita Hi Dave, long time no see. What's been going on with your new job? Actually, we DID a sort of j-box approach to an audio panel and some other functions that escape memory. On the single engine Cessnas about 1968 we built etched circuit boards with fingers to accept AMP twin-leaf connectors. I think it had connectors on all four edges and accepted harnesses from what was then a pretty busy, full stack of radios. It was abandoned some years later . . . the connector technology of the time against our ECB tabs proved less than desirable after a few years in the field. I'm sure a machined pin, d-sub would have been a better choice . . . but you and I both know Cessna's product design philosophy well . . . don't spend a penny more than you HAVE to . . . that penny-pinching bit us more than once. I'm not sure but I think we elected not to gold plate the ECB fingers . . . NOT a good idea. Bob . . . ________________________________________________________________________________
From: "Ed Perry" <eperry(at)san.rr.com>
Subject: Inline Fuse Rating
Date: Dec 07, 2001
Hi Bob, 3 things..... 1) first I am now experiencing the problem with the master & starter contactors having nuts that are too big. If you have any of the 5/16" nuts and star washers laying around, say 4 of each I would be happy to reimburse you for them. If you are interested I'll send you my address..... 2) If I understand your Figure Z1, I am going to route the B lead from the alternator to the battery side of the Starter contactor. I am running a 35 amp alternator supplied by Van's and I have a few 50 circuit breakers laying around, will this be enough to protect the 4awg wire? Or should I go with a heavier inline fuse? If the fuse what amp? 3) I am looking at my ACS ignition switch. On the back are the connectors for the MAGs, starter,etc. They look like little loops but are not threaded. What sort of connector do I use here, or is this a place for, gulp, SOLDER? As Always Thank You, Ed Perry eperry(at)san.rr.com ________________________________________________________________________________
Date: Dec 09, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Inline Fuse Rating
> >Hi Bob, > >3 things..... > >1) first I am now experiencing the problem with the master & starter >contactors having nuts that are too big. If you have any of the 5/16" >nuts and star washers laying around, say 4 of each I would be happy to >reimburse you for them. If you are interested I'll send you my >address..... By too big I presume you mean too thick. I need to know if the contactors have 5/16-24 or 5/16-18 thread. I can send you a hardware set with thin nuts and washers. Also, we had a discussion some time back about adding a starter-engaged light to your starter contactor. If the contactor you have is anything like the ones we sell, the two small terminals are not the same size. The "S" terminal will be 8-32 thread and this wire goes to your starter switch. The "I" terminal will be 6-32 . . . this is the terminal that gets and inline fuse or fusible link and connects to your STARTER ENGAGED annunicator. >2) If I understand your Figure Z1, I am going to route the B lead from >the alternator to the battery side of the Starter contactor. I am >running a 35 amp alternator supplied by Van's and I have a few 50 >circuit breakers >laying around, will this be enough to protect the 4awg wire? Or should I >go with a heavier inline fuse? If the fuse what amp? No, the 50A breaker is fine. Mount it on a bracked close to the starter contactor. >3) I am looking at my ACS ignition switch. On the back are the >connectors for the MAGs, starter,etc. They look like little loops but >are not threaded. What sort of connector do I use here, or is this a >place for, gulp, SOLDER? Is this an ACS-510 switch or something different? I've never seen an ignition switch with solder lugs. Are the tabs flat and thick enough that they COULD be threaded? I'm wondering if they missed the threading step in manufacturing. Did the switch come with a bag of screws and lockwashers not installed on the switch? Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 09, 2001
From: Andy <winterland(at)rkymtnhi.com>
Subject: electrical gurus
Anyone here (Bob?) want to tackle an electronics project? What I'd like to have (I bet a lot of people would) is a device which can respond to a remote signal, perhaps like a touch tone cell phone signal, to turn on and off the electric engine pre-heater. In other words, I wanna get up at 6:00 AM, see that its a good morning to fly, call the pre-heater on the phone, and tell it to turn itself on. Then, when I get to the airport a couple hours later, everything is warm and happy and ready to fire up. So far, I've found 2 possible ways to do this, but each has limitations: 1] There is a device sold by Radio Shack and others called the X-10 controller which does exactly this and will in fact control up to 10 independent circuits. (push 1 for your plane, push 2 for your hangarmates plane, 3 for the guy next door, and so on) The problem is that it requires standard phone lines in the hangar which we don't have. (Bringing them in would cost several thousand dollars) 2] There is another device sold by Bob Reiff (the heater guy) called the beeper box. You tape a telephone pager to it. The device listens for the sound of the beeper beeping and then the sound activates a switch which turns on the heater. This eliminates the phone line but Bob's box is quite pricey (almost $400), requires a seperate beeper and beeper service account, and will only handle a single circuit. Is there such thing as an X-10 type device that will work off a cell phone, or other radio type signal, instead of regular telephone land lines. Or, anybody know how to make one? Andy ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 09, 2001
Subject: Re: Starter Engaged Confusion
In a message dated 12/9/2001 10:37:23 AM Eastern Standard Time, nuckolls(at)aeroelectric.com writes: > Also, we had a discussion some time back about adding > a starter-engaged light to your starter contactor. If the > contactor you have is anything like the ones we sell, the > two small terminals are not the same size. The "S" terminal > will be 8-32 thread and this wire goes to your starter > switch. The "I" terminal will be 6-32 . . . this is the > terminal that gets and inline fuse or fusible link and > connects to your STARTER ENGAGED annunicator. > Hey everyone ! I had to say "hold everything here" when I saw this . My confusion on this is directed to Bob : Is'nt one of the potential failure modes of the start contactor to fail (welded contacts) in the closed position ? This would result in the starter being engaged when there is actually no voltage present at the "I" terminal & hence no illumination of the Starter Engaged annunciator . This is the major reason I thought I wanted the annunciator . Otherwise I know the starter is engaged if the prop is turning ! It seems to me that the pic-up point for the annunciator should be the high current terminal that gets power when the heavy contacts are closed . I realise the voltage ( for a 12 v sys) would be maybe 6 or 8 v during cranking so a lower rated annunciator lamp rating might be needed but @ least then I would know to turn off my batt master B4 my starter self destructs . Please clarify . Chris ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 09, 2001
Subject: Re: electrical gurus
In a message dated 12/9/2001 1:10:03 PM Eastern Standard Time, winterland(at)rkymtnhi.com writes: > Is there such thing as an X-10 type device that will work off a cell phone, > or other radio type > signal, instead of regular telephone land lines. Or, anybody know how to > make one? > > Andy > GEEEEZ Andy , you should head to the pattent office w/ this one . I know I'd love to have that . You better hurry though cause you got me thinking of persuing this . . . Can't wait to hear from Bob on this . Chris. ________________________________________________________________________________
Date: Dec 09, 2001
From: Vern Smith <vismith(at)sympatico.ca>
Subject: Re: electrical gurus
Hi Andy..it is possible to use a radio signal..have a receiver at your hangar, connected to a touch tone decoder (DTMF) to control almost anything you want..an old aircraft receiver will work, depending on the distance involved..as VHF is pretty much line of sight, and the range on the ground even with a good antenna may only be 4 or 5 miles depending on how powerful your transmitter is..I,ve used this type of system for turning on runway lights, etc..Radio Shack has a touch tone module which can be plugged into your mic jack with built in push to talk..Hams use them for repeater use, etc. Vern Smith Andy wrote: > > Anyone here (Bob?) want to tackle an electronics project? > > What I'd like to have (I bet a lot of people would) is a device which can respond to a remote > signal, perhaps like a touch tone cell phone signal, to turn on and off the electric engine > pre-heater. > > In other words, I wanna get up at 6:00 AM, see that its a good morning to fly, call the pre-heater > on the phone, and tell it to turn itself on. Then, when I get to the airport a couple hours > later, everything is warm and happy and ready to fire up. > > So far, I've found 2 possible ways to do this, but each has limitations: > > 1] There is a device sold by Radio Shack and others called the X-10 controller which does exactly > this and will in fact control up to 10 independent circuits. (push 1 for your plane, push 2 for > your hangarmates plane, 3 for the guy next door, and so on) The problem is that it requires > standard phone lines in the hangar which we don't have. (Bringing them in would cost several > thousand dollars) > > 2] There is another device sold by Bob Reiff (the heater guy) called the beeper box. You tape a > telephone pager to it. The device listens for the sound of the beeper beeping and then the sound > activates a switch which turns on the heater. This eliminates the phone line but Bob's box is > quite pricey (almost $400), requires a seperate beeper and beeper service account, and will only > handle a single circuit. > > Is there such thing as an X-10 type device that will work off a cell phone, or other radio type > signal, instead of regular telephone land lines. Or, anybody know how to make one? > > Andy > ________________________________________________________________________________
Date: Dec 09, 2001
From: Andy <winterland(at)rkymtnhi.com>
Subject: Re: electrical gurus
> Unfortunately we don't have line of sight to the airport. I'm about 8 miles away but on the side of a hill facing the wrong way. Andy > Hi Andy..it is possible to use a radio signal..have a receiver at your hangar, connected to a touch > tone decoder (DTMF) to control almost anything you want..an old aircraft receiver will work, > depending on the distance involved..as VHF is pretty much line of sight, and the range on the ground > even with a good antenna may only be 4 or 5 miles depending on how powerful your transmitter is.. ________________________________________________________________________________
Date: Dec 09, 2001
From: Vern Smith <vismith(at)sympatico.ca>
Subject: Re: electrical gurus
Have you considered using a CB hookup with a good directional antenna at each end..have sent data this way..Vern Andy wrote: > > > > > Unfortunately we don't have line of sight to the airport. I'm about 8 miles away but on the side of a > hill facing the wrong way. > > Andy > > > Hi Andy..it is possible to use a radio signal..have a receiver at your hangar, connected to a touch > > tone decoder (DTMF) to control almost anything you want..an old aircraft receiver will work, > > depending on the distance involved..as VHF is pretty much line of sight, and the range on the ground > > even with a good antenna may only be 4 or 5 miles depending on how powerful your transmitter is.. > ________________________________________________________________________________
Date: Dec 09, 2001
From: Jim and Lucy <jpollard(at)mnsi.net>
Subject: Re: electrical gurus
Buy a cell phone and a clapper. The cell phone ringing will activate a clapper. Have the clapper activate a circuit that locks the heater on for 3 hours. Works on tv anyway :) Jim Pollard ch601hds ea81 ________________________________________________________________________________
Date: Dec 09, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Starter Engaged Confusion
> >In a message dated 12/9/2001 10:37:23 AM Eastern Standard Time, >nuckolls(at)aeroelectric.com writes: > > >> Also, we had a discussion some time back about adding >> a starter-engaged light to your starter contactor. If the >> contactor you have is anything like the ones we sell, the >> two small terminals are not the same size. The "S" terminal >> will be 8-32 thread and this wire goes to your starter >> switch. The "I" terminal will be 6-32 . . . this is the >> terminal that gets and inline fuse or fusible link and >> connects to your STARTER ENGAGED annunicator. >> > > >Hey everyone ! I had to say "hold everything here" when I saw this . My >confusion on this is directed to Bob : Is'nt one of the potential failure >modes of the start contactor to fail (welded contacts) in the closed position >? This would result in the starter being engaged when there is actually no >voltage present at the "I" terminal & hence no illumination of the Starter >Engaged annunciator . This is the major reason I thought I wanted the >annunciator . Otherwise I know the starter is engaged if the prop is turning >! It seems to me that the pic-up point for the annunciator should be the high >current terminal that gets power when the heavy contacts are closed . I >realise the voltage ( for a 12 v sys) would be maybe 6 or 8 v during cranking >so a lower rated annunciator lamp rating might be needed but @ least then I >would know to turn off my batt master B4 my starter self destructs . Please >clarify . Chris When you take one of these contactors apart and study the way the main terminal contacts are bridged to engage the starter, the "I" terminal has to be closed too . . . the moveable contact inside is like a three-legged stool. Most 12v lamps are entirely adequate to the task for annunciation - especially if you are watching for the light to go out when you release the start button. Bob . . . ________________________________________________________________________________
Date: Dec 10, 2001
From: John Rourke <john@allied-computer.com>
Subject: Re: Starter Engaged Confusion
So... is there anything wrong with putting the indicator light on the starter side contact? Especially if it were an LED, which would draw an insignificant amount of current away from the starter (with dropping resistor of course)? -John "Robert L. Nuckolls, III" wrote: > > > > > >In a message dated 12/9/2001 10:37:23 AM Eastern Standard Time, > >nuckolls(at)aeroelectric.com writes: > > > > > >> Also, we had a discussion some time back about adding > >> a starter-engaged light to your starter contactor. If the > >> contactor you have is anything like the ones we sell, the > >> two small terminals are not the same size. The "S" terminal > >> will be 8-32 thread and this wire goes to your starter > >> switch. The "I" terminal will be 6-32 . . . this is the > >> terminal that gets and inline fuse or fusible link and > >> connects to your STARTER ENGAGED annunicator. > >> > > > > > >Hey everyone ! I had to say "hold everything here" when I saw this . My > >confusion on this is directed to Bob : Is'nt one of the potential failure > >modes of the start contactor to fail (welded contacts) in the closed position > >? This would result in the starter being engaged when there is actually no > >voltage present at the "I" terminal & hence no illumination of the Starter > >Engaged annunciator . This is the major reason I thought I wanted the > >annunciator . Otherwise I know the starter is engaged if the prop is turning > >! It seems to me that the pic-up point for the annunciator should be the high > >current terminal that gets power when the heavy contacts are closed . I > >realise the voltage ( for a 12 v sys) would be maybe 6 or 8 v during cranking > >so a lower rated annunciator lamp rating might be needed but @ least then I > >would know to turn off my batt master B4 my starter self destructs . Please > >clarify . Chris > > When you take one of these contactors apart and study the > way the main terminal contacts are bridged to engage the starter, > the "I" terminal has to be closed too . . . the moveable contact > inside is like a three-legged stool. > > Most 12v lamps are entirely adequate to the task for annunciation - > especially if you are watching for the light to go out when > you release the start button. > > Bob . . . > ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Remore telephone control
Date: Dec 09, 2001
Andy: You want an old Amateur Radio licensee. Remote control of radio repeaters is 50 years old - all done by tone control on the telephone patch. If done by audio (as in Babysitter), ANY sound which contains the control tone turns on your preheater - a locomotive whistle, scvreeching tires, etc. Avoid this by using CTCSS tones (double ones like on you touchtone phone) and the control circuit comes from the 'ham'. Don't go for those expensive commercial control circuit units. Details on request. Ferg Europa A064 ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 10, 2001
Subject: Re: Starter Engaged Confusion
In a message dated 12/10/2001 12:58:47 AM Eastern Standard Time, nuckolls(at)aeroelectric.com writes: > When you take one of these contactors apart and study the > way the main terminal contacts are bridged to engage the starter, > the "I" terminal has to be closed too . . . the moveable contact > inside is like a three-legged stool. > > Most 12v lamps are entirely adequate to the task for annunciation - > especially if you are watching for the light to go out when > you release the start button. > > Bob . . . > OK ,Thanks Bob , That sound sgreat ! Chris . Do Not Archive ! ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Remore telephone control
Date: Dec 10, 201
Fergus Kyle wrote: > > > Andy: > You want an old Amateur Radio licensee. Remote control of radio > repeaters is 50 years old - all done by tone control on the telephone patch. > If done by audio (as in Babysitter), ANY sound which contains the control > tone turns on your preheater - a locomotive whistle, scvreeching tires, etc. > Avoid this by using CTCSS tones (double ones like on you touchtone phone) > and the control circuit comes from the 'ham'. *** There are chips available that implement the entire tone decode function. You put audio in one end, and at the other end, the "three" wire pulses when you a tone encoded "three" comes in. - Jerry Kaidor, KF6VB ( jerry(at)tr2.com ) ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Remote radio control precautions
Date: Dec 09, 2001
Cheers, there have been a number of suggestions regarding Gary's request for info on how to remotely start a preheater. There are wyas to do it, and ways not to. One way not to, is to send an audio signal over the air by whatever radio frequency that can be monitored by the 'cranks'. If they think you're doing something interesting, they'll tape the tone, and send it on the same frequency later. You may not want that. The safest way is still by wired telephone (and that may not be "cellphone" which is just a radio, but they call it 'wireless' to avoid the radiating thought), since few are monitoring this mode. That's why some of these suggestions require the advice of someone who has the experience to have safely (and legally) done it before. Bob will know this. Good Luck, Ferg Europa A064 ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Remote radio control precautions
Date: Dec 10, 201
Fergus Kyle wrote: > > > Cheers, > there have been a number of suggestions regarding Gary's request > for info on how to remotely start a preheater. There are wyas to do it, and > ways not to. > One way not to, is to send an audio signal over the air by > whatever radio frequency that can be monitored by the 'cranks'. If they > think you're doing something interesting, they'll tape the tone, and send it > on the same frequency later. You may not want that. *** If you got fancy, you could have a little computer sitting on the phone line ( or radio ) and use some sort of encrypted request-response protocol. But that's getting into the "kill a gnat with a sledgehammer" territory. > > The safest way is still by wired telephone (and that may not be > "cellphone" which is just a radio, but they call it 'wireless' to avoid the > radiating thought), since few are monitoring this mode. *** "PCS" or "digital" cellphones are probably reasonably secure. If you listen to their freq with a scanner, I think you just hear noise. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 10, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Remote control of hangar equipment
> >Anyone here (Bob?) want to tackle an electronics project? > >What I'd like to have (I bet a lot of people would) is a device which can respond to a remote >signal, perhaps like a touch tone cell phone signal, to turn on and off the electric engine >pre-heater. > >In other words, I wanna get up at 6:00 AM, see that its a good morning to fly, call the pre-heater >on the phone, and tell it to turn itself on. Then, when I get to the airport a couple hours >later, everything is warm and happy and ready to fire up. > >So far, I've found 2 possible ways to do this, but each has limitations: > >1] There is a device sold by Radio Shack and others called the X-10 controller which does exactly >this and will in fact control up to 10 independent circuits. (push 1 for your plane, push 2 for >your hangarmates plane, 3 for the guy next door, and so on) The problem is that it requires >standard phone lines in the hangar which we don't have. (Bringing them in would cost several >thousand dollars) > >2] There is another device sold by Bob Reiff (the heater guy) called the beeper box. You tape a >telephone pager to it. The device listens for the sound of the beeper beeping and then the sound >activates a switch which turns on the heater. This eliminates the phone line but Bob's box is >quite pricey (almost $400), requires a seperate beeper and beeper service account, and will only >handle a single circuit. the pager is the easiest and least expensive way to go. The controls are easy, getting a good link is the hard part. Easiest links are via phone line. Next easiest is via radio of some kind but if you want to stay "legal" you need to have some licensed service to carry your commands . . . things like CB radio, cell phones, pagers and amateur radio have all been used successfully. Amateur radio repeater stations are generally located on very tall facilities so that their line of sight range can be extensive. I was president the Air Capitol Amateur Repeater Association when we formed up the club and acquired a spot 1200 feet up on a television tower in Hutchinson, KS. http://209.134.106.21/ktvh.jpg Those are the toes of my boots at the bottom of the frame. I took the picture looking down the center of the tower from the 1200 foot platform. From this kind of height, relatively low power, line of sight communications and control are possible over a wide area. The repeater we installed on that platform would perform well with a two-watt handheld transceiver 45 miles away in Wichita. It's not too difficult to get an amateur radio operators license that would let you access one or more local repeaters. You need to memorize some stuff and take a relatively slow code test (5 wpm). All you need then is a receiver decoder on the remote site and a touchtone pad on any transmitter fitted to talk to that repeater. Since you don't need a lot of variable frequency performance or other features, relatively cheap transceivers can be had from Ebay and similar services. The transceiver at: http://cgi.ebay.com/aw-cgi/eBayISAPI.dll?ViewItem&item=1306799707 is going to sell for peanuts. I built a remote control system that worked through a local repeater for another application about 10 years ago. Bought a couple of crystal controlled transceivers for about $20 each as I recall. Rigged an off the shelf touch tone controller to the remote receiver. The customer was able to control several different functions over 90 miles away and get a confirming reply from the remote site. Of course this is all hung out on a relatively public facility and subject to mischief by others who might try to figure out how your system works. It's relatively easy to make it secure even on an open service like a shared repeater. Nowadays, I would use a Basic-Stamp micro-controller running an algorithm against a time of day clock to constantly change the control codes. Not heavy duty security but difficult to crack since you would use it very infrequently. Even if someone observed and decoded your commands, it's unlikely that they would get more than a few samples a month to work with. One could acquire and assemble the total package for under 100 dollars. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 10, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Starter Engaged Confusion
> >So... is there anything wrong with putting the indicator light on the >starter side contact? Especially if it were an LED, which would draw an >insignificant amount of current away from the starter (with dropping >resistor of course)? > >-John that would work too . . . Bob . . . ________________________________________________________________________________
Date: Dec 11, 2001
From: Matt Dralle <dralle(at)matronics.com>
Subject: New Photo Share Main Index Page - The Detail You Asked
For... Hi Listers! I've been noticing a lot of people having fun with the new Email List Photo and File Share feature and I've seen a great many hits on the various member pages. A number of you wrote to say that some additional topic data on the Main Photo Share Index page would certainly be helpful and I would have to agree. It took a little programming, and it was a job retrofitting to all of the older Shares, but I think you'll be pleased with the outcome! I've added Poster Name, Photo Share Subject, and Target Email List data to the Main Index. Clicking on a Subject text opens a new window with the Photo Share and the thumbnails. Have a look and feel free to submit your photos for sharing! The instructions are at the top of the Main Photo Share Index Page. The URL is: http://www.matronics.com/photoshare Enjoy!! Matt Dralle Email List Admin. ________________________________________________________________________________
From: "ED KOWALSKI" <salned(at)msn.com>
Subject: MP-3 Player
Date: Dec 11, 2001
Right now I have a sony AM/FM Sterio CD player installed in our RV-8 and am thinking of going to an MP-3 player instead. Can they be tied into the Audio Panel (Garmin 340 )? Do you recomend any specific unit? Thanks!!!!!!!!............Ed Ed Kowalski, Wilmington Il. RV-8.......... S.N. #80127 N127EK Getting ready to Fly ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Remote control of hangar equipment
Date: Dec 11, 201
Robert L. Nuckolls, III wrote: > > > Of course this is all hung out on a relatively public facility > and subject to mischief by others who might try to figure out how > your system works. It's relatively easy to make it secure > even on an open service like a shared repeater. Nowadays, I > would use a Basic-Stamp micro-controller running an algorithm > against a time of day clock to constantly change the control > codes. *** Would the FCC interpret this as "codes & ciphers"? Or are those OK now? ( I haven't kept track over the last few years... ) - Jerry Kaidor, KF6VB ________________________________________________________________________________
Date: Dec 11, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Remote control of hangar equipment
> >Robert L. Nuckolls, III wrote: >> >> >> Of course this is all hung out on a relatively public facility >> and subject to mischief by others who might try to figure out how >> your system works. It's relatively easy to make it secure >> even on an open service like a shared repeater. Nowadays, I >> would use a Basic-Stamp micro-controller running an algorithm >> against a time of day clock to constantly change the control >> codes. > >*** Would the FCC interpret this as "codes & ciphers"? Or are those >OK now? ( I haven't kept track over the last few years... ) > > - Jerry Kaidor, KF6VB ANY bureaucrat could pick up on that rule and make an issue of it . . . the codes and ciphers rule has been around I believe since day-one and its apparent intent was to restrict communications to plain languages. Obviously, one could have legally used some obscure foreign dialect and still be "legal" . . . this task is more of a remote control activity that does not convey intelligence from one person to another and would (in my not so humble opinion) come under the jurisdiction of the rule. . . but this day and age (and while dealing with government) you never know. BOB, K0DYH ________________________________________________________________________________
Date: Dec 12, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: A conversation about shielding
