Today's Message Index:
----------------------
 
     1. 05:40 AM - Re: AT150 Interrogation Light (Fox5flyer)
     2. 06:05 AM - Re: Re: AT150 Interrogation Light (Robert L. Nuckolls, III)
     3. 06:08 AM - Re: Re: Z-19/RB Question (Robert L. Nuckolls, III)
     4. 06:20 AM - Re: Re: Z-19/RB Question (Robert L. Nuckolls, III)
     5. 06:59 AM - Re: Re: AT150 Interrogation Light (Kelly McMullen)
     6. 07:26 AM - Re: FYI: Powergate (Robert L. Nuckolls, III)
     7. 07:46 AM - Re: Re: AT150 Interrogation Light (Robert L. Nuckolls, III)
     8. 11:37 AM - Re: Re: Z-19/RB Question (Ed Holyoke)
     9. 12:32 PM - Re: ICOM A200 (Bill Boyd)
    10. 01:40 PM - Re: FYI: Powergate (Robert L. Nuckolls, III)
    11. 01:50 PM - Re: Re: Z-19/RB Question (Robert L. Nuckolls, III)
    12. 09:40 PM - Transpo V1200 regulator (Jeffrey W. Skiba)
    13. 11:07 PM - Official AeroElectric-List FAQ (Frequently Asked Questions) (Matt Dralle)
    14. 11:10 PM - Official AeroElectric-List Usage Guidelines (Matt Dralle)
 
 
 
Message 1
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  | 
      
      
| Subject:  | Re: AT150 Interrogation Light | 
      
      
      Thanks, Matt.  First, the engine uses one plug per cylinder.  The two ignitions
      come together in coil joiners (isolation modules).  I'd considered the possibility
      of a bad high tension lead, but sort of discounted that because the engine
      runs great from either ignition with no drop at all with mag checks.  Then
      again, that's just my logic talking and it doesn't mean that it's not a high tension
      lead.  I've changed plugs with the same result.  If I could figure out
      what "might" be causing it, I could probably do a little wire sorting and find
      the culprit, but I'm just not knowledgeable enough to get a clear picture in
      my mind what is happening.  Obviously, it's emanating from the left ignition circuit
      because when I turn off power to it, the noise in my headset stops and
      the interrogation light on the transponder goes out.  I've already checked all
      of the high tension leads with an ohm meter and none are significantly different
      which leads me to believe the problem lies in the "placement" of my wiring
      bundles somewhere.  Am I making sense?
      Thanks again,
      Deke
      
      
      mprather(at)spro.net wrote:
      > Deke,
      > 
      > Sounds like you're making progress..  Does the engine have two plugs per
      > cylinder?  If so, the problem could be as simple a faulty high tension
      > lead - or even a bad plug.
      > 
      > Along these lines, my guess would be that the source of noise is in the
      > high-energy portion of the system - as that seems most likely to radiate
      > offensive noise.  That's why I'd guess the noise is from a high tension
      > lead.
      > 
      > If not dual plugs, does your system use a coil switcher?  If so, maybe the
      > noise is in that portion of the circuit.
      > 
      > Good luck!
      > 
      > 
      > Matt-
      > 
      > 
      > >  
      > >  
      > > 
      > >  Thanks for your reply, Bob.  I appreciate all input.  Well, I flew this
      > >  morning for about an hour and the first thing I checked was that my cell
      > >  phone was turned off.  No change.  At cruise the light was on steady.
      > >  Next, I switched off my left ignition which did two things.  It stopped
      > >  the noise in my headset and the interrogation light on the transponder
      > >  went out and started blinking normally!  I'm getting close.  So, now I can
      > >  tear into the wiring and see where my left ignition wiring is in a common
      > >  bundle with my headset receive and also the transponder.  What would you
      > >  suggest here?  Obviously I need to either separate some wiring or do some
      > >  shielding, but I'm not sure which way I should go.  If you were to home in
      > >  on a specific wire, which would it be?  My engine is the NSI EA81 with
      > >  stock Electromotive ignition modules.  I personally don't think anything
      > >  is wrong with the ignitions.  I believe I just have an ignition wire
      > >  somewhere causing interference.  I'll dig my s!
      > >   chematics out to see if I can experience an epiphany.
      > >  Thanks again,
      > >  Deke
      > >  NE Michigan
      > > 
      > > 
      > > 
      > 
      
      
      --------
      Deke Morisse
      Kitfox S5 TD
      NSI/CAP
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=195978#195978
      
