Today's Message Index:
----------------------
 
     1. 02:00 AM - Yahoo! Auto Response (bczygan@yahoo.com)
     2. 02:14 AM - incandescent light question (Gilles Thesee)
     3. 06:25 AM - Re: incandescent light question (rampil)
     4. 06:30 AM - Re: Odyssey Battery Alternative (Speedy11@aol.com)
     5. 06:31 AM - Re: Odyssey Battery Alternative (Robert L. Nuckolls, III)
     6. 06:42 AM - Re: incandescent light question (Robert L. Nuckolls, III)
     7. 07:50 AM - Re: Odyssey Battery Alternative ()
     8. 08:24 AM - Re: Impossible problem (Ed Mueller)
     9. 08:54 AM - Re: Impossible problem (jaybannist@cs.com)
    10. 10:38 AM - Re: Odyssey Battery Alternative (Charlie England)
    11. 11:03 AM - Re: Impossible problem (Robert L. Nuckolls, III)
    12. 11:03 AM - Re: Odyssey Battery Alternative (Robert L. Nuckolls, III)
    13. 12:15 PM - Re: incandescent light question (Gilles Thesee)
    14. 01:51 PM - Basic wiring questions (Ralph Finch)
    15. 02:56 PM - Noise in headset when pressing to talk (Neil France)
    16. 03:04 PM - Re: Odyssey Battery Alternative (The Kuffels)
    17. 03:58 PM - Re: Noise in headset when pressing to talk (Allan Aaron)
    18. 06:16 PM - VDC Electronics battery charger offer (Sheldon Olesen)
    19. 06:36 PM - Re: Odyssey Battery Alternative (Robert L. Nuckolls, III)
    20. 08:01 PM - Twisted Pairs, Coils, and EM Fields (Gregory Clawson)
    21. 08:04 PM - [Fw: Huuuuuhhhh?] (RScott)
    22. 08:09 PM - Re: Odyssey Battery Alternative (Mike Creek)
    23. 09:11 PM - Re: [Fw: Huuuuuhhhh?] (Dale Rogers)
    24. 09:40 PM - Re: Twisted Pairs, Coils, and EM Fields (Robert L. Nuckolls, III)
 
 
 
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| Subject:  | Yahoo! Auto Response | 
      
      
      
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      MSN:  myehomebuy-easylife@hotmail.com
      Hope you have a good mood in shopping from their company!
      Best Regards 
      Julie!
      
      
Message 2
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| Subject:  | incandescent light question | 
      
      
      Hi Bob and all,
      
      The topic has already been adressed, but I was not able to retrieve the 
      messages or Bob's recommendations on preheating.
      
      The question recently arose on a French pilot list : when and why is a 
      landing light filament most fragile ?
      - When hot ?
      - When cold ?
      - When heating up ?
      - When cooling down ?
      -Why ?
      
      Etc...
      
      Thanks in advance for any input,
      Best regards,
      -- 
      Gilles
      http://contrails.free.fr
      
      
Message 3
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  | 
      
      
| Subject:  | Re: incandescent light question | 
      
      
      Gilles,
      
      The common wisdom is that most lamp failures occur on start due to
      three factors:
      cold filament stiffness
      heat shock/expansion
      and 3) flexion of the stiff filament due induction of the magnetic field
      in the helical filament
      
      Ira
      
      --------
      Ira N224XS
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=237963#237963
      
      
Message 4
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| Subject:  | Re: Odyssey Battery Alternative | 
      
      
      Well said, Dale.
      The rest of us knew what you meant.
      Stan Sutterfield
      Do not archive
      
      
      Charlie  England wrote:
      > Dale Rogers wrote:
      >> Made in mainland   (PDRC) China?
      >
      > If this is intended to be a political question,  it begs another. Have 
      > you bought any gas for your plane or car lately  (terrorism)? Or 
      > virtually any other consumer product (China  again)?
      >
      > I think that it's instructional that around 50 years  of economic 
      > isolation of Cuba has left it virtually unchanged in it's  government, 
      > economy or human rights. While after 30 years of trade  with China it 
      > isn't 'free', but it's a lot closer than it was 30  years ago, and its 
      > people are certainly a bit better off  economically.
      >
      > I have an 'alternative' view of this stuff. I  think that change must 
      > come from within, & if you want to have  external influence, the best 
      > way to drive it is to let the citizens  see how good it *could* be, 
      > with better  government.
      Charlie,
      
      It wasn't ~intended~ to be "political" - more  of a QA issue.
      There's been a lot of contaminated product coming from  the
      PRC.  I've seen a lot of poor quality hardware (tools,  shop
      equipment, electronics) coming from there.  Dunno if I want
      my  electric-dependent airplane to rely on a battery coming
      from such an  environment.
      
      Best regards,
      Dale R.
      