>By the way, my whole understanding of the purpose of using shielded wire >may be faulty. I thought it was that GPS is very noise-sensitive and >therefore one would like to keep radiated energy in the vicinity as low as >possible. I just assumed that every unshielded conductor acts like a little >antenna broadcasting whatever goes through it, and that its signal would be >a problem for the GPS even several feet away. Is the only problem actually >between wires that run in close proximity to one another for some distance? >I am in fact running all my radio-related wiring in separate bundles. Shielded wire has almost no beneficial effects for controlling "radiation" . . . shielding breaks up the CAPACITIVE coupling of fast rise-time voltages between adjacent conductors in airplanes that use airframe ground for the primary power return. In composite airplanes, where the ground must accompany the supply wire to remote loads, there is a small benefit to be gained to reduce MAGNETIC coupling of current variation noise between adjacent conductors by using the shield as a ground return. This absolutely forces concentric equal and opposite magnetic fields around the wire to cancel each other. Similarly, magnetic fields from other antagonists couple equally into both conductors with electrical effects nulled out at the ends of the conductor. You can get 90% of the SAME effect by bundling inbound and outbound conductors together in parallel bundles and 99% of the same effect by twisting them together (about 1 turn per inch). If you have the tools, skill and materials to deal comfortably with shielded wire for this application, it's not a bad thing to do . . . but the benefits over other techniques don't justify the effort if you're having to spend a lot of time on it -OR- if there are any concerns for operational integrity due to hassles of the special techniques involved. Most problems with MAGNETIC radiation involve the whisky compass or alternator whine coupled into audio systems. >Now that I think about it, people use GPS in all kinds of environments. Is >noise really that big a problem? And does noise really mean what I thought >it means -- eg a signal emanating from an unshielded DC conductor running >to, say, a light bulb? No, GPS is 1500 MHz . . . far above the range of system generated noises in your airplane. The strongest potential antagonist to GPS comes from harmonics of local oscillators in your VHF receivers falling on or near the GPS receiving frequencies . . . and this has been rare in practice. Most cases of poor GPS performance can be traced to antenna problems . . .poor design or location on the aircraft. Except for the minor benefits I've described above, the use of shielded wire in light aircraft is generally limited to P-leads, strobe-head-to-power-supply leads (both fast risetime voltages), and to avionics wiring where the installation instructions call out shielded wire. The biggest noise reduction comes from use of single point grounding (in both metal and plastic airplanes) described in my book. >You see, once you start ignorant people thinking, you cause all kinds of >mischief. No, just an opportunity to spread the words of understanding. Knowledge is one of the few commodities who's value goes up because it is shared with the maximum number of interested parties. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Remote control of hangar equipment
Date: Dec 12, 201
Robert L. Nuckolls, III wrote: > *** How about an "invisible" cipher? Let's say you have a code that you use to turn on the thingie. It consists of N CTCSS digits. The digits are always the same. HOWEVER, the digit-to-digit times vary with respect to the date, the time of day, the phase of the moon, whatever. Wrong times = no worko. - Jerry Kaidor ( jerry(at)tr2.com ) > >> against a time of day clock to constantly change the control > >> codes. > > > >*** Would the FCC interpret this as "codes & ciphers"? Or are those > >OK now? ( I haven't kept track over the last few years... ) > > > > - Jerry Kaidor, KF6VB > > ANY bureaucrat could pick up on that rule and make an > issue of it . . . the codes and ciphers rule has been > around I believe since day-one and its apparent intent was > to restrict communications to plain languages. Obviously, > one could have legally used some obscure foreign dialect > and still be "legal" . . . this task is more of a remote > control activity that does not convey intelligence from > one person to another and would (in my not so humble > opinion) come under the jurisdiction of the rule. . . > but this day and age (and while dealing with government) > you never know. > > BOB, K0DYH > > > > > > ________________________________________________________________________________
From: "Ross Mickey" <rmickey(at)ix.netcom.com>
Subject: Re: MP-3 Player
Date: Dec 12, 2001
----- Original Message ----- From: "ED KOWALSKI" <salned(at)msn.com> > Right now I have a sony AM/FM Sterio CD player installed in our RV-8 and > am thinking of going to an MP-3 player instead. Can they be tied into th> e Audio Panel (Garmin 340 )? Do you recomend any specific unit? Thanks> !!!!!!!!............Ed Ed, I see that you didn't get many public responses to your question. I am going to get an MP3 for my RV-6A. It will just plug into the SL15 Apollo audio panel. There are a few formats to choose from and just like building an airplane, mission is the key. MP3 players come in many sizes and formats. The four basic are the CD, minidisk, flash memory and hard drive. The flash memory are the smallest and least prone to skipping but tend to hold the smallest amount. The CD format allows you to burn MP3 CD's and is the largest. The hard drive hold the most (6-20mb) but are heavy and are just portable hard drives. I am leaning towards the Creative Nomad 32 on board. This has 32 kb flash memory and accepts 128kb SmartMedia cards. It is small, light and should hold 10 hours of music. If you want to carry your whole CD library with you, I would go with the Archos Nomad 20mb. This all assumes you are PC not Mac based. Ross ________________________________________________________________________________
Subject: MP-3 Player
Date: Dec 12, 2001
From: "David Glauser" <david.glauser(at)xpsystems.com>
> -----Original Message----- > From: Ross Mickey [mailto:rmickey(at)ix.netcom.com] > Sent: Wednesday, December 12, 2001 09:57 > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: MP-3 Player > > ... I am leaning towards the Creative Nomad 32 on > board. This has 32 kb flash memory and accepts 128kb > SmartMedia cards. It > is small, light and should hold 10 hours of music. If you > want to carry > your whole CD library with you, I would go with the Archos > Nomad 20mb. This > all assumes you are PC not Mac based. > > Ross Other disk-based systems to check out are the Neo Jukebox, available with drives up to 40GB, and the Neo Car Jukebox, available with 40GB and 60GB drives and already built to handle vibration. If you're a Mac type, there;s the iPod. The Nomad is actually made by Creative Labs, and Archos has a product called the Jukebox, available in several configurations. Search on Google for "Archos Jukebox", "Creative Labs Nomad", and "Jeo Jukebox". If you like to roll your own, there are several open-source and/or DIY MP3 player projects out there. I personally plan to install the Neo Car Jukebox in my Europa, and carry my entire 600+ CD music collection along. What the heck - the extra bits don't weigh all that much. David ________________________________________________________________________________
From: "Miles McCallum" <milesm(at)avnet.co.uk>
Subject: Re: A conversation about shielding
Date: Dec 12, 2001
----- Original Message ----- > > In composite airplanes, where the ground must accompany the supply > wire to remote loads, there is a small benefit to be gained to reduce > MAGNETIC coupling of current variation noise between adjacent > conductors by using the shield as a ground return. This absolutely > forces concentric equal and opposite magnetic fields around the > wire to cancel each other. Similarly, magnetic fields from other > antagonists couple equally into both conductors with electrical > effects nulled out at the ends of the conductor. > > You can get 90% of the SAME effect by bundling inbound and outbound > conductors together in parallel bundles and 99% of the same effect > by twisting them together (about 1 turn per inch). Interesting....My micromonitor manual calls for the majority of sensors to be connected by twisted pair inside a sheild. Does this mean I can substitute a pair of shielded wires without penalty? I thought the explanation very clear and understandable: I got 100%, 100% of the time in the electrics module tests when I did my A&P. Certainly doesn't mean I understood it (Once it gets beyond the "water in pipes" analogy, it's over my head) but I've learned more on this site (and via the aeroelectric connection) than I thought possible. What's more, it's interesting. Does this mean I'm turning into a geek? all the best Miles ________________________________________________________________________________
Date: Dec 12, 2001
From: Michael Hartmann <hartmann(at)sound.net>
Subject: Re: MP-3 Player
>----- Original Message ----- >> Right now I have a sony AM/FM Sterio CD player installed in our RV-8 and >> am thinking of going to an MP-3 player instead. Can they be tied into th>> e Audio Panel (Garmin 340 )? Do you recomend any specific unit? Thanks> > >an airplane, mission is the key. MP3 players come in many sizes and >formats. The four basic are the CD, minidisk, flash memory and hard drive. >The flash memory are the smallest and least prone to skipping but tend to >hold the smallest amount. The CD format allows you to burn MP3 CD's and is >the largest. The hard drive hold the most (6-20mb) but are heavy and are >just portable hard drives. I am leaning towards the Creative Nomad 32 on I don't have experience with the in-dash units, but have been using a portable Phillips Expanium EXP103 in my truck since early summer. I intend to install a panel-mount (dash-mount) mp3 player in my RV, but the EPX103 portable, fed into the aux music port of the intercom would definately be suitable. It has 100 second skip protection at 128Kbps, which is adequate. I haven't tried dropping it, but I've shaken it, rattled it, turn it upside down, and left it sitting on either the floor or dashboard of a truck bouncing down rough roads, and so far, it has never skipped. I've been using mp3s at home for a few years, and have one of my older desktops connected to the stereo as a dedicated mp3 'tape drive' for playing and recording them. I've converted all 300+ CDs in our collection to mp3s, and have started on the 500+ vinyl albums. In my opinion, 128Kbps is the optimum comprimise between quality and compression for every day use. The audio quality at the lower bitrates becomes objectionable; at the higher rates the sound improves, but only to a point, and with less compression. If you want CD quality, you're stuck with a CD. The audio quality of an mp3 at 128Kbps is as good or better than FM radio or the very best audio cassette. More than good enough in a noisy environment, even with good headsets. At 128Kbps you can expect your audio CDs to compress to about 10%. That is, roughly 10 audio CDs can be converted to 128Kbps mp3s and stored on a single data CD. The low end 32mb portables will not hold the music from even a single audio CD unless you go to a lower bit rate, making them fairly impractical. In the RV, I'd recommend a panel mounted in-dash unit for convenience, or a portable for economy and weight. A semi-permanent installation of a portable might be a good compromise. Or use a portable in conjunction with the current panel-mount stereo. The hard-drive based units are probably a little heavy for aircraft use, and having hundreds of hours of music on tap in an airplane that can get from Seattle to Key West in less than 20 seems like overkill. You will find reviews of several in-dash units online. The usual considerations of ease of use, clarity of display, etc that you would evaluate when choosing a unit for your car also apply when choosing one for your RV. You should also consider installed weight. Since you won't be installing speakers, power output is of no interest. Skip protection is important too. In my experience, 100 seconds is plenty. Less might even be enough. More would be better, everything else being equal. The mp3 format has been huge with computer geeks for years, but for reasons I don't understand, has been slow to catch on in the consumer audio market. The selection of players just continues to get better. You can find a reasonable selection of what is available now for cars (RVs) with specifications, and some reviews at: http://www.highwaymp3.com Another site that works pretty well for checking prices is: http://www.nextag.com/In_dash_MP3_CD~500122z3oz3kzmainz5-htm Good luck. - Mike hartmann(at)sound.net RV-6A in progress, N642MH (reserved) ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: MP-3 Player
Date: Dec 12, 201
*** I have a Casio E100 that's not doing much. I was thinking of making that into an in-plane MP3 player. With mono MP3's and a large Compact Flash card, it would hold a pretty reasonable number of songs. ( why mono? Rest of the plane is mono anyway, why waste the space? ) - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
From: Melvinke(at)aol.com
Date: Dec 12, 2001
Subject: Re: MP-3 Player
My Creative Nomad will not provide sufficient volume when pluged into the NAT intercom, through which a Walkman or Discman provide plenty of sound. When I interfaced the Nomad with a small amplifier, it locked up and had to be reset. In other words, the Nomad is no good for the purpose. ________________________________________________________________________________
From: "Phil Birkelbach" <phil(at)petrasoft.net>
Subject: Re: electrical gurus
Date: Dec 12, 2001
How about buying a little cheap pager with a vibrating motor. Take the thing apart and un-solder the motor and replace it with a relay. Put the pager in vibrate mode and you have a discrete signal to start some kind of timer that would run your heater for say two or three hours. If you really want to be fancy you could put a cellular phone near one of the touch tone decoders that have been discussed here and put the cell phone in auto-answer mode. Just dial the cell phone number when it answers punch in your code and there you have it. This would also give you a phone to use at the hanger as well as giving you the ability to control multiple devices and with a little creativity could give you some feedback, you could plug some noise maker into the same outlet with the heater and you can listen for the noise to make sure that it is working. You could also set this thing up to turn things off. Phil Birkelbach RV-7 - N727WB (Reserved) - Wings - Fuse ordered Houston, Texas http://www.myrv7.com Takeoffs are optional, Landings are mandatory. ----- Original Message ----- From: "Andy" <winterland(at)rkymtnhi.com> Subject: AeroElectric-List: electrical gurus > > Anyone here (Bob?) want to tackle an electronics project? > > What I'd like to have (I bet a lot of people would) is a device which can respond to a remote > signal, perhaps like a touch tone cell phone signal, to turn on and off the electric engine > pre-heater. > > In other words, I wanna get up at 6:00 AM, see that its a good morning to fly, call the pre-heater > on the phone, and tell it to turn itself on. Then, when I get to the airport a couple hours > later, everything is warm and happy and ready to fire up. > > So far, I've found 2 possible ways to do this, but each has limitations: > > 1] There is a device sold by Radio Shack and others called the X-10 controller which does exactly > this and will in fact control up to 10 independent circuits. (push 1 for your plane, push 2 for > your hangarmates plane, 3 for the guy next door, and so on) The problem is that it requires > standard phone lines in the hangar which we don't have. (Bringing them in would cost several > thousand dollars) > > 2] There is another device sold by Bob Reiff (the heater guy) called the beeper box. You tape a > telephone pager to it. The device listens for the sound of the beeper beeping and then the sound > activates a switch which turns on the heater. This eliminates the phone line but Bob's box is > quite pricey (almost $400), requires a seperate beeper and beeper service account, and will only > handle a single circuit. > > Is there such thing as an X-10 type device that will work off a cell phone, or other radio type > signal, instead of regular telephone land lines. Or, anybody know how to make one? > > Andy > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Randy Lervold" <randy@rv-8.com>
Subject: Re: MP-3 Player
Date: Dec 12, 2001
You will find the problem with many intercoms including the PS Engineering PM3000 that I have. It is because the entertaiment circuit is fed into the audio stream *before* the intercom volume control and is therefore attenuated. I bought a Boostaroo, a little battery powered linear amplifier that provides 12 db of boost, which helped, but still didn't solve the problem to my satisfaction. Consequently I'm presently building a whole new panel (for several reasons) into which I'm installing a PS Engerring PCD7100. This has it's own volume control for the music that is blended into the audio stream *after* the main voice volume control. Doesn't play MP3s, but store a small CD wallet in the cockpit should be no problem. Randy Lervold RV-8, 140 hrs. www.rv-8.com > My Creative Nomad will not provide sufficient volume when pluged into the NAT > intercom, through which a Walkman or Discman provide plenty of sound. When I > interfaced the Nomad with a small amplifier, it locked up and had to be > reset. In other words, the Nomad is no good for the purpose. ________________________________________________________________________________
Date: Dec 13, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: A conversation about shielding
> > >----- Original Message ----- >> >> In composite airplanes, where the ground must accompany the supply >> wire to remote loads, there is a small benefit to be gained to reduce >> MAGNETIC coupling of current variation noise between adjacent >> conductors by using the shield as a ground return. This absolutely >> forces concentric equal and opposite magnetic fields around the >> wire to cancel each other. Similarly, magnetic fields from other >> antagonists couple equally into both conductors with electrical >> effects nulled out at the ends of the conductor. >> >> You can get 90% of the SAME effect by bundling inbound and outbound >> conductors together in parallel bundles and 99% of the same effect >> by twisting them together (about 1 turn per inch). > >Interesting....My micromonitor manual calls for the majority of sensors to >be connected by twisted pair inside a sheild. Does this mean I can >substitute a pair of shielded wires without penalty? No, when a manufacturer calls out specific wiring techniques for their product, they should be observed. What you've suggested is probably true but one should give the designers a benefit of the doubt . . . perhaps they're aware of some vulnerability that is to readily apparent. On the other side of the coin, we should observe that adding shielding to a wire protects the system from a very narrow spectrum of antagonistic stresses which are also rare throughout the average system . . . there is no value in shielding-every- wire-just-to-be-safe . . . I've had a couple of builders do this and they added many pounds, dollars and hours to their projects without adding operational value. >I thought the explanation very clear and understandable: I got 100%, 100% of >the time in the electrics module tests when I did my A&P. Certainly doesn't >mean I understood it (Once it gets beyond the "water in pipes" analogy, it's >over my head) but I've learned more on this site (and via the aeroelectric >connection) than I thought possible. What's more, it's interesting. Does >this mean I'm turning into a geek? I sincerely hope so. There are many factions in our society who champion a variety of causes to rid us of one kind of evil or another . . . may I suggest that mankind's greatest threat in any venue comes from ignorance and lack of understanding? Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
From: "Russ Werner" <russ(at)maui.net>
Subject: Ground wire from aft mounted battery
Date: Dec 13, 2001
Aeroelectriceers, I am working on the aft fuselage in a Harmon Rocket II (modified RV4, aft battery) and have closely followed Bob's wiring strategy. I spoke with someone who wired the ground side a bit different and it seems to work well and save quite a few lbs. I'm interested in possible downsides on this method. Instead of running an additional 2awg wire from the Battery Negative terminal to the engine, run a short length to the nearby 1/8" aluminum longeron (running the full length of the airplane). At the forward end, run a braid or wire to a firewall/engine mount bolt and from there to a ground block for the panel. On the engine side of that same firewall/engine mount bolt, run a braid to the engine case. This will save many feet of 2awg wire. Also, can the main positive lead from the master contactor be routed to an insulated stud on the firewall rather than having the wire go through to the starter contactor or is that too many connections? Thanks, Russ Werner Maui HRII ________________________________________________________________________________
Subject: Avionics 101
Date: Dec 14, 2001
From: "Mike Gray" <mgray(at)graymatter.org>
Can any of the good folks out there tell me if there is a book on avionics - particularly interconnection and protocols etc. - that is similar in scope to the Bob's AeroElectric bible? Mike Gray ________________________________________________________________________________
From: "ED KOWALSKI" <salned(at)msn.com>
Subject: MP-3 Player
Date: Dec 14, 2001
Thanks to all that responded. You've been a great help and given me plenty to look into. Thanks Again...Ed Ed Kowalski, Wilmington Il. RV-8.......... S.N. #80127 N127EK Getting ready to Fly ________________________________________________________________________________
Date: Dec 14, 2001
From: "Builder's Bookstore" <winterland(at)rkymtnhi.com>
Subject: Re: Avionics 101
Mike Gray wrote: > > Can any of the good folks out there tell me if there is a book on > avionics - particularly interconnection and protocols etc. - that is > similar in scope to the Bob's AeroElectric bible? > Try Avionics Troubleshooting & Repair by Eric Mahler. Aside from the title, this book is really more of an installation guide than anything else, as it goes by the premise that most avionics problems are actually installation issues and, among other things, shows you how to check and perfect those connections. You can see a more detailed description in the Electrical and Panel section of Builder's Bookstore Andy Builder's Bookstore http://www.buildersbooks.com ________________________________________________________________________________
From: JusCash(at)aol.com
Date: Dec 14, 2001
Subject: Vans MP Gauge/Radio Interference
Hello Listers, I am having a problem with my Vans manifold pressure gauge and the electric trim indicator. When I key the transmitter the Vans manifold pressure gauge loses pressure using the Narco MK12D and gains pressure with the Garmin GNC250XL.=A0 Also the trim indicator will move from neutral to full nose up when I key the Garmin.=A0 The Narco does not effect it.=A0 I have tried every thing I could think of to isolate this problem, nothing seems to work.=A0 I am hoping someone else has experienced this problem and came up with a solution.=A0 I have used the Electrical Connection techniques faithfully throughout the wiring process.=A0 Maybe I missed something!!!!!!!!!!!!! Cash Copeland RV6 N46FC To the airport when I solve this problem ________________________________________________________________________________
From: "Randy Lervold" <randy@rv-8.com>
Subject: Re: Vans MP Gauge/Radio Interference
Date: Dec 14, 2001
This isn't help, just consolation. My Van's MAP gauge gains pressure when I xmit (UPSAT SL40). I've learned to live with it though as you really don't spend that much time transmitting. If anyone has a solution I'd be interested though. Randy Lervold RV-8, N558RL, 140.5 hrs. www.rv-8.com > I am having a problem with my Vans manifold pressure gauge and the electric > trim indicator. > When I key the transmitter the Vans manifold pressure gauge loses pressure > using the Narco MK12D and gains pressure with the Garmin GNC250XL.=A0 Also t> he > trim indicator will move from neutral to full nose up when I key the Garmin.> > The Narco does not effect it.=A0 > I have tried every thing I could think of to isolate this problem, nothing > seems to work.=A0 I am hoping someone else has experienced this problem and > came up with a solution.=A0 > I have used the Electrical Connection techniques faithfully throughout the > wiring process.=A0 Maybe I missed something!!!!!!!!!!!!! > > Cash Copeland > RV6 N46FC > To the airport when I solve this problem ________________________________________________________________________________
Date: Dec 16, 2001
From: Matt Dralle <dralle(at)matronics.com>
Subject: [ PLEASE READ ] : Matronics Network Upgrade Mon. 12/17/01
Listers, According to my ISP, Speakeasy, they will be doing some sort of "backbone upgrade" Monday, 12/17/01. Their message doesn't mention whether or not this will impact connectivity for any length of time. I wanted everyone to know that there might be a time when access to the Matronics Web Server and Email Lists might be unavailable. If there's a problem, I'll post a message from a different email address with details. Bottom line: Hopefully nobody will notice... Best regards, Matt Dralle Matronics Email List Admin. Matt G Dralle | Matronics | PO Box 347 | Livermore | CA | 94551 925-606-1001 V | 925-606-6281 F | dralle(at)matronics.com Email http://www.matronics.com/ WWW | Featuring Products For Aircraft ________________________________________________________________________________
Date: Dec 17, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Connecting a wire to a BNC connector
OK, crayon-level time (in case you can't tell)... Any special considerations in soldering a wire to a BNC connector? I'm building an RV-6 with capacative senders. How do I solder the doggone thing without melting the guts of the connector? Any types of soldering guns that are more suited to this than others? And what type of solder should I use? Told ya these were crayon-level :-) Semper Fi John RV-6 (fuel tank for left wing) ________________________________________________________________________________
From: "Ken Mattsson" <ken.mattsson(at)helsinki.fi>
Subject: battery solenoid + diode
Date: Dec 17, 2001
Hi everybody! This is my first post to this mail list, so if Im off topic please tell me so. Im reading Tony Bingelis Firewall Forward book, currently the chapter on electrical systems. On one wiring schematic for a complete electrical system there is a diode connected over the battery solenoid. It is connected from the relay connector to the primary plus of the solenoid, allowing current flow in that direction. What is this diode used for? Some kind of radio interference antimeasure? Ken Finland ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: Connecting a wire to a BNC connector
Date: Dec 17, 2001
Heat the end of the wire and coat it with some good electical solder(I use radioshack 63/37). Push the wire in the BNC hole and use a fine tip solder iron and heat the area where the wire sticks in and touch solder to it and it will wick up in there. Doesn't take long. Use proseal and completely coat the BNC on the inside of the tank so it won't leak fuel. Also, coat the wire were it comes out of the BNC for about 1 1/2" up the wire. This helps support the wire better from vibration. You're next BNC challenge will be figuring out how to connect the sender converter modules coming from the guage to the BNC you just installed! Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: John Lawson <jwlawson(at)hargray.com> Subject: AeroElectric-List: Connecting a wire to a BNC connector > > OK, crayon-level time (in case you can't tell)... > > Any special considerations in soldering a wire to a BNC connector? I'm building an RV-6 > with capacative senders. How do I solder the doggone thing without melting the guts of > the connector? Any types of soldering guns that are more suited to this than others? > And what type of solder should I use? > > Told ya these were crayon-level :-) > > Semper Fi > John > RV-6 (fuel tank for left wing) > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
Date: Dec 17, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: battery solenoid + diode
> >Hi everybody! > >This is my first post to this mail list, so if Im off topic please tell me so. > >Im reading Tony Bingelis Firewall Forward book, currently the chapter on electrical systems. On one wiring schematic for a complete electrical system there is a diode connected over the battery solenoid. It is connected from the relay connector to the primary plus of the solenoid, allowing current flow in that direction. > >What is this diode used for? Some kind of radio interference antimeasure? Go to http://www.aeroelectric.com and click on link to Article Reprints and Newsgroup Treads. On the next page, find and click on "An illustrated discussion about spike catching diodes and how they work." You may find a bunch of other goodies on this page worth reading as well. Bob . . . ________________________________________________________________________________
Date: Dec 17, 2001
From: John Rourke <john@allied-computer.com>
Subject: Re: battery solenoid + diode
This is a common trick, necessary for any coil that is turned on and off. When you turn on the circuit, a magnetic field builds up in the relay's coil. When you turn it off, the magnetic field collapses. Any moving magnetic field (even collapsing ones) induces a voltage in any wire in its path. The collapsing magnetic field crosses the many wires in the relay's coil and induces a large voltage spike in them, in the opposite direction of the voltage that created the magnetic field in the first place. The diode is there to "clamp" any such reverse voltage spike. -John Ken Mattsson wrote: > > > Hi everybody! > > This is my first post to this mail list, so if Im off topic please tell me so. > > Im reading Tony Bingelis Firewall Forward book, currently the chapter on electrical systems. On one wiring schematic for a complete electrical system there is a diode connected over the battery solenoid. It is connected from the relay connector to the primary plus of the solenoid, allowing current flow in that direction. > > What is this diode used for? Some kind of radio interference antimeasure? > > Ken > Finland > ________________________________________________________________________________
Subject: King radio.