      
Message 2
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  | 
      
      
| Subject:  | Re: AT150 Interrogation Light | 
      
      
      At 05:36 AM 8/1/2008 -0700, you wrote:
      >
      >Thanks, Matt.  First, the engine uses one plug per cylinder.  The two 
      >ignitions come together in coil joiners (isolation modules).  I'd 
      >considered the possibility of a bad high tension lead, but sort of 
      >discounted that because the engine runs great from either ignition with no 
      >drop at all with mag checks.  Then again, that's just my logic talking and 
      >it doesn't mean that it's not a high tension lead.  I've changed plugs 
      >with the same result.  If I could figure out what "might" be causing it, I 
      >could probably do a little wire sorting and find the culprit, but I'm just 
      >not knowledgeable enough to get a clear picture in my mind what is 
      >happening.  Obviously, it's emanating from the left ignition circuit 
      >because when I turn off power to it, the noise in my headset stops and the 
      >interrogation light on the transponder goes out.  I've already checked all 
      >of the high tension leads with an ohm meter and none are significantly 
      >different which leads me to believe the problem lies in th!
      >  e "placement" of my wiring bundles somewhere.  Am I making sense?
      
          On the TC side of aviation's house, all appliances considered
          for use on airplanes is evaluated for its stand-alone
          characteristics with respect to noise emissions, noise
          vulnerabilities, temperature limits, etc. The goal is
          to offer smooth integration of that device into an
          airplane where the installer does not need to accommodate
          a shortfall in performance.
      
          I presume that you have two identical ignition systems
          of which only one causes noise. I'm presuming further
          that few (if any) other builders have experienced the
          noise issues with these systems. This leads me to
          suggest that there is something "different" about the
          two systems installed on your airplane. It might be
          fixed by a wire installation revision . . . but if so,
          then perhaps theses systems have not been sufficiently
          refined sufficiently for smooth integration into aircraft.
      
          I mention all this because it offers a mode of investigation
          that looks for differences between the two systems. One
          generates an unacceptable level of noise while the other
          does not. How are wires routed differently between the two?
          You might try swapping components between the two systems
          to see if the problem follows the swap. You can use the
          12 lantern battery experiment to power each system up
          independently from ship's power . . . although this is
          a very long shot for a noise that the transponder sees.
      
          The transponder has already been qualified to tolerate
          a lot of conducted noise into ship's wiring . . . the
          energy that upsets it now is probably coming through
          the antenna. So, try disconnecting the transponder
          antenna for a short test to see if it stops triggering
          on the noise.
      
          This is a game of clue. You've identified the source
          of noise and victim to that noise. Now you need to
          ferret out the propagation mode. Once that's identified,
          the fix will be easy.
      
          Bob . . .
      
      
Message 3
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| Subject:  | Re: Z-19/RB Question | 
      
      
      At 10:09 PM 7/31/2008 -0700, you wrote:
      >
      >Just one more thing, Mike. I periodically test the diode feeding the 
      >E-Buss by turning on the master only or turning off the E-buss switch 
      >first and making sure that the stuff on the E-buss is hot. I don't want 
      >the alternate feed switch to be the single point of failure.
      
         The e-bus alternate feed switch cannot be a single point
         of e-bus failure since it's the second of two independent
         feed paths to the e-bus. If the alternate feed path is
         pre-flight tested and then "put away unless needed" then
         probability of it being available as needed is very high.
      
         This was the spirit and intent of the alternate feed path
         philosophy re-enforced by the notion that it was a good
         thing to shut battery contactors off during battery only
         operations.
      
         Bob . . .
      
      
Message 4
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| Subject:  | Re: Z-19/RB Question | 
      
      
      At 07:14 AM 7/31/2008 -0700, you wrote:
      >
      >Thanks Ed,  That is a helpful confirmation of my understanding. I am 
      >building my preflight/postflight checklists for this new z-19 system. I 
      >too don't want things to go 'offline' if the alternator dies.
      
         The only thing that happens when the alternator quits
         is that bus voltage drops from a nominal 14.2 volts down
         to about 12.6 volts. If you did NOTHING at this point in
         time, you would be no worse off than if you were flying
         a C-172 except that your options for load shedding
         for battery only ops are more limited in the C-172.
      
         If you were typical of C-172 drivers, you would have
         no idea how long the battery would carry the minimum
         loads you were able to achieve because not one C-172
         driver in 1000 has any first hand knowledge of (1)
         battery capacity and (2) how long his minimized loads
         will run from that capacity.
      
         If you did not have the alternate e-bus feeder
         installed (replace the diode with an avionics
         master switch) you MIGHT still have a leg up on a
         C-172 driver in that you could conduct the experiments
         to KNOW how much battery only endurance you had with
         that particular architecture.
      