      
      **************Worried about job security? Check out the 5 safest jobs in a 
      recession. 
      (http://jobs.aol.com/gallery/growing-job-industries?ncid=emlcntuscare00000003)
      
Message 5
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| Subject:  | Re: Odyssey Battery Alternative | 
      
      
      At 10:28 PM 4/5/2009, you wrote:
      >
      >Charlie England wrote:
      >>Dale Rogers wrote:
      >>>Made in mainland  (PDRC) China?
      >>
      >>If this is intended to be a political question, it begs another. 
      >>Have you bought any gas for your plane or car lately (terrorism)? 
      >>Or virtually any other consumer product (China again)?
      >>
      >>I think that it's instructional that around 50 years of economic 
      >>isolation of Cuba has left it virtually unchanged in it's 
      >>government, economy or human rights. While after 30 years of trade 
      >>with China it isn't 'free', but it's a lot closer than it was 30 
      >>years ago, and its people are certainly a bit better off economically.
      >>
      >>I have an 'alternative' view of this stuff. I think that change 
      >>must come from within, & if you want to have external influence, 
      >>the best way to drive it is to let the citizens see how good it 
      >>*could* be, with better government.
      >Charlie,
      >
      >It wasn't ~intended~ to be "political" - more of a QA issue.
      >There's been a lot of contaminated product coming from the
      >PRC.  I've seen a lot of poor quality hardware (tools, shop
      >equipment, electronics) coming from there.  Dunno if I want
      >my electric-dependent airplane to rely on a battery coming
      >from such an environment.
      
         Point taken. However, recall there was a time
         when "Made in Japan" labels gave one pause. We
         had some discussions here on the List about Harbor
         Fright's quality. Bottom line is that for any emerging
         technology, process or manufacturing culture, there
         will ALWAYS be those who's ambitions exceed their
         capabilities or willingness to accomplish the best-we-
         know-how-to-do. Shucks we see this today with "Made in
         USA" products. Why should we be having startup brownout
         discussions on otherwise perfectly wonderful appliances?
      
         Folks who rely on ANY words on any label to do a trade
         study are at risk for being disappointed. At the same
         time, those who automatically reject any product based
         on perceptions of a class of manufacturers are at
         risk of expending $time$ with poor return on investment.
         Folks who promulgate product avoidance based on
         culture are doing a disservice to those within that
         culture who are honestly striving to be competitive.
         Competition: the free market principal that brought us
         monster ram for pennies, gigaflop processors for
         dollars and $100 hand-helds that will find your
         driveway in zero-zero fog.
      
         I've seen stuff at H.F. that I wouldn't buy. I have
         a number of H.F. machine tools in my shop that service
         my needs nicely. A $350 lathe paid for itself in the
         first job! That was 7 years ago and it's still doing
         what I need done within limits of its design.
      
         Discussions here on the List can add the most value
         for its members by evaluating specific products from
         ANY source based on demonstrated price/performance
         benchmarks. Advice that paints a product with a brush
         dipped into cultural perceptions is demonstrably lacking
         in foundation and places top performers in that culture
         at a capriciously invented disadvantage.
      
         Further, while we may have disagreements with and
         even have reason to be fearful of governments (our
         own not withstanding!) recall that there are folks
         who design, build and sell products from all parts
         of the world who would probably like to be building an
         airplane in THEIR garage too.
      
         Finally, if it's a part with failure implications for an
         uncomfortable arrival with the earth . . . isn't
         that why failure tolerance is among our design goals?
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 6
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| Subject:  | Re: incandescent light question | 
      
      
      At 04:12 AM 4/6/2009, you wrote:
      ><Gilles.Thesee@ac-grenoble.fr>
      >
      >Hi Bob and all,
      >
      >The topic has already been adressed, but I was not able to retrieve 
      >the messages or Bob's recommendations on preheating.
      >
      >The question recently arose on a French pilot list : when and why is 
      >a landing light filament most fragile ?
      >- When hot ?
      >- When cold ?
      
         Tungsten passed from a brittle to ductile state
         as it rises in temperature. The legacy automotive
         lamp filaments were most vulnerable to vibration
         stresses while cold.
      
      >- When heating up ?
      
         Thermal stresses are highest during heat-up
         transition.
      
      >- When cooling down ?
      >-Why ?
      
         Modern halogen lamps are MUCH more robust than
         their ancestors. So much so that concerns about
         inrush limiting are almost insignificant in
         terms of adding to the service life of a lamp.
      
         Even when the halogen lamps are used in a wig-wag
         system, they do not cool enough between flashes
         to suffer a deleterious inrush current with each
         flash. See:
      
      http://www.aeroelectric.com/Pictures/Curves/Exemplar_Incandescent_Lamp_Inrush.gif
      
      http://www.aeroelectric.com/Pictures/Curves/Wig_Wag_Currents.jpg
      
          For new design, I'm certain that the builder
          will experience very good service life using
          modern automotive halogen lamps operating without
          benefit of inrush limiting.
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 7
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  | 
      
      
| Subject:  | Odyssey Battery Alternative | 
      
      Bob,
      
      
      Thanks for the dissertation on batteries J Actually this is very
      helpful. If dry cell or sealed batteries are indeed using the same old
      technology as the slosh type, then the extra $$ are indeed a complete
      waste of money, yes? 
      
      
      I suppose they do a bit of marketing with the carbon fibre casings etc.,
      but is there no better mouse trap hiding in there somewhere? I do not
      have the Braille factory specs, but that would be an interesting read.
      My main interest is their lower weight and smaller size. That takes more
      than marketing. There is nothing to say the BB battery at < $50 would
      not provide the same performance albeit without the lower internal
      resistance. I may be confused, but isn't cranking power what we want in
      batteries? When it's 10 degrees outside and I've had my ship plugged in
      for 30 minutes, I don't want to hear ra-ra-ra after just one try. If
      they can boost cranking power by 30 percent, why wouldn't you want that?
      If I lived in Southern CA, perhaps I wouldn't care. A mission specific
      thing.
      