From: "Terry Lamp" <tlamp(at)genesishcs.org>
Date: Dec 17, 2001
12/17/2001 09:55:28 AM If anyone is interested in a yellow tagged King KY 197 A Comm radio, please email privately Thanks Terry Long EZ Ohio ________________________________________________________________________________
Date: Dec 17, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Connecting a wire to a BNC connector
> >OK, crayon-level time (in case you can't tell)... > >Any special considerations in soldering a wire to a BNC connector? I'm building an RV-6 >with capacative senders. How do I solder the doggone thing without melting the guts of >the connector? Any types of soldering guns that are more suited to this than others? >And what type of solder should I use? > >Told ya these were crayon-level :-) First, what kind of wire is intended to receive the BNC connector? Is it a coaxial cable like RG-58, RG-142 or RG-400? If the wire is a common coaxial cable used in radio antenna systems, consider crimping the connector on. See: http://209.134.106.21/articles/bnccrimp.pdf and . . . http://209.134.106.21/articles/coaxconn/coaxconn.html If the connectors are unique to some special kind of coaxial cable and crimped connectors are NOT an option, then you've got your work cut out for you if you don't have some spare connectors and wire on which to practice. If you don't have experience with this operation, I suggest you find someone in your neighborhood that does. An electronic technician with a two-way radio company would be a good bet. You need to get some spare wire and connectors to train on . . . I wouldn't recommend that anyone fly the first soldered BNC connector that was part of their Soldering 101 curriculum. If you're forced to use the solder type connector then slip the clamping nut, washer and gasket over the trimmed end of the coax before you being to strip it. Strip insulations and outer conductor to the dimensions on the installation instructions for the type of connector you are using. If the center conductor is stranded wire, then "tin" the ends of exposed strands with just enough solder to stick the ends of the strands together. This operation is intended to immobilize the strands with respect to each other and has nothing to do with the integrity of the final soldered joint. Fill the solder cup of connector's center pin with a piece of .032" diameter wire solder. Just cut a piece of solder long enough to be totally contained inside the pin's wire opening. Put coax in vise with end sticking out horizontally, hold pin with needle nose pliers and apply heat to body of pin while holding pin poised over end of coax center conductor. As the solder inside melts, slip the pin down over the wire. When the joint cools, you can finish the connectors assembly by adding the outer conductor clamp ring, trimming the outer conductor so that the ends of the strands project no more than 1/16th of inch beyond the clamp surface and then push the body of the connector down over the prepared ends. Use a thin 7/16" wrench to gain a purchase on the connector body's wrench flats and another 7/16" wrench to snug the clamp nut down into the rear of the connector. In 1961, solder type BNCs was all we had. Got to work on hundreds of these things early on in my career. When affordable tools and crimp products came onto the scene, it wasn't hard to convince me that I needed to add solderless BNC capability to my toolbox! Bob . . . ________________________________________________________________________________
Date: Dec 17, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Ground wire from aft mounted battery
> >Aeroelectriceers, > >I am working on the aft fuselage in a Harmon Rocket II (modified RV4, aft >battery) and have closely followed Bob's wiring strategy. I spoke with >someone who wired the ground side a bit different and it seems to work well >and save quite a few lbs. I'm interested in possible downsides on this >method. > >Instead of running an additional 2awg wire from the Battery Negative >terminal to the engine, run a short length to the nearby 1/8" aluminum >longeron (running the full length of the airplane). At the forward end, run >a braid or wire to a firewall/engine mount bolt and from there to a ground >block for the panel. On the engine side of that same firewall/engine mount >bolt, run a braid to the engine case. This will save many feet of 2awg >wire. The scheme you describe has been used successfully in one form or another on thousands of airplanes. I wouldn't worry about a jumper from structure to the ground block at the front end of the longeron. How much is "many feet" of 2AWG wire? 2AWG wire weighs about 4 oz per foot . . . so a run of less than 12 feet will be under three pounds. Not perhaps a compelling weight difference but something to consider in your deliberations for weight reduction versus system performance. >Also, can the main positive lead from the master contactor be routed to an >insulated stud on the firewall rather than having the wire go through to the >starter contactor or is that too many connections. Insulated feed-through studs are a practical way to bring high quality, heavy current conductors through the firewall and maintain good electrical insulation for the penetration. HOWEVER, use only brass hardware and plan to cover the firewall side of the device with fire-putty . . . there isn't a speedshop feed-through out there that's truly qualified for firewall service on aircraft. Bob . . . ________________________________________________________________________________
Date: Dec 17, 2001
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: Connecting a wire to a BNC connector
John Lawson wrote: > > > OK, crayon-level time (in case you can't tell)... > > Any special considerations in soldering a wire to a BNC connector? I'm building an RV-6 > with capacative senders. How do I solder the doggone thing without melting the guts of > the connector? Any types of soldering guns that are more suited to this than others? > And what type of solder should I use? > > Told ya these were crayon-level :-) > > Semper Fi > John > RV-6 (fuel tank for left wing) > John, 'Gun' usually implies too much heat & power for small connectors. You can buy a pencil style iron & the proper electronics grade solder at Radio Shack or other electronics supply house for less than $10. Grind the tip to a longer, round point. 'Tin' the hot tip with solder. Keep a damp rag or sponge handy to clean the tip while working. (Pro's just use their blue jeans. You can tell a pro by the linear scars on his thighs from forgetting that he was wearing shorts.) With the wire prepared & after test fitting in the connector, wipe the hot iron's tip on the sponge, re-tin the tip with a very small amount of solder (this aids heat transfer; the black looking corrosion which forms on the tip actually insulates the tip). Now 'tin' the bare wire end with a *small* amount of solder & recheck its fit in the connector. Clean the iron on the sponge again, re-tin the iron with a *small* amount of solder, & apply heat to the connector, if possible. Quickly start touching your solder to the point where the wire & connector meet. The solder should flow into the joint between the wire & the connector. Note that you don't heat the solder with the iron, you heat the connector & let it heat the solder. This insures that everything got hot enough to make a proper joint. If it takes longer than about 2 seconds to actually heat the connector & flow the solder into the joint, something is wrong; stop & analyze the problem. The technique is very similar to 'sweating' a joint in copper pipe, except that you cannot use the same solder (no acid flux allowed for electronic work) & things happen much faster. Charlie Slobovia Outernational Airport RV-4 (sold) ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Connecting a wire to a BNC connector
Date: Dec 17, 201
John Lawson wrote: > > > OK, crayon-level time (in case you can't tell)... > > Any special considerations in soldering a wire to a BNC connector? *** This is a very well designed connector. All you solder is the center pin. You slide the nut, rubber gasket, & washer onto the coax, trim the end of the coax as appropriate, and solder the little tiny all-metal center pin onto the coax. Then you push the rest of the connector onto the coax over the center pin, and tighten the nut. Piece O'cake. See AC43-13 or the Amateur Radio Handbook for precise instructions. Use ordinary rosin-core radio solder. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
From: "Jim Robinson" <jbr(at)hitechnetworks.net>
Date: Dec 17, 2001
Subject: Re: Starter Engaged Confusion
Bob What difference is there in Fig Z-4 and new Fig Z-14. I cannot see any difference. There may not be any, but I am using Z-4 and wanted to make sure. Jim ________________________________________________________________________________
Date: Dec 17, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Starter Engaged Confusion
> >Bob > >What difference is there in Fig Z-4 and new Fig Z-14. I cannot >see any difference. There may not be any, but I am using Z-4 and >wanted to make sure. > >Jim There was a major correction to the diodes used on the crossfeed contactor. Wired per figure Z-4 and the system won't work right. Bob . . . ________________________________________________________________________________
Date: Dec 17, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Basic tool kit for dealing with electrical "things"
Hokay, another crayon-level question for the assembled multitudes... I'm building an RV-6 (2/3 finished with the first - left - wing). I'm going to put a wing leveler or single-axis autopilot (maybe two-axis, if I can afford it) and equip it for basic IFR. I'm putting electric elevator and aileron trim on it. I'm a novice when it comes to things electrical...that's why I bought 'The Aero-Electric Connection' :-) I'm getting ready to start doing some "things electric"...what would you folks suggest I purchase in the way of tools and supplies in order to do a good job of building the airplane and maintaining it? I'm not D. Trump (no one...well, ok...most people don't get rich in guvmint service), so I don't have a ton of $$, but I do believe firmly that good-quality tools pay for themselves many, many times over, both in terms of the quality of the work and in resale value...same goes for materials, in terms of doing a job that won't have to be done over again. I had a lot of good suggestions from folks on the RV-list about buying sheet metal tools, and I'm looking for the same from the 'trons in the house. Any suggestions on what I should get, and where? Are there any "starter" tool kits available that are worth looking at? (I told you I was at crayon level!). Semper Fi John RV-6 (left wing) ________________________________________________________________________________
From: " theslumlord" <theslumlord(at)mediaone.net>
Subject: fuse on the buss wire?
Date: Dec 17, 2001
Bob- I understand the need to protect the Alt B lead at the battery [protection is given to the wire to keep the battery from becoming an arc welder if the wire shorts] why isn't the lead from the batt contactor to the buss similarly protected? Ralph Bookout, Certified Slumlord RV6 finishing ________________________________________________________________________________
From: "Jim Robinson" <jbr(at)hitechnetworks.net>
Date: Dec 17, 2001
Subject: Re: fig z-4
Thanks Bob I will discard Z-4 and use Z-14. Thanks again for all your great help! Jim ________________________________________________________________________________
From: "Jim Robinson" <jbr(at)hitechnetworks.net>
Date: Dec 17, 2001
Subject: Re: fig Z-4
Bob I just compared my fig z-4 (rev 8/01) and can see no difference in the diodes or there direction. I'm I missing something? I spoke(emailed) to soon before I had a chance to check the drawings. Jim ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: Basic tool kit for dealing with electrical "things"
Date: Dec 17, 2001
John, I purchased the terminal crimper and BNC crimping tool from 'lectric Bob's associates at B&C Specialties. You may not need the BNC crimper, but the terminal crimper is a must. I went Home Depot and bought a wire stripper made by Ideal. I believe they call it an automatic stripper. Squeeze the handle and it grips the wire and cuts the insulation and pulls it off in one swoop. Also, some small wire cutters were purchased at Home Depot. Also picked up some pin crimpers for the sub connectors at Radio Shack. I haven't noticed a kit with all the right tools. I would start with the terminal crimpers, wire strippers, and wire cutters for total layout of about $55. Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: John Lawson <jwlawson(at)hargray.com> Subject: AeroElectric-List: Basic tool kit for dealing with electrical "things" > > Hokay, another crayon-level question for the assembled multitudes... > > I'm building an RV-6 (2/3 finished with the first - left - wing). I'm going to put a > wing leveler or single-axis autopilot (maybe two-axis, if I can afford it) and equip it > for basic IFR. I'm putting electric elevator and aileron trim on it. > > I'm a novice when it comes to things electrical...that's why I bought 'The Aero-Electric > Connection' :-) I'm getting ready to start doing some "things electric"...what would you > folks suggest I purchase in the way of tools and supplies in order to do a good job of > building the airplane and maintaining it? I'm not D. Trump (no one...well, ok...most > people don't get rich in guvmint service), so I don't have a ton of $$, but I do believe > firmly that good-quality tools pay for themselves many, many times over, both in terms of > the quality of the work and in resale value...same goes for materials, in terms of doing > a job that won't have to be done over again. > > I had a lot of good suggestions from folks on the RV-list about buying sheet metal tools, > and I'm looking for the same from the 'trons in the house. Any suggestions on what I > should get, and where? Are there any "starter" tool kits available that are worth > looking at? (I told you I was at crayon level!). > > Semper Fi > John > RV-6 (left wing) > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
Date: Dec 18, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Re: Connecting a wire to a BNC connector
> From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> > Subject: AeroElectric-List: Re: Connecting a wire to a BNC connector > > > > > >OK, crayon-level time (in case you can't tell)... > > > >Any special considerations in soldering a wire to a BNC connector? I'm building an RV-6 > >with capacative senders. How do I solder the doggone thing without melting the guts of > >the connector? Any types of soldering guns that are more suited to this than others? > >And what type of solder should I use? > > > >Told ya these were crayon-level :-) > > First, what kind of wire is intended to receive the BNC connector? > Is it a coaxial cable like RG-58, RG-142 or RG-400? If the > wire is a common coaxial cable used in radio antenna systems, > consider crimping the connector on. See: > > http://209.134.106.21/articles/bnccrimp.pdf > > and . . . > > http://209.134.106.21/articles/coaxconn/coaxconn.html > Ah, drat...I should have told you what kind of BNC connector, I didn't realize there were coax BNC connectors also...the plans show it as an "AV BNC 31-236-RFX BNC Bulkhead Terminal." It has one verrrrrry little socket for a wire (18 AWG, I think). > > If the connectors are unique to some special kind of > coaxial cable and crimped connectors are NOT an option, > then you've got your work cut out for you if you don't > have some spare connectors and wire on which to practice. > > If you don't have experience with this operation, I > suggest you find someone in your neighborhood that does. > An electronic technician with a two-way radio company > would be a good bet. > > You need to get some spare wire and connectors to train > on . . . I wouldn't recommend that anyone fly the > first soldered BNC connector that was part of their > Soldering 101 curriculum. > Good idea...I'm headed to Radio Shack today to get the necessary instructional materials :-) > If you're forced to use the solder type connector then > slip the clamping nut, washer and gasket over the trimmed > end of the coax before you being to strip it. > > Strip insulations and outer conductor to the dimensions > on the installation instructions for the type of connector > you are using. If the center conductor is stranded wire, > then "tin" the ends of exposed strands with just enough > solder to stick the ends of the strands together. This > operation is intended to immobilize the strands with > respect to each other and has nothing to do with the > integrity of the final soldered joint. > > Fill the solder cup of connector's center pin with a > piece of .032" diameter wire solder. Just cut a piece > of solder long enough to be totally contained inside > the pin's wire opening. > > Put coax in vise with end sticking out horizontally, > hold pin with needle nose pliers and apply heat to body > of pin while holding pin poised over end of coax center > conductor. As the solder inside melts, slip the pin down > over the wire. > > When the joint cools, you can finish the connectors > assembly by adding the outer conductor clamp ring, > trimming the outer conductor so that the ends of the > strands project no more than 1/16th of inch beyond > the clamp surface and then push the body of the connector > down over the prepared ends. > > Use a thin 7/16" wrench to gain a purchase on the > connector body's wrench flats and another 7/16" > wrench to snug the clamp nut down into the rear of > the connector. > > In 1961, solder type BNCs was all we had. Got to > work on hundreds of these things early on in my career. > When affordable tools and crimp products came onto the > scene, it wasn't hard to convince me that I needed to > add solderless BNC capability to my toolbox! > Thanks to you, Bob, and to the others who responded, much appreciated! :-) I'm headed to the Shack and to Home Depot to give myself some early Christmas presents. > *** This is a very well designed connector. All you solder is the center > pin. You slide the nut, rubber gasket, & washer onto the coax, trim the end > of the coax as appropriate, and solder the little tiny all-metal center pin > onto the coax. Then you push the rest of the connector onto the coax over > the center pin, and tighten the nut. Piece O'cake. See AC43-13 or the > Amateur Radio Handbook for precise instructions. Use ordinary rosin-core > radio solder. Hmmm...there wasn't a rubber gasket in the little bag that the connector came in (I just checked) - it does have a nut, a ring with a tab on it (tab has a hole in it), both of which I presume go onto the barrel of the connector...But on the plans I only see one wire leading to the end of the connector with the socket. ? Semper Fi John RV-6 (left wing tank) ________________________________________________________________________________
Date: Dec 18, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: fig Z-4
> >Bob > >I just compared my fig z-4 (rev 8/01) and can see no difference in >the diodes or there direction. I'm I missing something? >I spoke(emailed) to soon before I had a chance to check the >drawings. >Jim You apparently downloaded the corrected Z-4 in August (the original drawing was quite a lot older). Other than some changes to correct errors in notes, etc., the Z-4 you were working with was okay. Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 18, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: fuse on the bus wire?