         Now, having added the alternate feed path and the
         diode that prevents mis-routing of energy, you
         have an opportunity to craft a confident plan-b
         for dealing with alternator failure. The plan-b
         removes all loads not necessary for en route operation
         of the airplane . . . which can be quite small.
         This INCLUDES energies need to keep the battery
         contactor closed. Once you are cleared to land
         you can turn the battery master back ON and run
         any number of additional goodies you wish. Whether
         or not they continue to run to the parking spot
         is immaterial to the outcome of the flight.
      
         There is no compelling reason to fly with the alternate
         feed path closed. Even if your ships voltmeter feeds
         from the e-bus, it reads about .7v lower than
         main bus . . . so what? That value becomes the
         NORMAL operating point for the e-bus. The fact
         that it does not represent main bus voltage is
         of no consequence to you as a pilot in the operation
         of the airplane.
      
         Bob . . .
      
      
      >Read this topic online here:
      >
      >http://forums.matronics.com/viewtopic.php?p=195860#195860
      >
      >
      >Checked by AVG - http://www.avg.com
      >6:37 PM
      
      
              Bob . . .
      
              ----------------------------------------)
              ( . . .  a long habit of not thinking   )
              ( a thing wrong, gives it a superficial )
              ( appearance of being right . . .       )
              (                                       )
              (                  -Thomas Paine 1776-  )
              ----------------------------------------
      
      
Message 5
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  | 
      
      
| Subject:  | Re: AT150 Interrogation Light | 
      
      
      One cheap "tester" to find the source of the noise, is an old Walkman or 
      equivalent radio(yeah, those things about 2 generations older than the 
      Ipod), tuned away from any station, on the AM band, preferably near the 
      top...1650 or thereabouts.  Then just move it about taking all necessary 
      precautions with regard to the prop slice/dicer up front. Wherever the 
      noise peaks, is the location of the offender. I've found bad voltage 
      regulators that way, among other things. Just a resistance reading 
      doesn't prove a high tension lead isn't leaking noise, only proves 
      continuity.
      
      Fox5flyer wrote:
      >
      > Thanks, Matt.  First, the engine uses one plug per cylinder.  The two ignitions
      come together in coil joiners (isolation modules).  I'd considered the possibility
      of a bad high tension lead, but sort of discounted that because the engine
      runs great from either ignition with no drop at all with mag checks.  Then
      again, that's just my logic talking and it doesn't mean that it's not a high
      tension lead.  I've changed plugs with the same result.  If I could figure out
      what "might" be causing it, I could probably do a little wire sorting and find
      the culprit, but I'm just not knowledgeable enough to get a clear picture in
      my mind what is happening.  Obviously, it's emanating from the left ignition
      circuit because when I turn off power to it, the noise in my headset stops and
      the interrogation light on the transponder goes out.  I've already checked all
      of the high tension leads with an ohm meter and none are significantly different
      which leads me to believe the problem lies in th!
      >  e "placement" of my wiring bundles somewhere.  Am I making sense?
      > Thanks again,
      > Deke
      >  
      
      
Message 6
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  | 
      
      
| Subject:  | Re: FYI: Powergate | 
      
      
      At 08:31 AM 7/30/2008 -0700, you wrote:
      >
      >See: http://www.perfectswitch.com/downloads/relaybrochure.pdf
      >
      >This guy sells big SSRs. I'd like to see a schematic. But it might be 
      >worth looking into. My concern is that he might have miscalculated the 
      >dissipation, but I can't tell from the information.
      >
      >Anybody want to investigate and report back?
      
         Looks like these folks have resurrected an idea
         that was explored and abandoned 33 years ago:
      
      http://www.perfectswitch.com/mobipower110vmodule.htm
      
         This product appears to capitalize on the ability
         of the alternator to output voltage that is many
         times nominal rated output.
      
      http://aeroelectric.com/articles/When_is_110V_not_Over_Voltage.pdf
      
         I note further that this same company offers
         accessories fitted to modern alternators that
         utilize the alternator's higher voltage output
         abilities to accomplish certain welding
         operations.
      
      http://www.perfectswitch.com/alternators.htm
      http://www.perfectswitch.com/mobiarc150.htm
      http://www.perfectswitch.com/remotecontrolmodule.htm
      
         No doubt, modern diodes are considerably more robust
         that those we struggled with in 1975!
      
         They are in CA and too early to talk to on phone
         right now. I've e-mailed them for more information
         on the high current relays.
      
      
         Bob . . .
      