      
      The experience of one of our builders has shown that turning on the
      avionics 5 minutes before starting has disabled the Odyssey's ability to
      the point where it will not provide enough cranking power to turn over
      the engine. He flies a Jabaru 230 with the Jabaru 6-cylinder engine. I
      have not put a meter on the draw (I will), but I did learn that he has
      two GRT displays installed which require a heartbeat be maintained from
      the battery at all times. As you may know the GRT does not support
      internal battery backup directly.
      
      
      I already own an Odyssey and I'm not going to toss it in the trash but I
      will meter it and report on its performance later. Nevertheless, I will
      add a second battery to feed the Aux bus and the dual Lightspeed
      ignition in the event the rest of Z-13/8 fails to co-operate while
      flying over the airplane eating PA woods at night.
      
      
      Glenn
      
      
      From: owner-aeroelectric-list-server@matronics.com
      [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of
      Robert L. Nuckolls, III
      Sent: Saturday, April 04, 2009 10:07 AM
      Subject: Re: AeroElectric-List: Odyssey Battery Alternative
      
      
      At 07:28 AM 4/4/2009, you wrote:
      
      
      <recapen@earthlink.net>
      
      Thanks,
      
      Definitely something to think about when it becomes replacement time.
      My 680 is brand new - I replaced a four year old one that I had beaten
      up pretty hard during the construction process.  The new one seems to do
      fine at the present - but I keep a Battery Hawk on it between flights so
      it's always topped off.
      
      
        Why did you replace it? Was it sent to recycle because
        it's capacity had fallen below your e-bus run-time benchmark
        or because it didn't crank the engine any more?
      
        This thread started with the following statements:
      
      
      "Several of our hangar members have been experiencing trouble with
      reserve power using the popular Odyssey 680 battery. If running avionics
      and the like prior to starting (even briefly), the reserve power on
      these things really take a hit."
      
      "I am not a huge fan of jump starting an aircraft or starting on reduced
      voltage when my craft is already electrically dependent and the taking
      off into a emergency situation with less than full reserve."
      
      "Recently I found an option which has more cranking amps, (better A.H.
      value and about the same weight (or less). Albeit slightly more
      expensive, they may offer a good alternative for 680 users who find
      their batteries run down a bit too fast for their liking."
      
        "Reserve power" speaks to watt-seconds of energy
        contained when fully charged. This is closely
        related to the battery's rated capacity in Ampere-
        Hours although apparent capacity can vary widely 
        depending on loads due to the battery's internal
        losses (conduction = 1/resistance). Double the
        load on a battery and internal losses go up by
        a factor of 4.
      
        The terms "briefly" and "really takes a hit"
        are not quantified. Nor were the pre-cranking loads
        for operation of "running avionics and the like".
        So we're not privy to the numbers that define
        expected/desired battery performance. We also
        don't know the numbers that drove perceptions
        of "experiencing trouble".
      
        My words are not intended to cause anyone discomfort
        but it is helpful to understand the numbers behind
        a proposed exchange of product. Then each of you
        needs to decide how the exchange will improve on
        your personal expectations for system performance
        and the amount of $time$ you're willing to expend
        as a cost of ownership.
      
        The Braille batteries appear to have been fine
        tuned for lower internal resistance. This is 
        suggested by the greater "cranking" or "pulse"
        current ratings. But in terms of capacity, watt-seconds
        of energy stored is pretty much set by how many
        pounds of reactants (lead) is in the battery.
        Indeed, their a.h. ratings/pound of product weight
        are right in line with everybody else's products.
      
        They speak to the "conductance" test and something
        new . . . which it is not. The test is easily 
        performed with modern "battery analyzers". An
        example of this instrument can be seen at:
      
      http://www.midtronics.com/default.asp
      
        where we find no less than 15 different models
        of device selling for hundreds of dollars. What
        your buying with these capable instruments is
        convenience of light weight, compact size,
        digital readout, and perhaps some predictions
        of service-life. However, the data gathered
        is the same as that which you would get from
        this piece of arcane technology from Harbor
        Freight for about $60.
      
      http://aeroelectric.com/Pictures/Battery_Testers/HF91129_4.jpg
      
        The later device requires some understanding
        and skill but ultimately is a BETTER measure
        of cranking performance because the test loads
        are REAL and not extrapolated from short, pulsed
        values in the digital instrument.
      
        What does internal resistance (reciprocal of
        conductance) have to do with capacity? Nothing.
        Capacity is related to pounds of chemistry
        available to store energy. The efficiency with
        which that energy can be extracted for useful
        purposes IS affected by internal resistance. 
        This is discussed in some detail in the battery
        chapter update published at:
      
      http://aeroelectric.com/R12A/02_Battery_12A2.pdf
      
        Without knowing the nature and magnitude of 
        "experiencing trouble" which drives the decision
        to seek a more robust battery, we're not able
        to advance this deliberation based on physics
        and comparative measurements. I can only hypothesize
        as follows:
      
        The perceptions of poor battery performance are
        probably based on a pre-cranking battery load
        that is unnecessarily large. Without an e-bus
        and the ability to get your ATIS data and
        a departure clearance, then flipping on the
        battery master burdens the battery with loads
        that far exceed present requirements.
      