> >Bob- I understand the need to protect the Alt B lead at the battery >[protection is given to the wire to keep the battery from becoming an arc >welder if the wire shorts] Actually, the greatest risk to that wire is from shorted diodes inside the alternator . . . for short runs of HEAVY wire, there is little risk of the wire itself getting shorted to ground. >why isn't the lead from the batt contactor to the buss similarly protected? For the same reason as cited above. The large feeders are not at much risk of shorting in a way that puts the wire in jeopardy. We go to extra pains on installation to support such conductors and minimize risks but they are already very small. There are hundreds of thousands of airplanes that have no "extra" protection of large power distribution feedlines. Bob . . . ________________________________________________________________________________
Date: Dec 18, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Dumb Questions
> >I purchased the Starter Contactor and the 20A Sealed Relay from your >website, but I'm unsure which terminals to use for both of these items (I >can figure that the big ones on the Intermittent Relay are form the battery >and to the starter, but does it matter which one is which?) Which one of >the little ones to use for the Starter Switch? The two large terminals of the starter contactor are interchangeable. These carry current from battery to starter motor when the button is pushed. The solenoid coil of the starter contactor is internally connected to the contactor's mounting base . . . so one connection to the coil is achieved via attachment to grounded, metallic structure. The "S" terminal is 10-32 thread and receives power to energize the contactor via the starter switch. The "I" terminal is 8-32 thread and is optionally used to supply power to a STARTER ENGAGED indicator light. Most builders ignore this terminal. > I have the same kind of >questions regarding the little relay as well. The two large tabs of the relay are interchangeable and are connected to the switching contacts inside the relay. The two small tabs are also interchangeable and supply power to the solenoid coil that will energize the relay. Bob . . . ________________________________________________________________________________
Date: Dec 18, 2001
From: Ed Holyoke <bicyclop(at)pacbell.net>
Subject: Microair transponders
Hey Bob, Did you ever get any Microair transponders? I've got a 2 1/4" hole that wants one and not much room in my radio stack. Ed Holyoke RV-6 QB ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Connecting a wire to a BNC connector
Date: Dec 18, 201
John Lawson wrote: > > Ah, drat...I should have told you what kind of BNC connector, I didn't > realize there were coax BNC connectors also...the plans show it as an "AV > BNC 31-236-RFX BNC Bulkhead Terminal." It has one verrrrrry little socket > for a wire (18 AWG, I think). > *** Normally, one connects to a bulkhead connector by stripping the end of the coax for about a half inch. You separate the braid and center into two "wires". Solder a small ring termainal onto the braid end. Solder the center conductor to the bulkhead connector. Terminate the braid by fastening the ring terminal with one of the screws holding the bulkhead connector. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 18, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Crimpers?
I looked on the B&C web site for crimpers as one lister suggested...no luck, doesn't look like they're selling them any more. I find about a millyun different types of crimpers (ok...well...mebbe not that many) on the Digi-Key web site...and I found one in the Aircraft Spruce catalog...any suggestions on which one I should buy? I'm crimping terminals for the capacitative fuel senders in the tank for my RV-6. Help! Lost in crimper land John RV-6 (left wing tank) ________________________________________________________________________________
From: BAKEROCB(at)aol.com
Date: Dec 18, 2001
Subject: spike catching diodes
In a message dated 12/18/2001 2:52:36 AM Eastern Standard Time, aeroelectric-list- writes: <<....skip.... Go to http://www.aeroelectric.com and click on link to Article Reprints and Newsgroup Treads. On the next page, find and click on "An illustrated discussion about spike catching diodes and how they work.".....skip..... >> 12/18/01 Hello Bob, Thanks for your testing and detailed write up on this subject. But I'm still left with some very simple layman's questions / doubts. The diagram on page 212 of Tony Bingelis' book Firewall Forward provides a basis for discussion / questions. 1) Does the diode always get installed so that it provides a connection between the solenoid switch terminal and some other part of the circuit? 2) Does it matter which other part of the circuit that the diode connection goes to? I see on Tony's diagram that the diode connection is made to the plus or input side of the relay. I see that on your sketch you show the diode connection going to ground. Which is correct / better? 3) When diagramming this diode connection which is the proper direction for the diode triangle to be pointing? I see on Tony's diagram that the diode triangle has the base connected to the solenoid switch terminal. I see on your sketch that you have the point of the diode triangle connected to the solenoid switch terminal (and the base of the triangle connected to ground). 4) When the switch has been closed for some time is there supposed to be any current flow through the diode? 5) Which way is the current from the collapsing coil field supposed to flow through the diode when the switch is opened? In the direction that the diode triangle is pointing or opposite to the direction the diode triangle is pointing? 6) When one has a diode in hand how can one tell by looking at its markings which end the triangle is pointing towards? Many thanks for your help. 'OC' Baker, Builder of KIS TR-1 #116 4/14/97 - ?/?/? ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Crimpers?
Date: Dec 18, 2001
John, I just finished wiring my entire plane (RV6, IFR). I used basically 3 different crimpers. Here's what I have. 1 pair (red) AMP 18-22 guage ratcheting crimpers. (EBAY) 1 pair (Blue)AMP 16-18 guage ratcheting crimpers. (EBAY) 1 pair of generic "snapon or channel-lock" multi crimpier/stripper I also have a BNC crimper from Radio Shack which is working quite well. I used my rivet squeezer with a home-made die to squeeze the #2 battery cables, and the #8 bus wire. Since I used cannon plugs in the firewall and subpanel, I have a cheap pair of Radio Shack pin crimpers for the TypeIII Cannon Plug pins. This crimper also worked for the molex pins (Narco) and the D-Sub pins for other connectors. You really don't need a huge selection, just make sure you get the basics. The one thing I would recommend spending decent money on is a good set of "ideal" wire strippers. These are the "automatic" kind that work all at once. WAYYYYY better than the cheap generic onces, especially with Tefzel. My total cost in Crimpers is under $75.00, but who's keeping track! I swear, this part of the plane is going to nickel and dime me to DEATH! Cheers, Stein Bruch RV6, Minneapolis, Cowling. .;.......................................................................... ............................................................................ .......................................... I'm crimping terminals for the capacitative fuel senders in the tank for my RV-6. Help! Lost in crimper land John RV-6 (left wing tank) ________________________________________________________________________________
From: "Rob A" <racker(at)rmci.net>
Subject: Crimpers?
Date: Dec 18, 2001
Hmmm...right there at http://www.aeroelectric.com/Catalog/tools/tools.html#rct-1 Rob Acker (RV-6, wired with the tool above). > -----Original Message----- > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of John > Lawson > Sent: Tuesday, December 18, 2001 8:31 PM > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: Crimpers? > > > > > I looked on the B&C web site for crimpers as one lister > suggested...no luck, doesn't look like they're selling them any > more. I find about a millyun different types of crimpers > (ok...well...mebbe not that many) on the Digi-Key web site...and > I found one in the Aircraft Spruce catalog...any suggestions on > which one I should > buy? > > I'm crimping terminals for the capacitative fuel senders in the > tank for my RV-6. Help! > > Lost in crimper land > John > RV-6 (left wing tank) ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: Crimpers?
Date: Dec 18, 2001
John, The RCT-1 tool on B&C's site will do the terminals. The BCT-1 is for D-subs and Molex type pins(like your wing light wires that plug in at the fuselage). The RCT-2 is for BNC connectors. I didn't crimp the awg18 to the inner BNC connection. Soldering and then coating the BNC and 1 1/2" of the wire with proseal secures it. I talked to the inventor of this setup and this is how he advised doing it. Jerry Calvert Edmond Ok -6 ----- Original Message ----- From: John Lawson <jwlawson(at)hargray.com> Subject: AeroElectric-List: Crimpers? > > I looked on the B&C web site for crimpers as one lister suggested...no luck, doesn't look like they're selling them any more. I find about a millyun different types of crimpers (ok...well...mebbe not that many) on the Digi-Key web site...and I found one in the Aircraft Spruce catalog...any suggestions on which one I should > buy? > > I'm crimping terminals for the capacitative fuel senders in the tank for my RV-6. Help! > > Lost in crimper land > John > RV-6 (left wing tank) > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 18, 2001
Subject: Wire Stripping !!!!!!!!!
Hi Everyone , I don't chime in often but I've read promotion , of late , of the "Ideal" brand of automatic (single action) wire strippers . Everyone is welcome to use what they want or can afford but the Feds do not approve of these wire strippers because they truly do NOT have the performance capabilities of the similar style of strippers that use dies in place of the sharp edged $ 20 version . The "die" types are about $ 125 & they will virtually NEVER nick the wire or remove any strands . The only safe way to use the cheapies for aviation use is to visually inspect EVERY strip with great lighting & a jewelers loop to assure no nicks occured & all strands are present ! Are you really making any of your homebuilt dream "pretty good" or "good enough" ?? Then don't do it to the wire . The entire plane is obviously no better than it's weakest link & if it's an IFR bird it can be even more crucial that you maximize electrical integrity . Any wire bound for a crimped pin that is missing a single strand will be crimped to the wrong calibration . Just MHO & I welcome correction/critisism . FWIW I've seen multiple listings of the "die" type on Ebay & I got 5 pair of the "Stripmaster" wirestrippers for $ 75 total ! The auction seller was ebayqotm(at)hotmail.com . I believe she has more . I already had buddies that wanted the extras I had , but a few of you could go in on several & save big ! She had them in 10, 12, 14 gauge & 16 thru 26 gauge . Good Luck , Chris ________________________________________________________________________________
Date: Dec 19, 2001
From: John Rourke <john@allied-computer.com>
Subject: Re: Wire Stripping !!!!!!!!!
Chris - But the ones you bought *are* the "Ideal" brand, and they *also* use knife-edge cutting surfaces - I've been using them for years in manufacturing. Incidentally, they are essentially identical to the ones from Radio Shack - I used to pay $31 through my industrial supply house, until I realized they were the same as the ones at Radio Shack, but less than 1/2 the price (I thought they were $15 - but the catalog shows 12.99?). <http://www.radioshack.com/product.asp?catalog%5Fname=CTLG&category%5Fname=CTLG%5F005%5F005%5F009%5F000&product%5Fid=64%2D1919> -John CBFLESHREN(at)aol.com wrote: > > > Hi Everyone , I don't chime in often but I've read promotion , of late , of > the "Ideal" brand of automatic (single action) wire strippers . Everyone is > welcome to use what they want or can afford but the Feds do not approve of > these wire strippers because they truly do NOT have the performance > capabilities of the similar style of strippers that use dies in place of the > sharp edged $ 20 version . The "die" types are about $ 125 & they will > virtually NEVER nick the wire or remove any strands . The only safe way to > use the cheapies for aviation use is to visually inspect EVERY strip with > great lighting & a jewelers loop to assure no nicks occured & all strands are > present ! Are you really making any of your homebuilt dream "pretty good" or > "good enough" ?? Then don't do it to the wire . The entire plane is > obviously no better than it's weakest link & if it's an IFR bird it can be > even more crucial that you maximize electrical integrity . Any wire bound for > a crimped pin that is missing a single strand will be crimped to the wrong > calibration . Just MHO & I welcome correction/critisism . FWIW I've seen > multiple listings of the "die" type on Ebay & I got 5 pair of the > "Stripmaster" wirestrippers for $ 75 total ! The auction seller was > ebayqotm(at)hotmail.com . I believe she has more . I already had buddies that > wanted the extras I had , but a few of you could go in on several & save big > ! She had them in 10, 12, 14 gauge & 16 thru 26 gauge . Good Luck , Chris > ________________________________________________________________________________
From: "Jerry Calvert" <rv6bldr(at)home.com>
Subject: Re: Wire Stripping !!!!!!!!!
Date: Dec 18, 2001
----- Original Message ----- From: <CBFLESHREN(at)aol.com> Subject: AeroElectric-List: Wire Stripping !!!!!!!!! Chris, Your points have merit, but I can't resist. > Hi Everyone , I don't chime in often but I've read promotion , of late , of > the "Ideal" brand of automatic (single action) wire strippers . Everyone is > welcome to use what they want or can afford but the Feds do not approve of > these wire strippers because they truly do NOT have the performance > capabilities of the similar style of strippers that use dies in place of the > sharp edged $ 20 version . The "die" types are about $ 125 & they will > virtually NEVER nick the wire or remove any strands . The only safe way to My RV the experimental way = +/- $45k My RV the Fed way = +/-$450,000 ; ) > use the cheapies for aviation use is to visually inspect EVERY strip with > great lighting & a jewelers loop to assure no nicks occured & all strands are > present ! Are you really making any of your homebuilt dream "pretty good" or > "good enough" ?? Then don't do it to the wire . The entire plane is > obviously no better than it's weakest link & if it's an IFR bird it can be > even more crucial that you maximize electrical integrity . Any wire bound for > a crimped pin that is missing a single strand will be crimped to the wrong > calibration . Just MHO & I welcome correction/critisism . FWIW I've seen > multiple listings of the "die" type on Ebay & I got 5 pair of the My "Ideal" brand wirestrippers ARE Stripmasters! Says so right on 'em! Paid about the same price as ebay. > "Stripmaster" wirestrippers for $ 75 total ! The auction seller was > ebayqotm(at)hotmail.com . I believe she has more . I already had buddies that > wanted the extras I had , but a few of you could go in on several & save big > ! She had them in 10, 12, 14 gauge & 16 thru 26 gauge . Good Luck , Chris No flame! Just another opinion, which we all are welcome to have. Good day, Jerry Calvert Edmond Ok -6 ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 19, 2001
Subject: Re: Wire Stripping !!!!!!!!!
In a message dated 12/19/2001 2:07:16 AM Eastern Standard Time, john@allied-computer.com writes: > Chris - > > But the ones you bought *are* the "Ideal" brand, and they *also* use > knife-edge cutting surfaces - I've been using them for years in > manufacturing. Incidentally, they are essentially identical to the ones > from Radio Shack - I used to pay $31 through my industrial supply house, > until I realized they were the same as the ones at Radio Shack, but less > than 1/2 the price (I thought they were $15 - but the catalog shows > 12.99?). > > <http://www.radioshack.com/product.asp?catalog%5Fname=CTLG& > category%5Fname=CTLG%5F005%5F005%5F009%5F000&product%5Fid=64%2D1919> > > -John > Hi John , I'll conceed the Brands are alike but on the rest I have to disagree . I'll happily take macro photos of the two major differences in the two types of strippers & send them to you if it will clarify . The "die" are not sharp , which is why they do the least damage to the wire . The other major diff to compensate for the dull dies is the side of the tool that grips & holds the insulation consists of stippled metal surfaces that are equal to approx. 80 grit sandpaper in roughness to better grip Tefzel etc ....Check out the surfaces on the cheap version . This is the other reason why the production cost hence selling price is higher . Take care , Chris . ________________________________________________________________________________
From: "Gaylen Lerohl" <lerohl@rea-alp.com>
Subject: Re: Crimpers?
Date: Dec 19, 2001
John: Check these out: http://www.terminaltown.com/Pages/EclipseCrimpTools.html and http://www.terminaltown.com/Pages/SargentBrandCrimpers.html. Both ratcheting crimpers with interchangeable die sets for a good price. Gaylen Lerohl Terminaltown ----- Original Message ----- From: John Lawson <jwlawson(at)hargray.com> Subject: AeroElectric-List: Crimpers? > > I looked on the B&C web site for crimpers as one lister suggested...no luck, doesn't look like they're selling them any more. I find about a millyun different types of crimpers (ok...well...mebbe not that many) on the Digi-Key web site...and I found one in the Aircraft Spruce catalog...any suggestions on which one I should > buy? > > I'm crimping terminals for the capacitative fuel senders in the tank for my RV-6. Help! > > Lost in crimper land > John > RV-6 (left wing tank) > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: re: crimpers - thanks!
Date: Dec 19, 201
John Lawson wrote: > > --> > > Thanks to all who responded to my question about a source for crimpers. I > went right by those URLs that y'all sent me, if they'd been snakes I'd > have been bitten. Thanks for pointing them out! *** The Sargent crimper is an especially good unit. It has a finer-toothed ratchet than the Taiwanese ones, and the handles fold into each other ( one handle is wider than the other ) for better ergonomics ( it's easier for the hand to squeeze something small and close together than something wide and far apart ). In a Light Plane Maintenance crimper shootout, the Sargent outperformed everything except the $300 AMP crimper. That being said, I bought the Ideal ( Taiwanese ) crimper. It was perfectly adequate for my purposes, and the local electronics store had a wide selection of dies for it. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 19, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Crimpers?
> >> I looked on the B&C web site for crimpers as one lister suggested...no >luck, doesn't look like they're selling them any more. I find about a >millyun different types of crimpers (ok...well...mebbe not that many) on the >Digi-Key web site...and I found one in the Aircraft Spruce catalog...any >suggestions on which one I should . . . Never did sell the die sets. The Coax and PIDG tools on our site have removable dies and COULD be interchanged. When I first began to offer them about 5 years ago, I considered selling handles and die sets. Harking back over 40+ years of experience, I KNEW that keeping loose parts for tools in close proximity to the body of the tool was an iffy proposition. It doesn't take very many incidences of misplaced or lost parts to gobble up productive time exceeding the value of the tool when it comes time to change the color of a crimp tool's spots . . . That's why I elected to offer each tool complete to the intended task with the knowledge that when I'm ready to do the job, the tool is ready to support the effort. Bob . . . ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Wire Stripping !!!!!!!!!
Date: Dec 19, 201
Stein Bruch wrote: > You make a good point and I definately agree with you on the "Mil-Spec" > quality strippers. They do a better job, but it's all relative. Even the > Mil-Spec strippers will nick the wire somewhat. From my airline employment > days, I had the fortune of sitting in a class where we inspected wires > stripped with dozens of kinds of strippers under a HIGH power microscope. > > OK, here's the big point. ANY stripper which uses "mecahnical" > cutters/teeth will leave a scar on the wire somewhere. *** I believe AC43-13 has a table somewhere showing how many strands can be nicked or broken for different sizes of wire for an acceptable joint. Probably mostly applies to larger wire sizes. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 19, 2001
From: Mark Steitle <msteitle(at)mail.utexas.edu>
Subject: Re: Wire Stripping !!!!!!!!!
I have a electric thermal wire stripper that I would like to use when wiring my plane. Unfortunately, it has a burnt jaw (or thermal element), which is replaceable. Does anyone know where I could get a new set of jaws... Radio Shack has never heard of a thermal wire stripper. Go figure! > >Stein Bruch wrote: > > You make a good point and I definately agree with you on the "Mil-Spec" > > quality strippers. They do a better job, but it's all relative. Even the > > Mil-Spec strippers will nick the wire somewhat. From my airline employment > > days, I had the fortune of sitting in a class where we inspected wires > > stripped with dozens of kinds of strippers under a HIGH power microscope. > > > > OK, here's the big point. ANY stripper which uses "mecahnical" > > cutters/teeth will leave a scar on the wire somewhere. > >*** I believe AC43-13 has a table somewhere showing how many strands can be >nicked or broken for different sizes of wire for an acceptable joint. >Probably mostly applies to larger wire sizes. > > - Jerry Kaidor ( jerry(at)tr2.com ) > > ________________________________________________________________________________
Date: Dec 19, 2001
From: Mark Steitle <msteitle(at)mail.utexas.edu>
Subject: Re: Wire Stripping !!!!!!!!!
Well, now I feel like a dummy! A simple web search turned up a plethora of sources for this. The first site (http://www.teledyneinterconnect.com/products/wire_strippers/wirestrip_esd.asp) handles both Stripall and EDS. I think mine is an EDS brand (see attachment). They have a directory by state for suppliers. I think I have the riddle solved. This thread on stripping wires has been enlightening. > > >I have a electric thermal wire stripper that I would like to use when >wiring my plane. Unfortunately, it has a burnt jaw (or thermal element), >which is replaceable. Does anyone know where I could get a new set of >jaws... Radio Shack has never heard of a thermal wire stripper. Go figure! ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Dec 19, 2001
Subject: Re: Crimpers?
In a message dated 12/18/01 6:43:36 PM Pacific Standard Time, jwlawson(at)hargray.com writes: << jwlawson(at)hargray.com >> Hi John: I just bought a terminal crimper from B&C less than two weeks ago and ordered it from their web site. Try again. I have several times been unable to find stuff on their web site that I know they carry, then I go back a few days later and, lo and behold, there it is. Being somewhat computer challenged (ig'nernt) I don't have any idea what I'm doing wrong in the off times. Sometimes I have better luck going to B&C via the link on Bob Nuckoll's site (www.aeroelectric.com). Harry Crosby Pleasanton, California RV-6, finish kit stuff ________________________________________________________________________________
Date: Dec 19, 2001
From: William Mills <courierboy(at)earthlink.net>
Subject: Re: Crimpers?
Hi guys - Go to B&C by clicking on the link at Bob's AeroElectricConnection web site - I don't think the products we're talking about are "reachable" from the B&C home page (only starters and generators and stuff). I too couldn't navigate B&C very well - only way to get there is via AEC web site I think. Bill > >In a message dated 12/18/01 6:43:36 PM Pacific Standard Time, >jwlawson(at)hargray.com writes: > ><< jwlawson(at)hargray.com >> > >Hi John: I just bought a terminal crimper from B&C less than two weeks ago >and ordered it from their web site. Try again. I have several times been >unable to find stuff on their web site that I know they carry, then I go back >a few days later and, lo and behold, there it is. Being somewhat computer >challenged (ig'nernt) I don't have any idea what I'm doing wrong in the off >times. Sometimes I have better luck going to B&C via the link on Bob >Nuckoll's site (www.aeroelectric.com). > >Harry Crosby >Pleasanton, California >RV-6, finish kit stuff ________________________________________________________________________________
Date: Dec 19, 2001
From: John Top <jjtop1(at)earthlink.net>
Subject: Re: Wire Stripping !!!!!!!!!