        Keep in mind too that the energy required to
        get a well tuned engine started is but a few
        percent of a battery's capacity. This battery
        voltage/current curve . . .
      
      http://www.aeroelectric.com/Pictures/Curves/turbine_start_a.jpg
      
        was taken from a Beechjet engine start. It
        begins with over 800A and tapers to 300A
        over a period of 27 seconds. After all that
        abuse, the battery is tapped for perhaps 6%
        of contained energy.  I agree that we're
        comparing apples and oranges with respect to
        types of engines and design goals for two
        vastly different airplanes. But I'll suggest
        that if somebody is having trouble getting
        and engine started -OR- has seriously depleted
        a battery during pre-flight operations because
        of loads imposed before the alternator comes
        on line . . . a serious reevaluation of design
        goals and operating procedures is called for.
      
        Back to the Braille battery product.
        They probably do conform to marketing hype
        concerning a lower internal resistance. This
        is easily demonstrated with and instrument not
        unlike the Harbor Freight device cited above.
      
        Now the question: What does the more expensive
        battery buy you in terms of cost of ownership?
        Now that you've installed the Lexus of batteries,
        how are you going to modify your rules of 
        ownership and operation for the purpose of meeting
        design goals for your airplane? Are you going to
        do periodic capacity checks to make well
        considered decisions as to when the battery
        needs replacing? Is it a reasonable expectation
        that $time$ to maintain plust $time$ to buy the
        higher price battery will be SMALLER than $time$
        to buy an el-cheepo battery and replace it
        every year?
      
        Finally, rushing off to buy this premium
        battery product may not get you the same
        return on investment expected by those who are
        "experiencing trouble" with their current
        battery choices. Without an analysis of how
        their disappointment arises, there's no
        guarantee that YOUR purchase of the more
        robust battery will produce a good return
        on your investment.
      
        Bob . . .
      
      
Message 8
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  | 
      
      
| Subject:  | Re: Impossible problem | 
      
      
      Jay,
      
      	Any luck with the problem?  You might consider that maybe the original 
      wiring isn't correct, only appeared to be.  Years ago,  I wired a 
      project (not airplane related) and it worked fine.  Couple years later 
      made a minor alteration and all sorts of strange things started 
      happening.  Turned out the original wiring was incorrect.
      
      Ed
      
      
      On Apr 1, 2009, at 4:08 PM, jaybannist@cs.com wrote:
      
      > Bob,
      >
      >  Thanks. I had about decided that the laws of physics HAD been 
      > repealed, or that I was losing my ever-lovin' mind ! Now that you 
      > have confirmed that those laws are still intact; I know that my next 
      > step is to take all the wiring off those two switches. Then I will 
      > positively identify each wire before I reinstall it on the switch. 
      > I'll let you know if that fixes the problem.
      >
      >  Thanks again - Jay
      >
      >
      >  -----Original Message-----
      >  From: Robert L. Nuckolls, III <nuckolls.bob@aeroelectric.com>
      >  To: aeroelectric-list@matronics.com
      >  Sent: Wed, 1 Apr 2009 1:53 pm
      >  Subject: Re: AeroElectric-List: Impossible problem
      >
      >  At 12:37 PM 4/1/2009, you wrote:
      >
      >
      >> My MAIN source of concern is that EVERYTHING
      >>  worked properly before I made this change; and the
      >>  ONLY thing I changed was the source of power to
      >>  the coil and fuel pump switches.
      >>
      >>  Jay
      >   Understand. Without being able to put my
      >   hands on the problem, the most I (or anyone
      >   else) can do is hypothesize about a lot
      >   of things . . . the majority of which will
      >   be irrelevant/wrong.
      >
      >   The laws of physics do not shift their
      >   effects to confound us. There is a specific
      >   reason why you are experiencing the problem
      >   you cited. If you've ever played the board game
      >   Clue, you'll understand that arriving at root
      >   cause is a distillation of facts first to
      >   eliminate those that do not fit into an
      >   explanation of effects and finally identify the
      >   order in which remaining facts explain the
      >   cause for symptoms you've identified.
      >
      >   Snip off the tie wraps, check the wires, follow
      >   the path from bus to appliance with a voltmeter
      >   probe . . . nobody sez it's easy . . . but it
      >   works every time.
      >
      >   Bob . . .
      >
      >
      >  Email message sent from CompuServe - visit us today at 
      > http://www.cs.com
      >
      >
      
      
Message 9
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  | 
      
      
| Subject:  | Re: Impossible problem | 
      
      
       Ed,
      
      I think you are right. It did work before the change, but that might have just
      been dumb luck. 
      
      My airplane is hangered 40 miles and an hour's drive from my home, right through
      the middle of Dallas. The upshot is that I don't work on it as often as I want
      to, or should.? My next trip (this week) will be to do a BUNCH of re-wiring.?
      Stay tuned.
      
      Jay? ?? 
      
      
      -----Original Message-----
      From: Ed Mueller <ed@muellerartcover.com>
      Sent: Mon, 6 Apr 2009 10:22 am
      Subject: Re: AeroElectric-List: Impossible problem
      
      
      ?
      
      Jay,?
      ?
      
      ?  Any luck with the problem?  You might consider that maybe the original 
      wiring isn't correct, only appeared to be.  Years ago,  I wired a 
      project (not airplane related) and it worked fine.  Couple years later 
      made a minor alteration and all sorts of strange things started 
      happening.  Turned out the original wiring was incorrect.?
      ?
      
      Ed?
      ?
      