> OK, here's the big point. ANY stripper which uses "mecahnical" > > cutters/teeth will leave a scar on the wire somewhere. > >*** I believe AC43-13 has a table somewhere showing how many strands can be >nicked or broken for different sizes of wire for an acceptable joint. 'lectrik Bob: How about weighing in on this thread. Do we need to put up with the inconvenience of using a thermal stripper or is a more portable mechanical stripper adequate? What is the best approach to one or more mechanical wire strippers for our use? I notice that you don't have one in your catalog. Is that because you don't have a recommendation? I asked for a recommendation when I ordered some terminals and a crimper last week. I was told that they were using "stripmasters" in the shop, but didn't specify whether it was the "cutter" style or the "Custom Stripmaster" "die-type" stripper. I have a $20 "cutter style" Stripmaster for use on #22 to #10 wire that I have been using for everyday wiring jobs around the house. Do I need to buy a milspec Custom stripper (strippers) for my project? It looks like that could get pretty pricey pretty quick. I notice that the Ideal Customs do not handle a very wide range of wire sizes and that they list different strippers for PVC and Teflon coated wires. So what is the answer for those of us suffering from "stripperphobia?" I am not far enough along to know what wire sizes I will be dealing with, but I would imagine that the bulk of them will fall within a small range of sizes. Which sizes? Thanks -- John ________________________________________________________________________________
From: "Brian & Debi Shannon" <wings(at)theshannons.net>
Subject: Coax Feedline Question
Date: Dec 19, 2001
Bob or anyone, Is there any reason not to run two coax feedlines down the fuselage (composite) right next to each other after they have been routed away from their respective foil antennas (preferrably at an initial 90 deg angle from the antenna)? Thanks ________________________________________________________________________________
From: Aucountry(at)aol.com
Date: Dec 20, 2001
Subject: Re: Wire Stripping !!!!!!!!!
Where can I get a good pair of wire stripers and crimpers? ________________________________________________________________________________
From: Aucountry(at)aol.com
Date: Dec 20, 2001
Subject: Re: Wire Stripping !!!!!!!!!
that's strippers ________________________________________________________________________________
From: "Gary K" <flyink(at)efortress.com>
Subject: Re: Wire Stripping !!!!!!!!!
Date: Dec 20, 2001
Some people might think it's a waste of money, and I'm sure there are more economical and even better ways to do it, but I went out and bought the AMP Pro-Crimper with PIDG dies and Stripmaster from Techni-tool. With the amount of money spent on the plane and the amount of wires that have to be connected, the cost of the tools becomes insignificant compared to the absolute pleasure of working with quality and confidence. This is the most enjoyable part of building so far and I consider these "lifetime" tools. I may have to build another plane to justify the cost but that's the price I'm willing to pay ;<}. The mil stripper p/n that I got is 462ST11Q, it is an Ideal Stripmaster for tefzel wire and it has the one cutter with sizes from 16-26 ga. www.techni-tool.com Gary K. ----- Original Message ----- From: <Aucountry(at)aol.com> Subject: Re: AeroElectric-List: Wire Stripping !!!!!!!!! > > Where can I get a good pair of wire stripers and crimpers? > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: "Ned Thomas" <nthomas(at)mmcable.com>
Subject: Re: Wire Stripping !!!!!!!!!
Date: Dec 20, 2001
Yesterday our neighbor lady came over. She's got quite a bit of country in her. She seen my computer screen which happened to be a full page listing of the aeroelectric emails I received lately. There was a whole list of pretty much nothing but Wire Stripping!!!!!!! Which she read We're Stripping!!!!!!! She of course wanted to know what kind of computer discussion group would be stripping..... Just a little humor.... ----- Original Message ----- From: "Gary K" <flyink(at)efortress.com> Subject: Re: AeroElectric-List: Wire Stripping !!!!!!!!! > > Some people might think it's a waste of money, and I'm sure there are more > economical and even better ways to do it, but I went out and bought the AMP > Pro-Crimper with PIDG dies and Stripmaster from Techni-tool. With the > amount of money spent on the plane and the amount of wires that have to be > connected, the cost of the tools becomes insignificant compared to the > absolute pleasure of working with quality and confidence. This is the most > enjoyable part of building so far and I consider these "lifetime" tools. I > may have to build another plane to justify the cost but that's the price I'm > willing to pay ;<}. The mil stripper p/n that I got is 462ST11Q, it is an > Ideal Stripmaster for tefzel wire and it has the one cutter with sizes from > 16-26 ga. www.techni-tool.com > > Gary K. > > ----- Original Message ----- > From: <Aucountry(at)aol.com> > To: > Subject: Re: AeroElectric-List: Wire Stripping !!!!!!!!! > > > > > > Where can I get a good pair of wire stripers and crimpers? > > > > > > > > > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: Aucountry(at)aol.com
Date: Dec 20, 2001
Subject: Re: Wire Stripping !!!!!!!!!
In a message dated 12/20/01 5:33:22 AM, flyink(at)efortress.com writes: << and I'm sure there are more economical and even better ways to do it, but I went out and bought the AMP Pro-Crimper with PIDG dies and Stripmaster from Techni-tool. >> OK, I'm being lazy, where are they, do they have a web site, what is their phone number? ________________________________________________________________________________
Date: Dec 20, 2001
From: Quilters Confectionery <qltconf(at)earthlink.net>
Subject: In-Line fuse for Certified Aircraft - Cessna 150 Cigaret
AD AD 79-08-03 applies to my Cessna 150 H. ___________The important part is (this is not a complete copy - only an extract)___________________ To prevent an inflight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel, accomplish the following: A) Disconnect the wire, at the ammeter or at the electrical system bus as applicable, that connects the bus to the cigar lighter receptacle. Following the disconnection of this wire either: 1) Reconnect the wire to the electrical bus by using an existing or newly installed circuit protection device that is properly rated to protect the wire gauge used for this circuit, or 2) Disconnect the wire from the lighter receptacle at the opposite end and remove it from the airplane, or 3) Protect the wire by insulating its disconnected end, fold this wire end back against the wire bundle in which it is routed and secure it to that bundle. NOTE: For those installations reconnected in accordance with paragraph A 1 the proper rated circuit protection device to be used may be determined by consulting FAA Advisory Circular 43.13-1A. ____________________________ end of extract ____________________________________ My aircraft has had method 3 applied. I need my Cigaret Lighter back in operation to power things like my Anywhere Map system (wonderful). To do this, I want to go to method 1 - fuse in line with cigaret lighter My simple question is; Where can I get an in-line fuse holder that is approved for certified airplane use? I know we are not suppose to go to the local Ace hardware store for screws (mine all come from Spruce and I keep the records to be able to prove it). Does not sound right to go to the local Radio Shack for a fuse holder. I even looked in the WAG Aero catalog which specifies if an item is for certified aircraft (I like that) but no fuse holders. Spruce has them but no statement about being for certified aircraft. I think my A&P will sign off on the install but he is stickler for source of parts (good). I am confident this group has the answer. Sorry so long but to get a complete answer one needs a complete question and data behind it. Happy Holidays to All, Larry Owner/Operator N22027 :-) PS Bought Revision 10 The Aero Connection Book. It is absolutely wonderful! Best investment I have made in understanding things in my fun machine that the typical A&P's I have encountered are not able to help with. http://www.quiltsweets.com ________________________________________________________________________________
From: "John Brick" <jbrick(at)wolfenet.com>
Subject: KLN94 GPS Wiring
Date: Dec 20, 2001
Does anyone have the wiring schematic for the external connection to the KLN94. I would like to build a docking station for the "take home mode." According to the Pilot's Guide, all you have to do is ground the appropriate pin at the back of the unit...removed from the aircraft, of course. And hook up a power supply. John Brick Tacoma RV-4 ________________________________________________________________________________
From: CBFLESHREN(at)aol.com
Date: Dec 20, 2001
Subject: Re: In-Line fuse for Certified Aircraft - Cessna 150
Cigar... In a message dated 12/20/2001 12:48:59 PM Eastern Standard Time, qltconf(at)earthlink.net writes: > My simple question is; Where can I get an in-line fuse holder that is > approved for certified airplane use? I know we are not suppose to go to the > local Ace hardware store for screws (mine all come from Spruce and I keep > Hi Larry , Spruce ALSO has the nice "legal" bayonet (front load) fuse holders in thier catalog (P/N FU002) . Happy Holidays ! , Chris ________________________________________________________________________________
Date: Dec 20, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: In-Line fuse for Certified Aircraft - Cessna 150
Cigar... > >In a message dated 12/20/2001 12:48:59 PM Eastern Standard Time, >qltconf(at)earthlink.net writes: > > >> My simple question is; Where can I get an in-line fuse holder that is >> approved for certified airplane use? I know we are not suppose to go to the >> local Ace hardware store for screws (mine all come from Spruce and I keep >> > >Hi Larry , Spruce ALSO has the nice "legal" bayonet (front load) fuse holders >in thier catalog (P/N FU002) . Happy Holidays ! , Chris There's no such thing as an "approved fuse holder" . . . there are lots of products used on certified airplanes because they were on the drawings that fabricated the airplane the day it was certified. An aircraft manufacturer can put virtually ANYTHING on the airplane they choose as long as it meets all of the requirements for suitability to the intended task. A Bussmann HKP panel mounted fuse holder was used on thousands of Cessnas and Pipers in the early days of electrification of airplanes . . . but the HKP is neither certified nor approved for any application other than to replace a damaged fuseholder where the drawings call out that product . . . and then only if you buy the fuseholder through the OEM's service-parts system . . . ostensibly to insure that you're getting the REAL part and not some bogus substitute. Technically, the only legal replacement for the fuse is one acquired through Cessna service parts. Obviously, it probably came right out of Bussmann's or Littlefuse's catalogs. Just because Aircraft Spruce says "this part is 'legal' or 'used on certified ships' does not make it a shoo-in for your problem if you're really concerned about the legalities of so trivial an item. IF the legalities are important to you. Get the part from Cessna service parts and take the hit. Otherwise, go down to the local automotive parts store and get something that's rated to do the task and just don't tell anyone about it. The later action has a better than even chance that you'll get a part that is BETTER than the one originally certified onto the airplane. Bob . . . ________________________________________________________________________________
Date: Dec 20, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Coax Feedline Question
> >Bob or anyone, > > Is there any reason not to run two coax feedlines down the fuselage >(composite) right next to each other after they have been routed away from >their respective foil antennas (preferrably at an initial 90 deg angle from >the antenna)? > >Thanks None whatsoever . . . Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 20, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Wire Stripping !!!!!!!!!
> >> OK, here's the big point. ANY stripper which uses "mecahnical" >> > cutters/teeth will leave a scar on the wire somewhere. >> >>*** I believe AC43-13 has a table somewhere showing how many strands can be >>nicked or broken for different sizes of wire for an acceptable joint. > >'lectrik Bob: > >How about weighing in on this thread. > >Do we need to put up with the inconvenience of using a thermal >stripper or is a more portable mechanical stripper adequate? Before anyone runs out and buys anything expensive . . . let me finish a "shop notes" addition to the website. I've been following the thread and there's just enough truth in each admonition to lend credence to a lot of misunderstanding. I'll try to have it done this weekend . . . as an advance teaser, I can tell you that I'd have no problems wiring up an airplane with a $3 pair of strippers from Radio Shack . . . there are more CONVENIENT tools but it doesn't take a lot of practice or skill to get by inexpensively either. Got the piece illustrated and about half written last night. I need to take care of some customers for a couple of days. More to come soon . . . Bob . . . ________________________________________________________________________________
From: "Rick" <turboflyer(at)mediaone.net>
Subject: Transponder antenna location
Date: Dec 20, 2001
Is it possible to run two transponder antennas for the same transponder? Mine is blocked in the forward position by my radiator. Until I make a metal radiator scoop and mount to it at the lowest point, I am stuck. Rick ________________________________________________________________________________
From: ScramIt(at)aol.com
Date: Dec 20, 2001
Subject: Navaid and KLX135A
Hello all, I have a friend with a BendixKing KLX135A and a Navaid wing leveler. We can't get them to couple. Friends of ours say you can't use a 135A with the Navaid, They've tried the filter they've tried the smart coupler. Navaid says its the signal from the 135A and Bendix King says its the Navaid. Does anyone one know of someone who has that combo and has them working together? Thanks for your time, SteveD ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: In-Line fuse for Certified Aircraft - Cessna
150 Cigar...
Date: Dec 20, 2001
Robert L. Nuckolls, III wrote: > > > IF the legalities are important to you. Get the part from > Cessna service parts and take the hit. *** Another possibility is to fill out a 337, get something MIL-spec or somesuch and get a field approval for it. Takes a cooperative FSDO inspector. And it helps if the part has been used in some other certificated aircraft, or is MIL-spec so he won't feel he's sticking his neck out too far. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
From: "Dave Grosvenor" <dwg(at)iafrica.com>
Subject: Antenna
Date: Dec 22, 2001
I bought a Cessna comm antenna at the Fly Mart at AirVenture. When I measure the resistance between the outside of the BNC and the centre pin, I get 0 ohms (measured on the antenna, nothing else connected). Is there something inside these antennas that will make it look like a short circuit or is this thing dead? It's so simple I can't see how it can go faulty. Dave ________________________________________________________________________________
From: "Jesse Kluijfhout, PE1RUI" <jessevli(at)zeelandnet.nl>
Subject: Re: Antenna
Date: Dec 22, 2001
Hi Dave, Its possible that it looks like a short circuit, because you measured resistances. You should measure the resistances on the frequency you want to use it.. (That the impedance of a certain frequency). and not the DC resistance youve measured.. There are special antenna analyzer which can do this job for you. You could try simpler by connect the antenna to youre receiver, try to listen to a local frequency and notice if it does work or not... If it does, check the SWR with an SWR analizer. These are much cheaper than a antenna analyzer. You also could ask a local avionics shop or a local ham radio amateur, who might be willing to help you and let them borrow there SWR meter, or they might will be test it for you. Than youre sure. Regards, Jesse ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Antenna
Date: Dec 22, 2001
Dave Grosvenor wrote: > > > I bought a Cessna comm antenna at the Fly Mart at AirVenture. When I > measure the resistance between the outside of the BNC and the centre pin, I > get 0 ohms (measured on the antenna, nothing else connected). Is there > something inside these antennas that will make it look like a short circuit > or is this thing dead? It's so simple I can't see how it can go faulty. > *** It's common to have inductors or matching transformers insdie an antenna that will make it look like a short to DC. I would hook the antenna up to a handheld or a scanner and see if it receives well. Make sure you use a piece of coax so both "sides" of the antenna circuit are connected. If it receives well, compared to a hunk of wire ( say 21" of wire ) stuck into the center pin of the receiver input connector, then it's probably OK. It's also possible for an antenna to have a real internal short. So I would check it out before installing it, especially before transmitting on it. Otherwise, you could damage your transmitter. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 22, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Transponder antenna location
> > > Is it possible to run two transponder antennas for the same transponder? >Mine is blocked in the forward position by my radiator. Until I make a metal >radiator scoop and mount to it at the lowest point, I am stuck. > >Rick Not without more difficulty that you'd like to put up with. You might mount it temporarily as far aft as you can . . . perhaps back behind the seats. The degree of shadowing may be very small to negligible from that location. Bob. . . ________________________________________________________________________________
Date: Dec 22, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: A question on split battery electrical systems
>Robert: > >Thanks for your great website and your kind responses to my past questions. I >have another general question for which I'd appreciate your thoughts. Thank you for the kind words. I'm pleased that you find the information useful. . . > >I have been pursuing the design of an all electrical panel for my Europa which >at this point includes an auxiliary alternator on the vacuum pad of the Rotax 914 >and appropriate bussing as per The Aeroelectric Connection. Since the 914 >vacuum pad turns about 20% slower than a Lycoming pad, the output of an SD-8 >might be marginal; An SD-20 would do better, but may not fit. But what of that. First, are you sure you need dual alternators? How do you plan to use the airplane? The ignition systems on a 914 are self powered so the only thing you need to do is keep the panel lit up. > >The forward CG bias of a 914 installation - indeed, any installation with an Airmaster >CS prop - usually means that the battery must be installed behind the seats with a >commensurately heavy (7-8 lbs) run of welder's cables forward to the starter. Several builders >have used two batteries, though for redundancy rather than what I'm thinking of. > >My thought is to use one of the newer "high-crank-amps" batteries in the engine >compartment with a short run of cables to the alternator and contactor, and a fairly >small standard battery in the back for other system electrical loads. This could save >weight, because: >1. The total weight of the two batteries would be less than one large battery >2. the interconnecting cables could be thin gauge (10 or 12) and therefore much lighter >3. the overall AH capacity of the system might be reduced since (it seems to me) that the AH > rating of a battery is determined by cranking capability first and system load demands 2nd. > If a modest size battery with very low internal resistance is used, this could be the equivalent > of a larger battery with higher resistance. > >Have you had any experience with such "high-crank-amps" batteries or distributed systems >such as what I am proposing? Cranking will not be an issue if you use recombinant gas (RG) batteries. All you need to concern yourself with is alternator-out endurance. What is your minimum electrical load for comfortable termination of flight? Even with electric gyros, you can probably get this down to under 5 amps. If you need 3-4 hour endurance, then a 24 a.h. battery that is monitored for capacity (or simply replaced every two years) would cover you. I don't think I'd want to hose up a really nice airplane by loading it down with so much electrical hardware if we can keep it simple, easy to install and low cost to install and maintain. > >PS. Where can one get one of the "good" contactors shown on your website? All of the products on our website are sold from the catalog index/order form at http://www.aeroelectric.com/Catalog/BCcatalog.html Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Go ahead, make my day . . . > < show me where I'm wrong. > ================================= ________________________________________________________________________________
Date: Dec 22, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Connecting a wire to a BNC connector
> >> > >Ah, drat...I should have told you what kind of BNC connector, I didn't realize there were coax BNC connectors also...the plans show it as an "AV BNC 31-236-RFX BNC Bulkhead Terminal." It has one verrrrrry little socket for a wire (18 AWG, I think). 18AWG!!!!???!!! what coax needing a BNC connector has this big a wire down the middle? Did a search on the part number and couldn't turn anything up. Do you know who makes the connector? Brand name on package? Bob . . . ________________________________________________________________________________
From: "Jim Robinson" <jbr(at)hitechnetworks.net>
Date: Dec 22, 2001
Subject: Re: Transponder antenna location
> > > > > > > > Is it possible to run two transponder antennas for the same transponder? > >Mine is blocked in the forward position by my radiator. Until I make a > >metal radiator scoop and mount to it at the lowest point, I am stuck. > > > >Rick > > Not without more difficulty that you'd like to > put up with. You might mount it temporarily as far > aft as you can . . . perhaps back behind the seats. > The degree of shadowing may be very small to negligible > from that location. > > Bob. . . > In our Glasair 1 we ended up moving the antenna clear back in front of the tail on the belly from under the seat between the gear legs. It worked better , but still had a weak area directly ahead. I think the engine blocked it in that direction. Jim > advertising on the Matronics Forums. > members. > http://www.matronics.com/ > > > > > > > ________________________________________________________________________________
Date: Dec 23, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Re: AeroElectric-List Digest: 7 Msgs - 12/22/01
> > From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> > Subject: AeroElectric-List: Re: Connecting a wire to a BNC connector > > > > > >> > > > >Ah, drat...I should have told you what kind of BNC connector, I didn't realize there were coax BNC connectors also...the plans show it as an "AV BNC 31-236-RFX BNC Bulkhead Terminal." It has one verrrrrry little socket for a wire (18 AWG, I think). > > 18AWG!!!!???!!! what coax needing a BNC connector > has this big a wire down the middle? > > Did a search on the part number and couldn't turn > anything up. Do you know who makes the connector? > Brand name on package? > Ah, my untrained and uneducated mind sez it probably isn't coax. Sorry about that, I think I confused you with my remark about coax connectors. I took that part number off the Van's plans for the capacative fuel senders (they are to be hooked up to the EI fuel gauges that Van's sells). The connector fits into the inboard (root) rib for the fuel tank. There's one socket on the end of the connector that is inside the tank. The end inside the tank also has threads and a nut (to keep the connector from falling out of the hole)...there's also a small ring with a tab and a hole in the tab, I presume the ring goes on the connector and is for another wire? Altho in the plans, I only see one wire... The wire goes from the connector to the next rib outboard, where it is connected to the inboard sender plate. The wire then goes to the fifth rib outboard, where it connects to the sender plate there. The bag that the connector came in didn't have a part number of brand name, maybe EI makes or sells them? Perhaps it'd be worth an email to Van's to ask about it? Maybe some of the other RV builders can jump in here and help? Semper Fi John RV-6 (left wing fuel tank) ________________________________________________________________________________
From: BAKEROCB(at)aol.com
Date: Dec 23, 2001
Subject: Using BNC connectors
In a message dated 12/23/2001 2:52:37 AM Eastern Standard Time, jwlawson(at)hargray.com writes: <> And Bob Nuckolls responds: <<18AWG!!!!???!!! what coax needing a BNC connector has this big a wire down the middle? Did a search on the part number and couldn't turn anything up. Do you know who makes the connector? Brand name on package? Bob . . . >> 12/23/01 Hello John and Bob, May I attempt to contribute / clarify? 1) John, BNC connectors are designed to only connect coaxial wires / cables. 2) John, It is still not clear exactly what problem you are trying to solve. I believe that you are attempting to use a particular type of BNC bulkhead connector (31-236) to connect some non coaxial fuel quantity system wiring. Is that right? (I also note that type 31-236 is not for pressurized use. Will that make a leakage difference?) 3) Bob, type 31-236 (not a part number) 50 OHM MIL UG-625B Bulkhead BNC receptacles are made by Amphenol (among others). Newark stock number is 39F1337. 4) John, any time that you start using an object for an outside of intended designed purpose you must expect to do some freelancing / innovation / head scratching to make make it all fit or work. 5) John, when you ask a question in this forum the more specific and complete information that you can provide initially the better chance you have of getting a quicker meaningful / useful answer. Please let us know when / if the issue is resolved / understood. Thanks. 'OC' Baker, Builder of KIS TR-1 #116 4/14/97 - ?/?/? ________________________________________________________________________________
Date: Dec 24, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Re: AeroElectric-List Digest: 2 Msgs - 12/23/01
> From: BAKEROCB(at)aol.com > Subject: AeroElectric-List: Using BNC connectors > > > In a message dated 12/23/2001 2:52:37 AM Eastern Standard Time, > jwlawson(at)hargray.com writes: > > < realize there were coax BNC connectors also...the plans show it as an "AV BNC > 31-236-RFX BNC Bulkhead Terminal." It has one verrrrrry little socket for a > wire (18 AWG, I think).>> > > And Bob Nuckolls responds: > > <<18AWG!!!!???!!! what coax needing a BNC connector has this big a wire > down the middle? Did a search on the part number and couldn't turn anything > up. Do you know who makes the connector? Brand name on package? Bob . . . >> > > 12/23/01 > > Hello John and Bob, May I attempt to contribute / clarify? > > 1) John, BNC connectors are designed to only connect coaxial wires / cables. OK, I think I finally figured that out. :-) > 2) John, It is still not clear exactly what problem you are trying to solve. It's a Van's RV-6, I'm installing capacative senders for the EI fuel quantity gauge per the plans and directions supplied by Van's. > I believe that you are attempting to use a particular type of BNC bulkhead > connector (31-236) to connect some non coaxial fuel quantity system wiring. > Is that right? (I also note that type 31-236 is not for pressurized use. Will > that make a leakage difference?) That's correct. It's a non-pressurized tank, so using the connector doesn't appear to be a problem. > 3) Bob, type 31-236 (not a part number) 50 OHM MIL UG-625B Bulkhead BNC > receptacles are made by Amphenol (among others). Newark stock number is > 39F1337. > > 4) John, any time that you start using an object for an outside of intended > designed purpose you must expect to do some freelancing / innovation / head > scratching to make make it all fit or work. Hmmmmmm....I didn't know that that particular part was outside of its intended purpose...as I mentioned, I took all of the information right off the drawing and instructions that Van's supplied. > 5) John, when you ask a question in this forum the more specific and complete > information that you can provide initially the better chance you have of > getting a quicker meaningful / useful answer. Understand and agree. The part number shown on the drawing is all I have...no manufacturer, no MS or AN number, no nuthin'. I even searched Van's parts list and catalog, and couldn't find it, nor could I find it in the Spruce catalog. I think what confused Bob was my mention of "coax" when I said I didn't know that both coax and non-coax BNC connectors. Thanks for your input, hopefully what you found will help Bob (and me!). Semper Fi John ________________________________________________________________________________
From: SportAV8R(at)aol.com
Date: Dec 24, 2001
Subject: Re: Transponder antenna location
Hi, Bob, and everyone else on the List, Merry Christmas. I have a question in this vein. Right now I am in the middle of changing over the wheel pants on my RV-6A from the old style to the new 2-piece "pressure recovery" pants. These pants are quite generous in size, and come with a substantial, flat fiberglass/epoxy bulkhead in the back, to seal off the area behind the tire. I currently run a stubby stainless steel whip-with-corona-ball type of transponder antenna on the belly of the plane, where it occasionally quits working due to oily build-up. I suspect that it is a draggy installation, if such a short thing can have much drag. Here's where my thoughts are going: I have room to install a horizontal ground plane of about 5in. x 5 in. with same type of antenna in its center, pointed down vertiacally, just behind the bulkhead in the wheel pant. I have already scoped out in my head the coax routing and connectors required to make such an installation workable and removable for maintenance; it looks like 3 or possibly 4 bulkhead BNC connectors, and associated runs or RG-58 (or RG-400, is it, that Bob recommends now?) My biggest concern is possible adverse VSWR and radiation pattern effects from having this antenna radiating element about 12 inches from the center of the axle, with that metal wheel in proximity. I think the field of view from the tip of the antenna at a roughly 3 to 5 degree downward angle will be unrestricted 360 degrees, but looking strictly horizontally,, there will no doubt be some shadowing toward the front. What do you think? Is this idea worth pursuing? I really want to end up with a transponder antenna that doesn't need so much maintenance. Bill Boyd RV-6A O-320/Sensenich FP Hop-Along Air Field, 12VA Clifton Forge, VA ________________________________________________________________________________
Date: Dec 25, 2001
From: John Lawson <jwlawson(at)hargray.com>
Subject: Re: BNC connectors
BAKEROCB(at)aol.com wrote: > In a message dated 12/25/2001 2:54:36 AM Eastern Standard Time, > jwlawson(at)hargray.com writes: > > <<....skip.....It's a Van's RV-6, I'm installing capacative senders for the > EI fuel quantity gauge per the plans and directions supplied by Van's.>> > > That is what I deduced from your original request, but wasn't sure what kind > of wire (coax or non coax, sheilded or non shielded) that you were going to > be using. Yup, I should have mentioned that...it's regular ol' 18 AWG wire, pretty simple. > I think that is a very clever idea that someone came up with, using > a BNC bulkhead connector to pass wiring through the side of a fuel tank. > Normal use for that BNC fitting would be to pass coax wiring through the side > of an electronic box. Ah, I didn't know that...interesting! No wonder I couldn't find it in any of the catalogs (Spruce, Wick's, etc). > < doesn't appear to be a problem.>> > > I guess the real issue here is not whether the tank is pressurized or not, > but whether or not fuel will leak out more readily through a non pressurized > bulkhead fitting. Maybe the sealing goop that you plan to smear around the > inside and outside of the fitting is supposed to solve that problem. > You're exactly right, the directions say to apply Proseal at the connector, if I remember correctly. > < have...no manufacturer, no MS or AN number, no nuthin'. I even searched > Van's parts list and catalog, and couldn't find it, nor could I find it in > the Spruce catalog. I think what > confused Bob was my mention of "coax" when I said I didn't know that both > coax and non-coax BNC connectors.>> > > Being a non electronic type myself I know how easy it is to get lost in their > domain. My extent of experience with things electrical is turning them on and off...oh, and when I was a kid, getting a shock from licking the terminals of a 9v battery. Didn't do that again... > One way to self educate is through catalogs. Mouser, Newark, and > Digikey are three biggies in the business. If you want to pursue this I > recommend starting with a Newark catalog <> or 1-800-4-NEWARK. I'll look Newark up tonite, thanks :-) I have the Digikey site bookmarked. > Another gotcha in this area is numbers. There are part numbers, style > numbers, type numbers, stock numbers, manufacturer's numbers, distributor's > numbers, catalog numbers, industry standard's numbers, etc., etc., etc. So > when one wants to use a number it can be very important to identify just > whose number it is and what kind of number it is supposed to be. Good point, I hadn't thought about the variety of numbers that could be attached to that part. > 'OC' Baker, Builder of KIS TR-1 #116 4/14/97 - ?/?/? Thanks, OC, much appreciated. For Electric Bob: hope this input from OC clarifies things a bit, he's very helpful! I presume that I'll need to solder the wire to the connector. Van's recommends coating the sealing the exposed soldered end of the wire where it connects to the connector. > PS: Maybe Vans can put you in touch with the people who have invented or done > this non standard use of the BNC fitting and they can give you some advice > about how to solder / connect the wires to it. I'll do just that! Maybe Bob has a suggestion or two, also. > Realize that normally one would crimp the proper type of BNC fitting to the > end of a coax wire then attach that fitting to the exterior of the bulkhead > fitting in order to make a connection. Got that...'now I see', said the blind man :-) thanks for the help. > PPS: I presume that you have available one of the books "XX Years of the > RVAtor". > Full of good tips.Easy Publishing, 505-865-3466. Sure do! Semper Fi John ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: BNC connectors
Date: Dec 25, 2001
John Lawson wrote: > > > My extent of experience with things electrical is turning them on and off...oh, > and when I was a kid, getting a shock from licking the terminals of a 9v battery. > Didn't do that again... > *** Gee, I've done that for years. Can tell a nice fresh one from a stale one, from a dead one... "Ah, 1983 Eveready. A fine vintage...." - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
From: "David A. Leonard" <dleonar1(at)maine.rr.com>
Subject: Avionics Master switches
Date: Dec 25, 2001
Merry Christmas all! I just ran across this article on avionics master switches...It seems to disagree with Bob's analysis of the need for them..and being one to stir the pot..here it is: http://www.avweb.com/articles/avmaster.html I tend to believe they are unnecessarymyself, liking Bob's logic....higher parts count.. single point failure, etc.. Dave Leonard.. a man with a '72 Bellanca Viking with no avionics master.. ________________________________________________________________________________
Date: Dec 25, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: New pricing on 760VHF Transceiver
Check out the new pricing on the Microair 760VHF transceiver at http://www.aeroelectric.com/ Bob . . . ________________________________________________________________________________
From: "Gary K" <flyink(at)efortress.com>
Subject: Re: Transponder antenna location
Date: Dec 25, 2001
I'm ready to mount a transponder antenna and I was wondering what some basic guidelines are for the location and orientation. I have a composite fuselage with a metal tail. I was hoping to mount it inside the fuselage somewhere but I don't have a plan yet. Any tips are appreciated. Happy Holidays, Gary K. ----- Original Message ----- From: <SportAV8R(at)aol.com> Subject: Re: AeroElectric-List: Re: Transponder antenna location > > Hi, Bob, and everyone else on the List, Merry Christmas. I have a question > in this vein. Right now I am in the middle of changing over the wheel pants > on my RV-6A from the old style to the new 2-piece "pressure recovery" pants. > These pants are quite generous in size, and come with a substantial, flat > fiberglass/epoxy bulkhead in the back, to seal off the area behind the tire. > I currently run a stubby stainless steel whip-with-corona-ball type of > transponder antenna on the belly of the plane, where it occasionally quits > working due to oily build-up. I suspect that it is a draggy installation, if > such a short thing can have much drag. > > Here's where my thoughts are going: I have room to install a horizontal > ground plane of about 5in. x 5 in. with same type of antenna in its center, > pointed down vertiacally, just behind the bulkhead in the wheel pant. I have > already scoped out in my head the coax routing and connectors required to > make such an installation workable and removable for maintenance; it looks > like 3 or possibly 4 bulkhead BNC connectors, and associated runs or RG-58 > (or RG-400, is it, that Bob recommends now?) > > My biggest concern is possible adverse VSWR and radiation pattern effects > from having this antenna radiating element about 12 inches from the center of > the axle, with that metal wheel in proximity. I think the field of view from > the tip of the antenna at a roughly 3 to 5 degree downward angle will be > unrestricted 360 degrees, but looking strictly horizontally,, there will no > doubt be some shadowing toward the front. > > What do you think? Is this idea worth pursuing? I really want to end up > with a transponder antenna that doesn't need so much maintenance. > > Bill Boyd > RV-6A O-320/Sensenich FP > Hop-Along Air Field, 12VA > Clifton Forge, VA > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
Date: Dec 26, 2001
From: ripsteel(at)edge.net (Mark Phillips)
Subject: Re: New pricing on 760VHF Transceiver
OK, sold. So what's the latest on the XPNDR? (looking for the package deal!) Fom the PossumWorks in TN Mark "Robert L. Nuckolls, III" wrote: > > Check out the new pricing on the Microair 760VHF > transceiver at http://www.aeroelectric.com/ > > Bob . . . > ________________________________________________________________________________
Date: Dec 26, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Transponder antenna location
> >I'm ready to mount a transponder antenna and I was wondering what some basic >guidelines are for the location and orientation. I have a composite >fuselage with a metal tail. I was hoping to mount it inside the fuselage >somewhere but I don't have a plan yet. Any tips are appreciated. > >Happy Holidays, Gary K. If it were my airplane, I'd try for fuselage centerline with the shortest practical feedline. Many builders have reported successful operation with antennas inside a composite tailcone but common logic tells us there would be degraded performance due to shadowing and attenuation of the signal with surrounding materials. Bottom line is that you can try about anything and go to an alternative plan if ATC can't see you as well as you think they should. Bob . . . ________________________________________________________________________________
Date: Dec 26, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Avionics Master switches
> >Merry Christmas all! > >I just ran across this article on avionics master switches...It seems to >disagree with Bob's analysis of the need for them..and being one to stir the >pot..here it is: http://www.avweb.com/articles/avmaster.html > >I tend to believe they are unnecessary myself, liking Bob's logic....higher >parts count.. single point failure, etc.. > >Dave Leonard.. a man with a '72 Bellanca Viking with no avionics master.. Those articles are all over the place. I get one e-mailed to me several times a year. When I could find e-mail addresses, I've written a number of authors asking for specifics as to the magnitude and source of transients that exceed the capabilities of the radio to deal with it. Never had an answer from any one of them. The general flow of these articles is to first instill a lot of concern for the uncertainties based on divine revelation. For example, the article you cited says: "Your panel of state-of-the-art avionics might represent one-quarter or one-third of the total value of your (TRUE) aircraft. To invest this kind of money and not have proper protection doesn't make economic sense or even common sense." Hmmmm . . . I guess "protection" is a "common sense" issue, not a scientific issue. The article goes on to say: "You might think that you could just turn on and off the radios individually before and after starting the aircraft and wouldn't have a need for an avionics master switch, but that's only half-true. You may be able to turn on and off the navigation and communications equipment, but how about the intercom, fuel computer, glideslope receiver, marker beacon, altitude encoder, HSI, flight directorwell the list goes on. None of those units normally have an on-off switch. Their designers assume that the installing agency knows what they are doing and will provide spike protection." Here the author chooses to ignore or is completely ignorant of the fact that the "installing agency" has no responsibility whatsoever with respect to protecting any aircraft accessory from system gremlins real or imagined. The installer is obligated by regulation and ignorance to follow the instructions that come with the product. Our guardian angles with clubs are quick to bless installations in accordance with approved documentation . . . right or wrong. Any installer with the brass to do something original either faces an uphill battle to convince the "angels" that the science is correct and that the deviation is a good thing . . . when tradition and ignorance are so pervasive, why bother? These articles also fail to mention the hundreds of products with solid state innards that are routinely attached to the main bus of tens of thousands of airplanes and amassed millions of failure-free flight hours. It's easier to ignore the efforts of capable designers and chalk the apparent success up as "a universe of accidents looking for someplace to happen." Dr. Tom's credentials are impressive . . . he owns "one of the finest radio shops on the West Coast", has the blessings of the FAA for functioning as a DER and even earned a PhD in nuclear physics. . . . Hmmmmm . . . won't belabor the obvious question there. The article wraps up with: "If you have modern solid-state avionics (nav/comms, DME, GPS, fuel flow computer, etc.) then in my opinion an avionics master switch is a must. The few dollars you try to save by not installing one will return to haunt you in repair bills, guaranteed." Hmmm. . . "guaranteed" . . . These articles have been around for decades and they'll persist as along as there are consumers ready to buy into the advertising hype. They never contain any data or specifics as to the threats or weaknesses in the design of potential victims. As a sideline datapoint, I've been working with a number of folks at Raytheon who are considering the next generation glass cockpit products for inclusion into light aircraft. These systems are far more complex and potentially fragile than any piece of avionics produced to date . . . but all are tested to DO-160 to DEMONSTRATE an ability to withstand anything the airplane might throw at it . . and nature too. People have agonized for years about "spikes" from starter motors . . . you ought to see what we do to provide immunity from most effects of lightning. Now that's a SPIKE! Bob . . . ________________________________________________________________________________
Date: Dec 26, 2001
From: Gary Liming <gary(at)liming.org>
Subject: Re: Avionics Master switches
>To invest this kind of money and not have proper > protection doesn't make economic sense or even common sense." > > Hmmmm . . . I guess "protection" is a "common sense" issue, > not a scientific issue. The article goes on to say: Personally, I've always been suspect of arguments that invoke "common sense" or anything else you can't really define well - after all, it is common sense that tells you earth is flat! > People have agonized for years about "spikes" from starter > motors . . . you ought to see what we do to provide immunity > from most effects of lightning. Now that's a SPIKE! This one is interesting - I asked what can be done to protect against lightning strikes once before, and was promptly admonished not to fly into bad weather for an answer. Assuming my plane is out on the field at a tie-down, where it may spend the vast majority of its time, is there anything that can be done about the charge from a near miss? (I'm not even going to ask about a direct hit.) Gary Liming ________________________________________________________________________________
Date: Dec 26, 2001
From: Steve Kay <skay(at)optonline.net>
Subject: Re: Avionics Master switches
Never thought about that Gary. I might add a ground spike to my tie down. -Steve > This one is interesting - I asked what can be done to protect against > lightning strikes once before, and was promptly admonished not to fly into > bad weather for an answer. Assuming my plane is out on the field at a > tie-down, where it may spend the vast majority of its time, is there > anything that can be done about the charge from a near miss? (I'm not even > going to ask about a direct hit.) > > Gary Liming > ________________________________________________________________________________
Date: Dec 26, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: New pricing on 760VHF Transceiver & Xpndr Availability
> >OK, sold. So what's the latest on the XPNDR? (looking for the package deal!) > >Fom the PossumWorks in TN >Mark > >"Robert L. Nuckolls, III" wrote: > >> >> Check out the new pricing on the Microair 760VHF >> transceiver at http://www.aeroelectric.com/ >> >> Bob . . . >> The FAA is still chasing them around the paperwork mountain. Just checked with my distributor and they tell me they're going to ship my back-ordered T2000SFL transponders on Jan 04!!!!! We shall see what we shall see. I'll post a note on the AeroElectric List and on the website when I know it's a Done Deal. I think I have three transponders coming that are not spoken for. If the pricing hasn't changed since I placed the order, they'll sell for $1195. The prewired harness will be $55 . . . and like the VHF760, we'll eventually publish our own installation manual and diagrams. Bob . . . ________________________________________________________________________________
Date: Dec 26, 2001
Subject: Avionics Master switches
From: czechsix(at)juno.com
I read this article on avionics masters and sent an e-mail to the author asking if he could back up his conclusion with solid evidence. I'll let you guys know if I hear anything back. I gave him the web address to Lectric Bob's article on avionics master switches. I'd be interested to hear Bob's comments too... --Mark Navratil Cedar Rapids, Iowa RV-8A finish kit due to arrive this week if Roadway doesn't lose it somewhere..... _______ From: "David A. Leonard" <dleonar1(at)maine.rr.com> Subject: AeroElectric-List: Avionics Master switches Merry Christmas all! I just ran across this article on avionics master switches...It seems to disagree with Bob's analysis of the need for them..and being one to stir the pot..here it is: http://www.avweb.com/articles/avmaster.html I tend to believe they are unnecessarymyself, liking Bob's logic....higher parts count.. single point failure, etc.. Dave Leonard.. a man with a '72 Bellanca Viking with no avionics master.. ________________________________________________________________________________
Date: Dec 26, 2001
From: Gary Liming <gary(at)liming.org>
Subject: Re: New pricing on 760VHF Transceiver &
Xpndr Availability > I'll post a note on the AeroElectric List and > on the website when I know it's a Done Deal. I know Microair has a "panel" version of the 760 - one that looks like am ICOM A200, kind of. Do you know if it is functionally the same as the 2 1/4 inch round one? Do you carry it too, and if so, have a price? I think I would like the panel version because I am used to that format and would fumble with the switches less. Gary Liming ________________________________________________________________________________
Date: Dec 26, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Avionics Master switches
> > >I read this article on avionics masters and sent an e-mail to the author >asking if he could back up his conclusion with solid evidence. I'll let >you guys know if I hear anything back. I gave him the web address to >Lectric Bob's article on avionics master switches. I'd be interested to >hear Bob's comments too... already posted mine . . . I'm sure we're all interested in what the good doctor has to say. Bob . . . ________________________________________________________________________________
From: "Ned Thomas" <nthomas(at)mmcable.com>
Subject: Re: New pricing on 760VHF Transceiver & Xpndr Availability
Date: Dec 26, 2001
Bob, I am interested in the T2000SFL. Will the T2000SFL require an encoder? If so do you recommend any encoders to go with the T2000SFL? Thanks Ned > The FAA is still chasing them around the paperwork > mountain. Just checked with my distributor and they > tell me they're going to ship my back-ordered T2000SFL > transponders on Jan 04!!!!! We shall see what we shall > see. I'll post a note on the AeroElectric List and > on the website when I know it's a Done Deal. > > I think I have three transponders coming that are not > spoken for. If the pricing hasn't changed since I placed > the order, they'll sell for $1195. The prewired harness > will be $55 . . . and like the VHF760, we'll eventually > publish our own installation manual and diagrams. > > Bob . . . > > ________________________________________________________________________________
From: "John Anderson" <janderson412(at)hotmail.com>
Subject: Re: Transponder antenna location
Date: Dec 27, 2001
Upper or lower side of the fuse Bob? ----- Original Message ----- From: Robert L. Nuckolls, III Subject: AeroElectric-List: Re: Transponder antenna location lls(at)aeroelectric.com> > >I'm ready to mount a transponder antenna and I was wondering what some basic >guidelines are for the location and orientation. I have a composite >fuselage with a metal tail. I was hoping to mount it inside the fuselage >somewhere but I don't have a plan yet. Any tips are appreciated. > >Happy Holidays, Gary K. If it were my airplane, I'd try for fuselage centerline with the shortest practical feedline. Many builders have reported successful operation with antennas inside a composite tailcone but common logic tells us there would be degraded performance due to shadowing and attenuation of the signal with surrounding materials. Bottom line is that you can try about anything and go to an alternative plan if ATC can't see you as well as you think they should. Bob . . . = = = c-list = Get mor ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Avionics Master switches EGAD