      
      On Apr 1, 2009, at 4:08 PM, jaybannist@cs.com wrote:?
      ?
      
      > Bob,?
      
      >?
      
      >  Thanks. I had about decided that the laws of physics HAD been 
      > repealed, or that I was losing my ever-lovin' mind !? Now that you 
      > have confirmed that those laws are still intact;? I know that my next 
      > step is to take all the wiring off those two switches.? Then I will 
      > positively identify each wire before I reinstall it on the switch.? 
      > I'll let you know if that fixes the problem.?
      
      >?
      
      >  Thanks again - Jay?
      
      >?
      
      
      ________________________________________________________________________
      Email message sent from CompuServe - visit us today at http://www.cs.com
      
Message 10
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| Subject:  | Re: Odyssey Battery Alternative | 
      
      
      ________________________________
      From: Dale Rogers <dale.r@cox.net>
      Sent: Sunday, April 5, 2009 10:28:08 PM
      Subject: Re: AeroElectric-List: Odyssey Battery Alternative
      
      
      Charlie England wrote:
      > Dale Rogers wrote:
      >> Made in mainland  (PDRC) China?
      > 
      > If this is intended to be a political question, it begs another. Have you bought
      any gas for your plane or car lately (terrorism)? Or virtually any other consumer
      product (China again)?
      > 
      > I think that it's instructional that around 50 years of economic isolation of
      Cuba has left it virtually unchanged in it's government, economy or human rights.
      While after 30 years of trade with China it isn't 'free', but it's a lot
      closer than it was 30 years ago, and its people are certainly a bit better off
      economically.
      > 
      > I have an 'alternative' view of this stuff. I think that change must come from
      within, & if you want to have external influence, the best way to drive it is
      to let the citizens see how good it *could* be, with better government.
      Charlie,
      
      It wasn't ~intended~ to be "political" - more of a QA issue.
      There's been a lot of contaminated product coming from the
      PRC.  I've seen a lot of poor quality hardware (tools, shop
      equipment, electronics) coming from there.  Dunno if I want
      my electric-dependent airplane to rely on a battery coming
      from such an environment.
      
      Best regards,
      Dale R.
      
      Ahh, yes, that makes sense; sorry for the misunderstanding. I wonder where the
      higher priced ones are made. 
      
      One thing I did notice is that the internal resistance is rather high; from something
      like 11 to 16 mOhms. IIRC, the Odessey is closer to 6 mOhms. I'm using
      a similarly rated battery in my RV-4 (Lyc O-320) & it cranks 'ok' but I doubt
      it would be up to the task on a hi compression IO360.
      
      Charlie
      
Message 11
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| Subject:  | Re: Impossible problem | 
      
      At 10:52 AM 4/6/2009, you wrote:
      >Ed,
      >
      >I think you are right. It did work before the change, but that might 
      >have just been dumb luck.
      >
      >My airplane is hangered 40 miles and an hour's drive from my home, 
      >right through the middle of Dallas. The upshot is that I don't work 
      >on it as often as I want to, or should.  My next trip (this week) 
      >will be to do a BUNCH of re-wiring.  Stay tuned.
      
      
         Ed beat me to it. I was about to ask too. We're
         all interested in what you find out!
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 12
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| Subject:  | Odyssey Battery Alternative | 
      
      
      At 09:48 AM 4/6/2009, you wrote:
      >Bob,
      >
      >Thanks for the dissertation on batteries J Actually this is very 
      >helpful. If dry cell or sealed batteries are indeed using the same 
      >old technology as the slosh type, then the extra $$ are indeed a 
      >complete waste of money, yes?
      
         No. All lead-acid batteries use lead, lead dioxide, lead sulfate,
         sulfuric acid and water to craft a reversible electrical energy
         storage system.
      
      http://en.wikipedia.org/wiki/Lead-acid_battery
      
          Fabrication methods that exploit this reaction have seen
          huge evolutionary steps since the time that Plante'
          first described the phenomenon in 1859 (before the
          civil war!)
      
          Even during my short experience with lead-acid
          technology (my first car was a 6v, '41 Pontiac
          acquired in 1961) we've see amazing improvements
          in robusness, volumetric efficiency, electrical
          efficiency, ease of integration and cost of
          ownership for this venerable process.
      
      >I suppose they do a bit of marketing with the carbon fibre casings 
      >etc., but is there no better mouse trap hiding in there somewhere? I 
      >do not have the Braille factory specs, but that would be an 
      >interesting read. My main interest is their lower weight and smaller 
      >size. That takes more than marketing. There is nothing to say the BB 
      >battery at < $50 would not provide the same performance albeit 
      >without the lower internal resistance. I may be confused, but isn't 
      >cranking power what we want in batteries? When it's 10 degrees 
      >outside and I've had my ship plugged in for 30 minutes, I don't want 
      >to hear ra-ra-ra after just one try. If they can boost cranking 
      >power by 30 percent, why wouldn't you want that? If I lived in 
      >Southern CA, perhaps I wouldn't care. A mission specific thing.
      