Date: Dec 26, 2001
Bob: Bravo! Your latest tilt at the "Delightfully Bewildered" Doctor of atomic science is a masterpiece of contemplated logic........... It ranks with the Cessna Master Square and the Car Battery Care topics and has therefore taken its place in the front of my Construction Log with AC43.13 and assorted other Rules to Live by. Without your shared experience and willingness to deliver, we would all be the poorer. Best regards for 2002 - and Don't Give Up the Shippppp! Ferg diesel Europa A064 ________________________________________________________________________________
Date: Dec 27, 2001
Subject: Re: AeroElectric-List Digest: 12 Msgs - 12/26/01
From: Grant Corriveau <grantC(at)total.net>
on 12/27/01 02:51, AeroElectric-List Digest Server at aeroelectric-list-digest(at)matronics.com wrote: > Those articles are all over the place. I get one e-mailed ... > "Your panel of state-of-the-art avionics FWIW - just as a sidebar - the ole' reliable 727 did indeed have avionics masters installed. Our company routinely kept those in the 'ON' position. The brand new state-of-the-art A320 with more avionics and computers than anyone can count, doesn't have any avionics master switches. I don't know what sort of electrical spikes are caused when the generators kick in during engine start (at about 53% of N1 rotation speed, the generator suddenly assumes the full load of the electrical busses), but the mechanical jolt is violent enough to actually make the engine pods shake, and the impact can be felt in the flight deck! And I couldn't count the number of times a year that the electrical system bounces around from engine-generator power, to Auxiallary-gen power, to ground power, to nothing (the worst case is when the ground plug falls out of the socket 2 minutes before pushback and everything suddenly goes black - then someone hurredly plugs it back in and all the lights and bells and whistles come on doing self-tests while the pilots frantically fumble through the flight computer pages to ensure that none of the data has been lost or corrupted!!! joy oh joy!). All without any 'master switch' protection at all. -- Grant Corriveau Montreal Zodiac 601hds/CAM100 C-GHTF www.theWingStayedON.ca ________________________________________________________________________________
Date: Dec 27, 2001
Subject: 'Lectric Bob fuseblocks...good service
From: Grant Corriveau <grantC(at)total.net>
>> I just ran across this article on avionics master switches...It seems to >> disagree with Bob's analysis of the need for them.. While on the topic of some of the innovative ideas encouraged by the Aeroelectric manual, let me provide an update regarding my fuseblocks. I utilized the automotive style fuseblocks as suggested in Bob's book - One 20 terminal unit for the main bus, a 10 terminal unit for my essential bus, and a 6 terminal unit for my engine/ignition bus. These are conveniently located on the outboard side panels, freeing up valuable instrument panel space. The only snag I had was that first the 10-slot unit, then the 6-slot unit revealed a loosening in the grip on the fuse in the top right hand slot, resulting in an intermittant circuit. I want to emphasize that this is the only problem that I've had - all the other slots on all the other units are working just fine. I have eliminated the possibility that I may have somehow kicked them getting in and out of the aircraft (they are well protected by their position). When I change them, I will re-examine the installation technique to see if there is any way that I did something to cause the problem - I can't see how.... but (another thing I will investigate is whether my 'generic' fuses have the same terminal gauge as original manufacturers equipment?) Anyways, the convenience of this unit was displayed in the short-term solution, which was to merely switch the faulty circuit to the next available slot for the time being. And in my 'winter works' project, I will merely have to unbolt the fuseblock itself and drop in the new unit. Here's where the good service comes in. As soon as I had advised Bob Nuckolls of the problem a replacement unit appeared in the mail, along with a request that I return the defective unit for investigation. That's great service! I'll post more later on as required - just wanted to give 'kuddos' where due. All the best in '02, -- Grant Corriveau Montreal Zodiac 601hds/CAM100 C-GHTF www.theWingStayedON.ca ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Lightning and ground spikes
Date: Dec 26, 2001
"Never thought about that Gary. I might add a ground spike to my tie down. -Steve" Steve: Not in a million years...... the whole idea of lightning protection is to induce the strike in an Alternative path - not the one you're trying to protect. The aircraft is best protected by lettijng it 'float' between positive and negative fields and intriguing the tendrils 'feeling' for the alternative route to go elsewhere. Then the aircraft will not be nearly so 'attractive' a route. So mebbe a post twenty feet away, well grounded and sharp at the top would induce the feelers to it. Then if a strike occurs (or even a preemptive one) it will mean only cleaning tiny spots of molten steel off the 'plane. Regards, Ferg A064 P.S: There is still (I hope) an superb account of the destruction of a composite aircraft in Southern UK on the Brit AAIB list. The discussion of the pica-minute by pica-minute travel of the lightning is an education........... ________________________________________________________________________________
Date: Dec 27, 2001
From: Steve Kay <skay(at)optonline.net>
Subject: Re: Lightning and ground spikes
Fergus Kyle wrote: > > "Never thought about that Gary. I might add a ground spike to my tie > down. -Steve" > > Steve: > Not in a million years...... the whole idea of lightning > protection is to induce the strike in an Alternative path - not the one > you're trying to protect. Got it... I was thinking in terms of the avionics and directing the path "around" them by using the skin of the airframe. I must admit, I've seen buildings and there wiring fried by lightning while the nice shinning apd aluminum Grumman step van along side was not touched! -Steve ________________________________________________________________________________
Date: Dec 27, 2001
From: Miller Robert <rmiller3(at)earthlink.net>
Subject: Re: AeroElectric-List Digest: 12 Msgs - 12/26/01
> All without any 'master switch' protection at all. > Yes... but do you know what protection circuits are built into the electrical system, and into each box in the avionics, that are not controlled by the crew? The system may well be protected in a variety of ways, both voltage and thermal, invisible to the crew. Robert Grant Corriveau wrote: > > on 12/27/01 02:51, AeroElectric-List Digest Server at > aeroelectric-list-digest(at)matronics.com wrote: > > > Those articles are all over the place. I get one e-mailed > ... > > "Your panel of state-of-the-art avionics > > FWIW - just as a sidebar - the ole' reliable 727 did indeed have avionics > masters installed. Our company routinely kept those in the 'ON' position. > > The brand new state-of-the-art A320 with more avionics and computers than > anyone can count, doesn't have any avionics master switches. I don't know > what sort of electrical spikes are caused when the generators kick in during > engine start (at about 53% of N1 rotation speed, the generator suddenly > assumes the full load of the electrical busses), but the mechanical jolt is > violent enough to actually make the engine pods shake, and the impact can be > felt in the flight deck! And I couldn't count the number of times a year > that the electrical system bounces around from engine-generator power, to > Auxiallary-gen power, to ground power, to nothing (the worst case is when > the ground plug falls out of the socket 2 minutes before pushback and > everything suddenly goes black - then someone hurredly plugs it back in and > all the lights and bells and whistles come on doing self-tests while the > pilots frantically fumble through the flight computer pages to ensure that > none of the data has been lost or corrupted!!! joy oh joy!). > > All without any 'master switch' protection at all. > > -- > Grant Corriveau > Montreal > Zodiac 601hds/CAM100 > C-GHTF > www.theWingStayedON.ca > ________________________________________________________________________________
From: "David Swartzendruber" <dswartzendruber(at)earthlink.net>
Subject: 'Lectric Bob fuseblocks...good service
Date: Dec 27, 2001
Bussman has evidently had some issues with the fuse not being held tightly enough for some applications because they now,(a couple of years ago), offer a version of the fuse block with greater grip on the fuse. They do this by putting little spring steel clips over the fingers that grip the fuses. The resulting fuse block was somewhat more pricey, and this info is a couple years old, so I'm not sure if they still offer it. I don't have any service experience with the enhanced fuseblocks because the solution to the issue I'm remembering was to replace the fuseblock with some circuit breakers. Bob, have you seen one of the fuseblocks with these little clips? David Swartzendruber Wichita > > > While on the topic of some of the innovative ideas encouraged > by the Aeroelectric manual, let me provide an update > regarding my fuseblocks. > > I utilized the automotive style fuseblocks as suggested in > Bob's book - One 20 terminal unit for the main bus, a 10 > terminal unit for my essential bus, and a 6 terminal unit for > my engine/ignition bus. These are conveniently located on the > outboard side panels, freeing up valuable instrument panel space. > > The only snag I had was that first the 10-slot unit, then the > 6-slot unit revealed a loosening in the grip on the fuse in > the top right hand slot, resulting in an intermittent circuit. > > I want to emphasize that this is the only problem that I've > had - all the other slots on all the other units are working > just fine. > > I have eliminated the possibility that I may have somehow > kicked them getting in and out of the aircraft (they are well > protected by their position). When I change them, I will > re-examine the installation technique to see if there is any > way that I did something to cause the problem - I can't see > how.... but (another thing I will investigate is whether my > 'generic' fuses have the same terminal gauge as original manufacturers > equipment?) > > Anyways, the convenience of this unit was displayed in the > short-term solution, which was to merely switch the faulty > circuit to the next available slot for the time being. And > in my 'winter works' project, I will merely have to unbolt > the fuseblock itself and drop in the new unit. > > Here's where the good service comes in. As soon as I had > advised Bob Nuckolls of the problem a replacement unit > appeared in the mail, along with a request that I return the > defective unit for investigation. That's great service! > > I'll post more later on as required - just wanted to give > 'kuddos' where due. > > All the best in '02, > > -- > Grant Corriveau > Montreal > Zodiac 601hds/CAM100 > C-GHTF > www.theWingStayedON.ca > ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: Lightning and ground spikes
Date: Dec 27, 2001
Fergus Kyle wrote: > > "Never thought about that Gary. I might add a ground spike to my tie > down. -Steve" > > Steve: > Not in a million years...... the whole idea of lightning > protection is to induce the strike in an Alternative path - not the one *** If I was running an airport in a lightning-prone area, I might provide a "lightning tower" - just a tall steel pole. So lightning would tend to hit the tower in preference to the airplanes. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 27, 2001
From: Jim Duckett <perfeng(at)3rivers.net>
Subject: Transponder
Bob, I was on the Microair web site the other night and see that they are waiting for TSO cert.(still) before they release their transponder for sale. Any idea when you'll be getting any? With their time table staement last year of "a couple of months", it should only take me 10 minutes or so to finish my 7. Just wondering...won't be working on the panel for another few minutes... Jim Duckett, RV-7A ________________________________________________________________________________
Date: Dec 27, 2001
From: Steve Kay <skay(at)optonline.net>
Subject: Re: Lightning and ground spikes
Thats because you're an aircraft owner...not an airport owner... -Steve jerry(at)tr2.com wrote: > > Fergus Kyle wrote: > > > > "Never thought about that Gary. I might add a ground spike to my tie > > down. -Steve" > > > > Steve: > > Not in a million years...... the whole idea of lightning > > protection is to induce the strike in an Alternative path - not the one > > *** If I was running an airport in a lightning-prone area, I might provide a > "lightning tower" - just a tall steel pole. So lightning would tend to > hit the tower in preference to the airplanes. > > - Jerry Kaidor ( jerry(at)tr2.com ) > ________________________________________________________________________________
From: BAKEROCB(at)aol.com
Date: Dec 27, 2001
Subject: spike catching diodes
12/27/01 Hello Bob, I'd like to try again on this subject. Please see my previous post below. Many thanks. 'OC' Subj: spike catching diodes Date: 12/18/2001 In a message dated 12/18/2001 2:52:36 AM Eastern Standard Time, aeroelectric-list- writes: <<....skip.... Go to http://www.aeroelectric.com and click on link to Article Reprints and Newsgroup Treads. On the next page, find and click on "An illustrated discussion about spike catching diodes and how they work.".....skip..... >> 12/18/01 Hello Bob, Thanks for your testing and detailed write up on this subject. But I'm still left with some very simple layman's questions / doubts. The diagram on page 212 of Tony Bingelis' book Firewall Forward provides a basis for discussion / questions. 1) Does the diode always get installed so that it provides a connection between the solenoid switch terminal and some other part of the circuit? 2) Does it matter which other part of the circuit that the diode connection goes to? I see on Tony's diagram that the diode connection is made to the plus or input side of the relay. I see that on your sketch you show the diode connection going to ground. Which is correct / better? 3) When diagramming this diode connection which is the proper direction for the diode triangle to be pointing? I see on Tony's diagram that the diode triangle has the base connected to the solenoid switch terminal. I see on your sketch that you have the point of the diode triangle connected to the solenoid switch terminal (and the base of the triangle connected to ground). 4) When the switch has been closed for some time is there supposed to be any current flow through the diode? 5) Which way is the current from the collapsing coil field supposed to flow through the diode when the switch is opened? In the direction that the diode triangle is pointing or opposite to the direction the diode triangle is pointing? 6) When one has a diode in hand how can one tell by looking at its markings which end the triangle is pointing towards? Many thanks for your help. 'OC' Baker, Builder of KIS TR-1 #116 4/14/97 - ?/?/? ________________________________________________________________________________
Date: Dec 27, 2001
Subject: Re: Avionics Master switches
From: b green <rvinfo(at)juno.com>
An exerpt from my BENDIX/KING KX 125 Instalation manual: CAUTION THE KX 125 SHOULD ONLY BE TURNED ON AFTER ENGINE STARTUP. THIS IS A SIMPLE PRECAUTION WHICH HELPS PROTECT THE SOLID STATE CIRCITRY AND EXTENDS THE OPERATING LIFE OF YOUR AVIONICS EQUIPMENT. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> writes: > > > > > > >Merry Christmas all! > > > >I just ran across this article on avionics master switches...It > seems to > >disagree with Bob's analysis of the need for them..and being one to > stir the > >pot..here it is: http://www.avweb.com/articles/avmaster.html > > > >I tend to believe they are unnecessary myself, liking Bob's > logic....higher > >parts count.. single point failure, etc.. > > > >Dave Leonard.. a man with a '72 Bellanca Viking with no avionics > master.. > > Those articles are all over the place. I get one e-mailed > to me several times a year. When I could find e-mail addresses, > I've written a number of authors asking for specifics as to > the magnitude and source of transients that exceed the > capabilities of the radio to deal with it. Never had an > answer from any one of them. The general flow of these > articles is to first instill a lot of concern for the > uncertainties based on divine revelation. For example, > the article you cited says: > > "Your panel of state-of-the-art avionics might represent > one-quarter or one-third of the total value of your (TRUE) > aircraft. To invest this kind of money and not have proper > protection doesn't make economic sense or even common sense." > > Hmmmm . . . I guess "protection" is a "common sense" issue, > not a scientific issue. The article goes on to say: > > "You might think that you could just turn on and off the > radios individually before and after starting the aircraft > and wouldn't have a need for an avionics master switch, > but that's only half-true. You may be able to turn on and > off the navigation and communications equipment, but how > about the intercom, fuel computer, glideslope receiver, > marker beacon, altitude encoder, HSI, flight directorwell > the list goes on. None of those units normally have an > on-off switch. Their designers assume that the installing > agency knows what they are doing and will provide spike > protection." > > Here the author chooses to ignore or is completely ignorant > of the fact that the "installing agency" has no responsibility > whatsoever with respect to protecting any aircraft accessory > from system gremlins real or imagined. The installer is > obligated by regulation and ignorance to follow the instructions > that come with the product. Our guardian angles with clubs > are quick to bless installations in accordance with approved > documentation . . . right or wrong. Any installer with the > brass to do something original either faces an uphill battle > to convince the "angels" that the science is correct and that > the deviation is a good thing . . . when tradition and > ignorance are so pervasive, why bother? > > These articles also fail to mention the hundreds of > products with solid state innards that are routinely > attached to the main bus of tens of thousands of airplanes > and amassed millions of failure-free flight hours. > It's easier to ignore the efforts of capable designers > and chalk the apparent success up as "a universe of > accidents looking for someplace to happen." > > Dr. Tom's credentials are impressive . . . he owns > "one of the finest radio shops on the West Coast", has > the blessings of the FAA for functioning as a DER and > even earned a PhD in nuclear physics. . . . Hmmmmm . . . won't > belabor the obvious question there. > > The article wraps up with: > > "If you have modern solid-state avionics (nav/comms, DME, GPS, > fuel flow computer, etc.) then in my opinion an avionics > master switch is a must. The few dollars you try to save by not > installing one will return to haunt you in repair bills, > guaranteed." > > Hmmm. . . "guaranteed" . . . These articles have been around > for decades and they'll persist as along as there are consumers > ready to buy into the advertising hype. They never contain any > data or specifics as to the threats or weaknesses in the design > of potential victims. > > As a sideline datapoint, I've been working with a number of > folks at Raytheon who are considering the next generation > glass cockpit products for inclusion into light aircraft. > These systems are far more complex and potentially fragile > than any piece of avionics produced to date . . . but all > are tested to DO-160 to DEMONSTRATE an ability to withstand > anything the airplane might throw at it . . and nature too. > People have agonized for years about "spikes" from starter > motors . . . you ought to see what we do to provide immunity > from most effects of lightning. Now that's a SPIKE! > > > Bob . . . > > > > > messages. > > > > > > ________________________________________________________________________________
From: "Paul Messinger" <paulm(at)tenforward.com>
Subject: Re: Avionics Master switches
Date: Dec 27, 2001
I might point out that IF you follow ALL the electrical design suggestions that Bob recommends AND have equipment that was DESIGNED to current 160 requirements you need not worry about electrical damage. However I have some electronics from major mfgrs that was manufactured in 1999 (designed years before that)that does not meet 160. Further some appear to not have suitable protection for devices across the input bus that are rated for 18V max. Those with spam cans that have older electronics and factory stock electrical charging systems should use consider the use of an avionics master and/or turn off everything during starting and shutdown. The origins of the ""requirement"" for avionics master switches is not clear. However FBO's found that they had fewer equipment problems in the 50"s and 60" with rental acft if there was a avionics master and if it was used. Personally I like a single switch for power control and have a second one in the very unlikely event of failure. This is a personal preference not due to worrys. I have included proper spike transient supression at the source in my acft similar to what Bob suggests and use the Avionics master for personal choice only. My conclusion is that a properly designed electrical system does not need the additional cautions of avionics off during start up and shutdown. However I have yet to see a spam can built before 1990 that had a good electrical design. Paul Messinger EAA tech Con. Electronics engineer. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of b green Subject: Re: AeroElectric-List: Re: Avionics Master switches An exerpt from my BENDIX/KING KX 125 Instalation manual: CAUTION THE KX 125 SHOULD ONLY BE TURNED ON AFTER ENGINE STARTUP. THIS IS A SIMPLE PRECAUTION WHICH HELPS PROTECT THE SOLID STATE CIRCITRY AND EXTENDS THE OPERATING LIFE OF YOUR AVIONICS EQUIPMENT. ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Dec 27, 2001
Subject: RC Allen Wiring
Bob: I am trying to wire my RC Allen electric AI & DG. The plug that fits the back of the instrument has me a little confused. Nothing came with the instruments so I ordered the plugs from Gulf Coast. Nothing then came with the plugs and I don't know how to wire or operate these plugs. They are parts number MS90376-12R. It also says Caplugs EC-12. Can you help me? Len Leggette RV-8A N901LL (res) Greensboro, N.C. Hanger # 23 at INT ________________________________________________________________________________
Date: Dec 27, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Instrument panel planning - please comment
Hello listers, This evening, I worked on the design of my instrucment panel and I completed two different models. I would like to have your assistance to debug the panel for any important missing things or any usability issue. Please notice that while I reserved space for a DG and an AH, these flight instruments will not be installed initially. I also reserved a space for additional 2-1/4" gauges. Most circuits will be protected with fuse blocs from Aeroelectrics. I want to have a dual-battery electrical system and dual ignition for a carburated EA-81 installation. The Comm is an Apollo SL-40 with integrated VOX intercom. The transponder will be a 2-1/4" device (when one is available) :-) The ventilation is assured with Van's Aircraft vents system. For cabin heat, I picked up a method on this list that I think is very simple. I will have a cabin header radiator backed with computer fans (activated with on-off switch and a dimmer). I will operate three facet fuel pumps... one at each leading edge fuel tank and an additional one for emergency use. The EIS is the Advanced EIS for water cooled engine (from Grand-Rapid). It monitors EGT, water temp, water pressure, fuel pressure, oil temp, oil pressure, OAT, engine hours, CHT, dc voltage. Current loading will be monitored separately with an ammeter. If you foresee any bugs with this setup, please let me know before I cut the panel. http://mthobby.pcperfect.com/ch601/images/Dec27-1.JPG http://mthobby.pcperfect.com/ch601/images/Dec27-2.JPG Thank! Michel PS: please let me know if this is off-topic for this list. ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Avionics Cooling Hose
Date: Dec 27, 2001
Hello, Can anybody tell me - what is the exact correct type and size of hose for cooling radios? You know, the kind that goes into the cooling port on the back of the radio? Thanks in advance, - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
From: "John Harlow" <jharlow(at)onearrow.net>
Subject: Re: Instrument panel planning - please comment
Date: Dec 28, 2001
A few quick thoughts. Can't answer if this is off topic for this group or not, but I do have some comments on your design. As a two place A/C the throttle should in the center so both pilots can reach it ( I see you have two shown). The layout of the flight instruments in 2.JPG is the better choice but I would move it further left so the AH and DG or more in the center of vision. I installed the Control Vision exp buss http://www.controlvision.com/frame.cfm?link=avionics.htm which made the wiring job easier and took up less panel space. Also don't forget a vacuum gage. ________________________________________________________________________________
Date: Dec 28, 2001