          You're speaking in non-quantified concerns, conditions
          and design goals. Yes, it's probably a given that a
          $200 battery has features justifying its increases
          in cost over a $50 battery of the same capacity. Do
          you need and/or can you exploit a 30% increase in cranking
          power? If you arbitrarily say "yes" . . . then perhaps
          an upgrade to Braille products is selling your design
          goals short. How about a ni-cad? Those are super cranking
          batteries . . . but they have trade-offs.
      >
      >The experience of one of our builders has shown that turning on the 
      >avionics 5 minutes before starting has disabled the Odyssey's 
      >ability to the point where it will not provide enough cranking power 
      >to turn over the engine. He flies a Jabaru 230 with the Jabaru 
      >6-cylinder engine. I have not put a meter on the draw (I will), but 
      >I did learn that he has two GRT displays installed which require a 
      >heartbeat be maintained from the battery at all times. As you may 
      >know the GRT does not support internal battery backup directly.
      
         Okay. What is the capacity of the battery he's using?
         How large are his avionics loads? Is he just running
         the necessary electro-whizzies for pre-flight . . .
         or is the whole panel lit up? 5 minutes is a long
         time to set there with the panel all lit up. This battery
         is supposed to carry e-bus loads for how long? Minutes,
         an hour? THREE hours?
      
         Your narrative doesn't inform us sufficiently to offer
         considered advice. If a 5-minute panel load is degrading
         cranking performance, the FIRST question can be answered
         only by capacity and load testing the battery. There's
         a high probability that his battery is trashed. But if
         his panel loads are say, 50 amps . . . AND assuming that
         the 5-minute pre-flight ops are part of his design
         goals, then let's see . . .
      
         The PC680 is rated for 7 milliohms internal resistance
         and a 20 hour capacity of 17 a.h. We don't have performance
         curves for the PC680 but the ratings are similar to this
         battery . . .
      
      http://www.aeroelectric.com/Pictures/Curves/17AH_12V_Capacity_vs_Load.gif
      
         Gee, 50A of panel load is going whack the battery pretty
         hard in 5 minutes. Okay how about a 17A panel load. Hmmm . . .
         5 minutes of operation should leave plenty of snort to
         crank the engine. Lighter loads are still more attractive.
      >
      >I already own an Odyssey and I'm not going to toss it in the trash 
      >but I will meter it and report on its performance later. 
      >Nevertheless, I will add a second battery to feed the Aux bus and 
      >the dual Lightspeed ignition in the event the rest of Z-13/8 fails 
      >to co-operate while flying over the airplane eating PA woods at night.
      
         If that design philosophy assuages your concerns, by
         all means. My point is that these systems operate
         based on easily deduced and interpreted numbers.
         Just for grins, if you do have a capacity meter,
         fully charge your battery, do a standard preflight,
         crank the engine . . . say twice without turning
         the alternator on. Shut everything down and THEN
         do a capacity test at the discharge level appropriate
         to your endurance loads.
      
         If you find that the system falls short on design
         goals, perhaps you DO need a different battery . . .
         but the upgrade may have more to do with CAPACITY
         than it does with getting the engine started. Given
         that were comparing TWO 17 a.h. batteries, perhaps
         the upgrade you're anticipating would have an
         exceedingly poor return on investment.
      
         It concerns me that with two engine-driven power
         sources, a battery with an exemplar reputation,
         and some form of metering for battery condition
         that you're still not comfortable with the as-installed
         system. This suggests that you've not created, tested
         and are maintaining a plan-a, plan-b, plan-c approach
         to failures. This leaves you in the unhappy position
         of (1) constantly worrying; a lack of confidence
         based on lack of knowledge and (2) being ready to buy some
         new electro-whizzy because of some perceived incremental
         increase in performance described in their 4-color
         marketing brochures.
      
         Bob . . .
      
      
Message 13
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  | 
      
      
| Subject:  | Re: incandescent light question | 
      
      
      Robert L. Nuckolls, III a crit :
      >
      >   Tungsten passed from a brittle to ductile state
      >   as it rises in temperature. The legacy automotive
      >   lamp filaments were most vulnerable to vibration
      >   stresses while cold. 
      
      Bob, Ira and all,
      
      Thanks for your response.
      
      Best regards,
      -- 
      Gilles
      http://contrails.free.fr
      
      
Message 14
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| Subject:  | Basic wiring questions | 
      
      
      I have landing/taxi lights, LED nav lights, a Bob Archer VOR antenna, and an
      APRS tx/rx antenna in the ends of the wings of an RV-9A (one antenna in each
      tip).
      
      1. For the powered items, can I run a single positive wire of adequate size
      to a terminal block, then feed the devices from the block?
      
      2. For the antennas, yes they will be using coax, but should I nevertheless
      try to run the coax physically separate from the power wires?  In addition
      to the above power wire I have a 3-wire bundle run from the strobe power
      supply in the fuselage to the wing-tip strobe lights.  I installed a conduit
      about 18 inches away from the Vans wire holes for this purpose.
      
      Thanks,
      
      Ralph Finch
      Davis, CA
      RV-9A QB-SA
      
      
Message 15
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  | 
      
      
| Subject:  | Noise in headset when pressing to talk | 
      
      Hello listers, I hope you can help me figure out a small problem I have 
      please.
      
      I have a mk IV Kitfox fitted with a Bendix King KY97A radio coupled to a 
      Flightcom 403mc intercom, which has been in service without trouble for 
      a number of years.
      The aircraft has not flown for around seven months, and I am putting it 
      back into service.
      When the pilots side ptt is pressed, there is a loud constant noise 
      through both headsets, when the copilots ptt is pressed, there is no 
      noise.
      
      I replaced the wiring and earths to the pilots stick, but it made no 
      difference
      
      I then removed the wire from pin no. 7( pilots ptt switch), on the rear 
      of the unit to eliminate the ptt switch and wiring, and substituted a 
      long length of wire which I touched directly to the battery negative,  
      and the noise was still there.
      I checked the pins and sockets which all look in perfect condition, but 
      cleaned them anyway.
      
      If I use the long length of wire from the battery to pin no. 6 (copilot 
      ptt switch ) it works perfectly with no noise. 
      
      The noise I hear in my headset, is not transmitted , I have checked the 
      radio reception from a hand held radio using different headsets plugged 
      into the pilot and copilot sockets, and reception is perfect with no 
      background noise.
      
      
      Has anyone  any ideas what it could be  please?
      
      
      Any help would be greatly appreciated, thanks in advance,
      
      Neil.
      
Message 16
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| Subject:  | Re: Odyssey Battery Alternative | 
      
      
      Don't understand the problem with PC-680 batteries.  This is the type 
      supplied by Glasair for their Sportsman kits.  No-one has reported any 
      similar experience.  Glenn said his friend has two GRTs with the need for a 
      keep alive clock current.  Can't find a specification on the GRT web site 
      for this current but most circuits of this type use about 1 ma.  But suppose 
      the current is 10 ma.  In this case if he hasn't flown in a while this load 
      could significantly deplete the battery (over 10 amp-hours) in only 3 weeks. 
      At least it is worth measuring to determine if this is part of the problem.
      
      Tom Kuffel 
      
      
Message 17
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  | 
      
      
| Subject:  | Noise in headset when pressing to talk | 
      
      I had a similar problem and it turned out to be a problem with my
      lightspeed headset. I send them back to lightspeed and they fixed them
      at no charge.
      Allan
      
      ________________________________
      
      From: owner-aeroelectric-list-server@matronics.com
      [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Neil
      France
      Sent: Tuesday, 7 April 2009 7:55 AM
      Subject: AeroElectric-List: Noise in headset when pressing to talk
      
      
      Hello listers, I hope you can help me figure out a small problem I have
      please.
      
      I have a mk IV Kitfox fitted with a Bendix King KY97A radio coupled to a
      Flightcom 403mc intercom, which has been in service without trouble for
      a number of years.
      The aircraft has not flown for around seven months, and I am putting it
      back into service.
      When the pilots side ptt is pressed, there is a loud constant noise
      through both headsets, when the copilots ptt is pressed, there is no
      noise.
      
      I replaced the wiring and earths to the pilots stick, but it made no
      difference
      
      I then removed the wire from pin no. 7( pilots ptt switch), on the rear
      of the unit to eliminate the ptt switch and wiring, and substituted a
      long length of wire which I touched directly to the battery negative,
      and the noise was still there.
      I checked the pins and sockets which all look in perfect condition, but
      cleaned them anyway.
      
      If I use the long length of wire from the battery to pin no. 6 (copilot
      ptt switch ) it works perfectly with no noise. 
      
      The noise I hear in my headset, is not transmitted , I have checked the
      radio reception from a hand held radio using different headsets plugged
      into the pilot and copilot sockets, and reception is perfect with no
      background noise.
      
      
      Has anyone  any ideas what it could be  please?
      
      
      Any help would be greatly appreciated, thanks in advance,
      
      Neil.
      
      
Message 18
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  | 
      
      
| Subject:  | VDC Electronics battery charger offer | 
      
      Bob,
      
      VDC Electronics is offering  aviation specific battery chargers at a  
      reduced price if you trade in an a non-aviation charger.   Their  
      aviation chargers are temperature compensated so there is no over or  
      undercharging. They claim that the new chargers will increase the  
      battery life.  Are regular battery chargers inadequate for the task,  
      especially if the batteries are being replace every year or so?   Is  
      this a marketing gimmick or something worthwhile?
      
      Sheldon Olesen
      
      http://www.batteryminders.com/batterycharger/home.php
      
      
Message 19
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  | 
      
      
| Subject:  | Re: Odyssey Battery Alternative | 
      
      
      At 04:29 PM 4/6/2009, you wrote:
      >
      >Don't understand the problem with PC-680 batteries.  This is the 
      >type supplied by Glasair for their Sportsman kits.  No-one has 
      >reported any similar experience.  Glenn said his friend has two GRTs 
      >with the need for a keep alive clock current.  Can't find a 
      >specification on the GRT web site for this current but most circuits 
      >of this type use about 1 ma.  But suppose the current is 10 ma.  In 
      >this case if he hasn't flown in a while this load could 
      >significantly deplete the battery (over 10 amp-hours) in only 3 
      >weeks. At least it is worth measuring to determine if this is part 
      >of the problem.
      >
      >Tom Kuffel
      
         The thread started with an observation that one or more
         folks where having trouble getting their engine started
         after a 5 minute pre-starting load of unknown magnitude.
      
         An idea was proposed that a particular brand of
         battery might be a good replacement. It was advertised
         to have greater cranking capability.
      