Subject: Panel arrangement
From: Grant Corriveau <grantC(at)total.net>
on 12/28/01 02:51, AeroElectric-List Digest Server at aeroelectric-list-digest(at)matronics.com wrote: > From: Michel Therrien <mtherr(at)yahoo.com> > Subject: AeroElectric-List: Instrument panel planning - please comment > > > Hello listers, > > This evening, I worked on the design of my instrucment > panel and I completed two different models. I would Michel, The second version with the regular 6 instruments front and center is a more conventional setup and will allow for easier transitioning with other aircraft/other pilots. This setup was agreed to by all the major manufacturers many years ago as 'the best' overall way to scan the instruments in instrument flying. If you are delaying the gyros, then I would temporarily relocate the ALT/VSI to the center column, and blank out the other two for now. In your other diagram (.1 I think), where you have the AH & DG top and center I would recommend the following. Initially set it up just as you have drawn, leaving your gyro holes blanked off. But later when you add the gyros, relocate them to the two center holes where they will be most visible. Swap the AH and ALT positions and the DG and VSI positions, and then you will almost have the 'recommended' setup - just the VSI (the least important of all) will be out of place. (But still next to the Altimeter, so not too bad actually). So, either one can work quite well I think. Happy cutting, -- Grant Corriveau Montreal Zodiac 601hds/CAM100 C-GHTF www.theWingStayedON.ca ________________________________________________________________________________
Date: Dec 28, 2001
From: David Mullins <n323xl(at)mediaone.net>
Subject: Re: Instrument panel planning - please comment
Michel, After looking over your two layouts, This is what I can find: 1: Layout #1 does not have a standard flight instrument scan. If you've flown other aircraft or will, it will be to your benefit to keep this as a standard layout. 2: The layout of the switches and other controls seems to be a little hap-hazard by placing them where there was space available. 3: The layout of panel #2 is starting to look better but it is missing a MAG compass. 4: The switch positions are getting better, plus no more than 5 in a row. There are still some just put where there is space. 5: If this is a single or tandem panel, why do you have two throttles? 6: I believe that the EIS system has all your alarms for Oil Pressure, Oil Temp, ALT, Voltage, etc. That is why I only found one enunciator light or buzzer (Idiot light for you shadetree mechanics) 7: The VSI does not need the extra cutout in the panel. Mine adjusted through the lower left screw hole. The Altimeter does need it. The Artificial Horizon may need one for the caging feature. I took your two photos and put together a layout as a guide for you. That file is attached. You will get it, but I don't think the list will. Are you drawing this in CAD, Panel Planner or something else? You can check out the panel for my KR2S at: Http://n323xl.iwarp.com/panel1.htm I laid my panel out in Turbocad V7 and had the resultant file sent to a waterjet cutter. I saved a lot of time and frustration by doing it this way. It also did not cost that much to have done. Triple check all your dimensions before sending the file out. You only want to do this once. Dave Mullins Nashua, New Hampshire http://n323xl.iwarp.com Michel Therrien wrote: > > Hello listers, > > This evening, I worked on the design of my instrucment > panel and I completed two different models. I would > like to have your assistance to debug the panel for > any important missing things or any usability issue. > > Please notice that while I reserved space for a DG and > an AH, these flight instruments will not be installed > initially. I also reserved a space for additional > 2-1/4" gauges. > > Most circuits will be protected with fuse blocs from > Aeroelectrics. > > I want to have a dual-battery electrical system and > dual ignition for a carburated EA-81 installation. > > The Comm is an Apollo SL-40 with integrated VOX > intercom. The transponder will be a 2-1/4" device > (when one is available) :-) > > The ventilation is assured with Van's Aircraft vents > system. > > For cabin heat, I picked up a method on this list that > I think is very simple. I will have a cabin header > radiator backed with computer fans (activated with > on-off switch and a dimmer). > > I will operate three facet fuel pumps... one at each > leading edge fuel tank and an additional one for > emergency use. > > The EIS is the Advanced EIS for water cooled engine > (from Grand-Rapid). It monitors EGT, water temp, > water pressure, fuel pressure, oil temp, oil pressure, > OAT, engine hours, CHT, dc voltage. Current loading > will be monitored separately with an ammeter. > > If you foresee any bugs with this setup, please let me > know before I cut the panel. > > http://mthobby.pcperfect.com/ch601/images/Dec27-1.JPG > > http://mthobby.pcperfect.com/ch601/images/Dec27-2.JPG > > Thank! > > Michel > PS: please let me know if this is off-topic for this > list. > > ===== > ---------------------------- > Michel Therrien CH601-HD > http://pages.infinit.net/mthobby > http://mthobby.pcperfect.com/ch601 > > Send your FREE holiday greetings online! > http://greetings.yahoo.com > ________________________________________________________________________________
Date: Dec 28, 2001
From: David Mullins <n323xl(at)mediaone.net>
Subject: Re: Instrument panel planning - please comment
Sorry, the link to my instrument panel pages is: http://n323xl.iwarp.com/blpanel1.htm Dave Mullins Nashua, New Hampshire http://n323xl.iwarp.com ________________________________________________________________________________
Date: Dec 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Instrument panel planning - please comment
See below: --- John Harlow wrote: > As a two place A/C the throttle should in the center > so both pilots can > reach it ( I see you have two shown). In a CH601, there is only one control stick in the center... that's why there are two throttle controls, one on each side. > The layout of > the flight instruments > in 2.JPG is the better choice but I would move it > further left so the AH and > DG or more in the center of vision. I'll explore that a little more... What limits me is the height of the panel. When it starts to curve down, I rapidly loose space and it forces me to revert to the first design. > I installed the Control Vision exp buss > http://www.controlvision.com/frame.cfm?link=avionics.htm > which made the > wiring job easier and took up less panel space. > Also don't forget a vacuum gage. I'll look into this. Thanks! Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
Date: Dec 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Instrument panel planning - please comment
Good feedback David! --- David Mullins wrote: > 1: Layout #1 does not have a standard flight > instrument scan. I got that comment from someonelse as well who is an airline pilot... > 2: The layout of the switches and other controls > seems to be > a little hap-hazard by placing them where there > was space > available. This is almost right. I tried to group them so I have the sensitive switches together (fuel pumps for instance) and the lights switches together. These details are hard to see and you'd probably need my CAD file to see them more clearly. > 3: The layout of panel #2 is starting to look better > but it is missing > a MAG compass. With this setup, the compass would be on top of the panel... not inside the panel. > 5: If this is a single or tandem panel, why do you > have two throttles? Because the control stick is between the seats (this is a Zenair CH601). > 6: I believe that the EIS system has all your alarms > for Oil Pressure, > Oil Temp, ALT, Voltage, etc. That is why I only > found one > enunciator light or buzzer (Idiot light for you > shadetree mechanics) I'm also thinking about using illuminated switches which would show when they are turned on. These are cheap switches found in local electronics surplus stores. They are rated for 20 amps at 12v. Any good or bad comments about these switches would be appreciated. > 7: The VSI does not need the extra cutout in the > panel. Mine adjusted > through the lower left screw hole. I'm planning for the same thing... actually, I started from another CAD file which had this cutout... I added the position for the hole and I will only drill that hole, not the cutout. > The Artificial Horizon may need one for the > caging feature. Thanks! > I took your two photos and put together a layout as > a guide for > you. That file is attached. You will get it, but I > don't think the list will. > Are you drawing this in CAD, Panel Planner or > something else? I'm using Autocad Lite. I can make the dwf file available. > You can check out the panel for my KR2S at: > > Http://n323xl.iwarp.com/panel1.htm I'll look at your page later today... > file sent to a waterjet cutter. I saved a lot of Good tip.... how can I find such a place? Thank you very much for taking time to provide that information! Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
Date: Dec 28, 2001
Subject: Re: Instrument panel planning - please comment
From: <racker(at)rmci.net>
> http://www.controlvision.com/frame.cfm?link=avionics.htm >> which made the >> wiring job easier and took up less panel space.> > I'll look into this. > > Thanks! > > Michel Michel, I researched the Controlvision offerings carefully (using the Aeroconnection and RV-List archives) before deciding to instead use Bob's fuseblock arrangement. My research concluded (all IMHO only): 1) This device adds lots of extra parts to perform the simple task of wire overcurrent protection (which in turn may/probably reduces reliability). The fuseblock arrangement is a simple wire/switch/fuse arrangement. 2) The unit cannot handle high current devices, which then requires the installation of traditional buss bars or fuseblocks anyway. Why have two completely different current protection methods when one will do the whole job for far cheaper? 3) If the Controlvision fails in the field, you are stuck. Switches/fuses can be had at any auto parts store so you can get back airborne again quickly. 4) The unit has an avionics master function, which is a designed in single point failure. Its not good for your entire avionics stack to go down all at once . 5) As for saving panel space, this unit actually uses *more* space than toggle switches (which are smaller both in height and depth). Rob Acker (RV-6). ________________________________________________________________________________
From: "David A. Leonard" <dleonar1(at)maine.rr.com>
Subject: Re: AeroElectric-List Digest: 18 Msgs - 12/27/01
Date: Dec 28, 2001
Hey all, this just in from the author of the Avionics master switch article at Avionics West. I asked him what his reaction to our groups' discussion on master switches.., and directed himto Bob's article on masters.. This was his response to me, which was timely, but still reflects an opinion, rather than citing a standard or a research paper. David, In my opinion an avionics master switch is a must. In fact, some of the installation manuals require an avionics master switch to be installed. Without it, the installation would be illegal. Do you know of any aircraft purchased today that does not have an avionics master switch? Cheers, tom Seems like more of the "common sense" with no science approach to me. Dave Leonard ________________________________________________________________________________
From: "iflych2" <iflych2(at)home.com>
Subject: Re: Instrument panel planning - please comment
Date: Dec 28, 2001
"I'm also thinking about using illuminated switches which would show when they are turned on. These are cheap switches found in local electronics surplus stores. They are rated for 20 amps at 12v." You might want to try these under low light conditions before making your decision. They can be very distracting. N571RS ________________________________________________________________________________
Date: Dec 28, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Avionics Master switches
> >An exerpt from my BENDIX/KING KX 125 Instalation manual: > > CAUTION > >THE KX 125 SHOULD ONLY BE TURNED ON AFTER ENGINE STARTUP. THIS IS A >SIMPLE PRECAUTION WHICH HELPS PROTECT THE SOLID STATE CIRCITRY AND >EXTENDS THE OPERATING LIFE OF YOUR AVIONICS EQUIPMENT. Yup . . . saw that too . . . saw similar paragraphs in manuals from Narco, Terra and Genave. Called all of those folks and asked to talk to the person who would know about the technical validity of that note. In no case could anyone identify the potential source, triggering event or magnitude of a potential hazard to the product. ALL products offered DO-160 certification as a feature of their product's capabilities. The last question was "why is the note there?" . . . "Uh . . . dunno, let me get back to you on that." I've asked this question about 10 times in the past 10 years. About half really did bother to call back to admit, "well, gee . . . we've been saying that for years and nobody has ever considered whether or not it was valid." . . . whereupon I asked, "Then if a radio comes back on warranty and parts failed were even remotely vulnerable to stresses from the ship's power, would you void the warranty?" "Hmmmm . . . I guess not." "Okay, then what you're telling me is that if a radio comes in with failed components and you don't know if the radio was ON or OFF during engine cranking, then you won't automatically assume that it was ON and tell the owner he screwed up and killed his radio?" "We'd have no basis for making such a claim." Obviously, this is not a transcript of the conversation but I think my paraphrasing is accurate. Nobody I've talked to was able to offer a scientific explanation to substantiate the statement that still appears in many manuals. Bob . . . ________________________________________________________________________________
Date: Dec 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Panel arrangement
Thank you Grant for your feedback! See below: --- Grant Corriveau wrote: > The second version with the regular 6 instruments > front and center is a more OK...with all the feedback I got, I'll work on this one from now on. > If you are delaying the gyros, then I would > temporarily relocate the ALT/VSI > to the center column, and blank out the other two > for now. That's my intention and I would put a hand held GPS on the left side. Would you know if there are things to avoid? What needs to be far from a compass? Or from a radio? Thanks and I wish you a happy year 2002! Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
From: "Ned Thomas" <nthomas(at)mmcable.com>
Subject: Re: AeroElectric-List Digest: 18 Msgs - 12/27/01
Date: Dec 28, 2001
My 1976 Grumman Tiger was not equipped with a master switch from the factory. I have had no problems. ----- Original Message ----- From: "David A. Leonard" <dleonar1(at)maine.rr.com> Subject: AeroElectric-List: Re: AeroElectric-List Digest: 18 Msgs - 12/27/01 > > Hey all, this just in from the author of the Avionics master switch article > at Avionics West. > > I asked him what his reaction to our groups' discussion on master > switches.., and directed himto Bob's article on masters.. > > This was his response to me, which was timely, but still reflects an > opinion, rather than citing a standard or a research paper. > > > David, > > In my opinion an avionics master switch is a must. In fact, some of the > installation manuals require an avionics master switch to be installed. > Without it, the installation would be illegal. Do you know of any aircraft > purchased today that does not have an avionics master switch? > > Cheers, > tom > > Seems like more of the "common sense" with no science approach to me. > > Dave Leonard > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
Date: Dec 28, 2001
From: Gary Liming <gary(at)liming.org>
Subject: DG replacement
With the advent of the cheap $100-150 GPS from Walmart, etc. and an $80 external antenna, what is wrong with the idea of finding one that can be mounted in the panel, and dedicated with the compass rose and heading screen on full time, and replacing it with the DG? This would be in addition to any other GPS navaid. Can GPS antennas be easily attached to two units, as in a simple "y" harness, or are two antennas a must? Also, If some of the coming $1000 electronic Artificial Horizon units turn out well, you don't need a vacuum pump anymore, making this price competitive with the vacuum instruments. (I am assuming an essential bus arrangement or even a separate battery back up for it.) Gary Liming ________________________________________________________________________________
Date: Dec 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Instrument panel planning - please comment
Good comment! I just checked and yes, in daylight situation it is nice, but at night, I would not need any other cabin light and that would be bothersome. I then checked how much current a bulb uses. It takes 0.039 amp at 12.38 volts for a wattage of 0.48 watts. So, for the 10 bulbs, we're talking about 5 watts. If I want to dim them off, I cannot use an ordinary dimmer as what I want to control is not the +12v, but rather the return to the ground. I saw resistors that are rated 10 watts that seems to be casted in a heatsink (RCD resistors TYPE 175 as an example). How much heat would such resistors generate at 5 watts? Would this be an appropriate solution to dim the light for night flying? Under this scenario, the instrument lighting switch would be a dpdt switch and would on one pole control power to the dimmer for instrument lights and the other pole would control the return path to the ground from the lighted switches (either direct or through resistor). Please advise on that. --- iflych2 wrote: > > > "I'm also thinking about using illuminated switches > which would show when they are turned on. These are > cheap switches found in local electronics surplus > stores. They are rated for 20 amps at 12v." > > You might want to try these under low light > conditions before making your > decision. They can be very distracting. > N571RS > > ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
Date: Dec 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: DG replacement
The only thing wrong with using a GPS or another electronic toy instead of a DG is regulatory requirements... Even though a GPS will not drift and need reajustment every 10 minutes, it is not considered as being acceptable by our regulatory agency (Transport Canada). For night flying, I need to have on board either a Directional Gyroscope or a Stabilized Magnetic Compass. When asking what a Stabilized Magnetic Compass is, I could not get any answer. One of my friend, tried harder than me and succeeded to speak with one of the team members that wrote the regulation... it is some sort of a remote gyro. Michel --- Gary Liming wrote: > > > > With the advent of the cheap $100-150 GPS from > Walmart, etc. and an $80 > external antenna, what is wrong with the idea of > finding one that can be > mounted in the panel, and dedicated with the compass > rose and heading > screen on full time, and replacing it with the DG? > This would be in > addition to any other GPS navaid. > > Can GPS antennas be easily attached to two units, as > in a simple "y" > harness, or are two antennas a must? > > Also, If some of the coming $1000 electronic > Artificial Horizon units turn > out well, you don't need a vacuum pump anymore, > making this price > competitive with the vacuum instruments. (I am > assuming an essential bus > arrangement or even a separate battery back up for > it.) > > Gary Liming > > > > Forum - > Contributions of > any other form > > latest messages. > other List members. > > aeroelectric-list(at)matronics.com > http://www.matronics.com/subscription > http://www.matronics.com/photoshare > http://www.matronics.com/browselist/aeroelectric-list > http://www.matronics.com/search > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > > > > ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://mthobby.pcperfect.com/ch601 Send your FREE holiday greetings online! http://greetings.yahoo.com ________________________________________________________________________________
From: "Ralph E. Capen" <recapen(at)earthlink.net>
,
Subject: Coax through plastic bushings
Date: Dec 28, 2001
Folks, As I'm pondering through the construction of my Vertical Stabilizer, I'm trying to determine the correct bushings to use in the upper and lower forward ribs to route my antenna coax through. I already have the Comant CI-182 antenna which fits inside the VS cap and am planning to run RG400 which Bob (Nuckolls) says is about .27" diameter. Here's where I'm stuck...the SB437-4 bushings that Van's (and others) sell has a measured OD of .4375" (7/16") and a measured ID of .274. This means that it should (weasel word) fit. This doesn't really comfort me in preassembling this thing counting on .004 to snake coax through. There is a little lip on the inside of the bushing that could be reamed out for a little better slop. Does anyone out there have any RG400 and one of these bushings that would be willing to test fit it and report...or would be willing to give away a foot or so so I can measure it myself??? Thanks, Ralph Capen RV6AQB N822AR(rsvd) Closed my pre-QB HS - now working on the VS ________________________________________________________________________________
From: "Carl Froehlich" <carlfro(at)erols.com>
Subject: DG replacement
Date: Dec 28, 2001
Use two antennas - simple, more reliable. Although we all tend to fly by GPS heading, for IFR work the FARs specifically state you must have a gyro based DG and AI. I will meet this requirement using the ICARUS solid state gyro AI/DG and iPAQ PDA display, with an RC Allen electric AI as backup. The GPS input to the ICARUS unit will be the GX-60. The second iPAQ on the panel will have the AnyWhere map, fed by a separate GPS receiver. The GX-60 and the AnyWhere map/GPS are feed from separate electric busses. Carl Froehlich RV-8A (mounting empennage for the last time!!) Vienna, VA -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com]On Behalf Of Gary Liming Subject: AeroElectric-List: DG replacement With the advent of the cheap $100-150 GPS from Walmart, etc. and an $80 external antenna, what is wrong with the idea of finding one that can be mounted in the panel, and dedicated with the compass rose and heading screen on full time, and replacing it with the DG? This would be in addition to any other GPS navaid. Can GPS antennas be easily attached to two units, as in a simple "y" harness, or are two antennas a must? Also, If some of the coming $1000 electronic Artificial Horizon units turn out well, you don't need a vacuum pump anymore, making this price competitive with the vacuum instruments. (I am assuming an essential bus arrangement or even a separate battery back up for it.) Gary Liming http://www.matronics.com/browselist/aeroelectric-list ________________________________________________________________________________
From: "Emrath" <Emrath(at)home.com>
Subject: Re: DG replacement
Date: Dec 28, 2001
I purchased a $90 model a year of so ago. The problem is that it doesn't update fast enough for the RV planes. OK in the Cessna 172, but not is a light twin. Marty in Brentwood TN ----- Original Message ----- From: "Gary Liming" <gary(at)liming.org> Subject: AeroElectric-List: DG replacement > > > With the advent of the cheap $100-150 GPS from Walmart, etc. and an $80 > external antenna, what is wrong with the idea of finding one that can be > mounted in the panel, and dedicated with the compass rose and heading > screen on full time, and replacing it with the DG? This would be in > addition to any other GPS navaid. > > Can GPS antennas be easily attached to two units, as in a simple "y" > harness, or are two antennas a must? > > Also, If some of the coming $1000 electronic Artificial Horizon units turn > out well, you don't need a vacuum pump anymore, making this price > competitive with the vacuum instruments. (I am assuming an essential bus > arrangement or even a separate battery back up for it.) > > Gary Liming > > http://www.matronics.com/browselist/aeroelectric-list > > ________________________________________________________________________________
From: jerry(at)tr2.com
Subject: Re: DG replacement
Date: Dec 28, 2001
jdnewsum wrote: > > > The only thing wrong with using a GPS or another > electronic toy instead of a DG is regulatory > requirements... *** Not so! If you use a GPS readout for your DG, you are completely dependant on the GPS system for your navigation. Imagine if it all goes *pop* in the soup... I remember reading somewhere that the ambient GPS signal is something like -160dbm. Not only that, there's a *button* somewhere that can turn it all off! Sometimes, they disable GPS by NOTAM in certain areas. Can you imagine a NOTAM reading "everybody's DG will die on such & such a date within 300 miles of such and such a VORTAC"? Also, a GPS display can only show you ground track direction. When ATC gives you the ole "fly heading 150", he expects you to go the same direction as the last 10 airplanes he gave that vector to. - Jerry Kaidor ( jerry(at)tr2.com ) ________________________________________________________________________________
Date: Dec 28, 2001
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Avionics Cooling Hose
> >Hello, > > Can anybody tell me - what is the exact correct type and size of hose >for cooling radios? You know, the kind that goes into the cooling port on >the back of the radio? > > Thanks in advance, > > - Jerry Kaidor ( jerry(at)tr2.com ) > Jerry, I know I've seen at least two sizes over the years but I'll bet the modern multi-output fans use 5/8" scat tube. How many radios do you have that need cooling?


December 01, 2001 - December 28, 2001

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