         This isn't about the goodness of one battery or the
         badness of another. It's about KNOWING what the
         design goals are and then deducing why they're
         not being met. The original problem may be no more
         profound than the fact that PC680 was shot. Without
         getting the numbers, all the rest is conversation.
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 20
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  | 
      
      
| Subject:  | Twisted Pairs, Coils, and EM Fields | 
      
      
      Bob-
      I recently bought an IVOPROP magnum inflight adjustable propeller; the adjustment
      is done with an electric motor.  The power and ground leads are both approximately
      12 feet long, as are the two leads that go from the switch to the carbon
      brushes.  The installation directions explicitly state "Do not cut the wires";
      I called IVOPROP and asked if that applied to all four wires, or only the
      ones going out to the prop.  They stated that all the wires should be left alone,
      as the resistance of the wires was part of the calculation for circuit breaker
      selection, and shorter wires would result in the breaker tripping more easily.
      So, I have two pair of 12 fort wires to stow in behind the panel of an
      RV-7.
      
      I don't want simply to coil the wires out of concern for the EM field the coil
      would produce whenever I'm changing the pitch of the prop.  Can I take the power/ground
      pair and twist them, take the two leads out to the prop and twist them,
      then twist the two twisted pairs together, and finally stow them in a loose
      but well-secured coil?  Memories from college physics lead me to think the electrons
      flowing in opposite directions should cancel each others' fields, but
      those memories are a little hazy.
      
      Thank you,
      Gregory Clawson
      RV-7, E-6/200, N687LC (res)
      
      
            
      
Message 21
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| Subject:  | [Fwd: Huuuuuhhhh?] | 
      
      
Message 22
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  | 
      
      
| Subject:  | Odyssey Battery Alternative | 
      
      
      Forgive me for adding more "conversation", but 680's have performed well for
      me.
      
      I use a PC-680 on an O-540 installation.  I'm on the second 680 and both
      have performed well.  I trashed the first one during the building process by
      hitting it with 15 or so full discharges after leaving the master on.  Then
      I overcharged it numerous times with a non-maintaining car charger. It still
      started the 540 but was getting weak after two months of flying.  I put in
      the second one and it just goes and goes even on cold morning starts. I have
      to say it has plenty of reserve, but I haven't measured how much. 
      
      Mike  
      
      -----Original Message-----
      From: owner-aeroelectric-list-server@matronics.com
      [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L.
      Nuckolls, III
      Sent: Monday, April 06, 2009 6:34 PM
      Subject: Re: AeroElectric-List: Odyssey Battery Alternative
      
      <nuckolls.bob@aeroelectric.com>
      
      At 04:29 PM 4/6/2009, you wrote:
      <kuffel@cyberport.net>
      >
      >Don't understand the problem with PC-680 batteries.  This is the 
      >type supplied by Glasair for their Sportsman kits.  No-one has 
      >reported any similar experience.  Glenn said his friend has two GRTs 
      >with the need for a keep alive clock current.  Can't find a 
      >specification on the GRT web site for this current but most circuits 
      >of this type use about 1 ma.  But suppose the current is 10 ma.  In 
      >this case if he hasn't flown in a while this load could 
      >significantly deplete the battery (over 10 amp-hours) in only 3 
      >weeks. At least it is worth measuring to determine if this is part 
      >of the problem.
      >
      >Tom Kuffel
      
         The thread started with an observation that one or more
         folks where having trouble getting their engine started
         after a 5 minute pre-starting load of unknown magnitude.
      
         An idea was proposed that a particular brand of
         battery might be a good replacement. It was advertised
         to have greater cranking capability.
      
         This isn't about the goodness of one battery or the
         badness of another. It's about KNOWING what the
         design goals are and then deducing why they're
         not being met. The original problem may be no more
         profound than the fact that PC680 was shot. Without
         getting the numbers, all the rest is conversation.
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 23
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  | 
      
      
| Subject:  | Re: [Fwd: Huuuuuhhhh?] | 
      
      Obviously a product of the public school system.
      
      Dale R.
      COZY MkIV #0497
      Ch. 13
      
      RScott wrote:
      >  
      
      < newspaper clipping >
      
      
Message 24
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  | 
      
      
| Subject:  | Re: Twisted Pairs, Coils, and EM Fields | 
      
      
      At 09:58 PM 4/6/2009, you wrote:
      
      >Bob-
      >I recently bought an IVOPROP magnum inflight adjustable propeller; 
      >the adjustment is done with an electric motor.  The power and ground 
      >leads are both approximately 12 feet long, as are the two leads that 
      >go from the switch to the carbon brushes.  The installation 
      >directions explicitly state "Do not cut the wires"; I called IVOPROP 
      >and asked if that applied to all four wires, or only the ones going 
      >out to the prop.  They stated that all the wires should be left 
      >alone, as the resistance of the wires was part of the calculation 
      >for circuit breaker selection, and shorter wires would result in the 
      >breaker tripping more easily.  So, I have two pair of 12 fort wires 
      >to stow in behind the panel of an RV-7.
      
          This borders on bizarre. I cannot imagine anbody
          figuring wire length into the sizing of a circuit
          breaker.
      
      
      >I don't want simply to coil the wires out of concern for the EM 
      >field the coil would produce whenever I'm changing the pitch of the 
      >prop.  Can I take the power/ground pair and twist them, take the two 
      >leads out to the prop and twist them, then twist the two twisted 
      >pairs together, and finally stow them in a loose but well-secured 
      >coil?  Memories from college physics lead me to think the electrons 
      >flowing in opposite directions should cancel each others' fields, 
      >but those memories are a little hazy.
      
          I'm pretty sure just running them in parallel
          bundles is fine. I've written the company to
          inquire as to the physics behind any determination
          of criticality for bundle length.
      
          Watch this space.
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
 
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