      
Message 7
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  | 
      
      
| Subject:  | Re: AT150 Interrogation Light | 
      
      
      At 06:55 AM 8/1/2008 -0700, you wrote:
      >
      >One cheap "tester" to find the source of the noise, is an old Walkman or 
      >equivalent radio(yeah, those things about 2 generations older than the 
      >Ipod), tuned away from any station, on the AM band, preferably near the 
      >top...1650 or thereabouts.  Then just move it about taking all necessary 
      >precautions with regard to the prop slice/dicer up front. Wherever the 
      >noise peaks, is the location of the offender. I've found bad voltage 
      >regulators that way, among other things. Just a resistance reading doesn't 
      >prove a high tension lead isn't leaking noise, only proves continuity.
      
         Good point! I've still got some pocket transistor
         radios around that have been used for that purpose
         years ago. In my case, I was tracking down arcing
         insulators on power poles. The directional qualities
         of their "loopstick" antennas can be exploited to
         deduce direction of a received signal (as described
         in the 'Connection's chapter on antennas).
      
         I've not had occasion to use one of these radios
         in many years. I heard of a more modern utilization
         in a class on RFI/EMC issues about 15 years ago. The
         speaker told how he boxed a pocket radio up in an
         RF tight, aluminum enclosure. He brought a coax
         connector through the box and tied it to a "primary
         of a transformer" wound around the radio. I think
         it was 5 turns of 22awg wire. He also brought out
         the headphone circuit through RFI filters.
      
         The radio was turned ON, tuned to the high end
         of the band, volume up to max and the box closed.
         A short piece of coax could be fitted at the end
         with either magnetic or electric field probes
      
      http://aeroelectric.com/Pictures/Tools/RF_Antenna_Test_Tools/Sniffer_Probes.jpg
      
         I built these probes for use on a very broadband
         spectrum analyzer. Another name for a fancy
         receiver.
      
         This poor man's electronic "stethoscope" was useful
         for "sniffing" about the airplane for the purpose
         of pinpointing the exit location for a radiated
         noise source. This also assumes that the noise
         source is also broad band with components in the
         audible range. In other words, a relatively clean,
         RF energy or energy at very high frequencies would
         not produce a signal that one would expect to hear
         with this tool.
      
         In the case before us, the repetition rate for
         ignition system currents are very much in the audio
         range and have a base-band component that is at
         or below the broadcast band detection range of
         the pocket radio.
      
         This system would not be useful for finding
         conducted noise sources where the offending signal
         stays pretty much in the wiring. Once it's absolutely
         confirmed that the transponder's antagonist is
         radiated (coming in through the antenna) then
         perhaps Kelly's suggestion offers a useful tool for
         further investigation.
      
         Bob . . .
      
      
Message 8
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  | 
      
      
| Subject:  | Re: Z-19/RB Question | 
      
      
      Bob,
      
      What I was saying is that I use the "alternate feed switch" (labeled 
      "E-Buss") as the primary feed to the E-buss, sort of like an avionics 
      master, and that the diode on the master is now a backup and as such, I 
      need to make sure it hasn't failed leaving only one feed path available 
      to my essential equipment. I do test the feed path, but I don't put it 
      away until needed, as you say, because I feel having it on simplifies 
      the process of load shedding (including the contactor and alternator 
      field) in case of alternator failure (or ground ops). I chose this 
      method because I don't want to risk inflight  re-booting of my EFIS and 
      autopilot by flipping switches in the wrong order. That I don't have to 
      do (admittedly easy) math with the .7 volt diode drop is gravy, not the 
      deciding factor.
      
      It strikes me that, if one didn't mind having an extra switch, the diode 
      could be eliminated as well, leaving the E-Buss as a separate entity 
      from the main buss. The philosophy of having independent feed paths and 
      being able to simply shed unnecessary loads would still be served.
      
      Pax,
      
      Ed Holyoke
      
      
      Robert L. Nuckolls, III wrote:
      > <nuckolls.bob@cox.net>
      >
      > At 10:09 PM 7/31/2008 -0700, you wrote:
      >> <bicyclop@pacbell.net>
      >>
      >> Just one more thing, Mike. I periodically test the diode feeding the 
      >> E-Buss by turning on the master only or turning off the E-buss switch 
      >> first and making sure that the stuff on the E-buss is hot. I don't 
      >> want the alternate feed switch to be the single point of failure.
      >
      >   The e-bus alternate feed switch cannot be a single point
      >   of e-bus failure since it's the second of two independent
      >   feed paths to the e-bus. If the alternate feed path is
      >   pre-flight tested and then "put away unless needed" then
      >   probability of it being available as needed is very high.
      >
      >   This was the spirit and intent of the alternate feed path
      >   philosophy re-enforced by the notion that it was a good
      >   thing to shut battery contactors off during battery only
      >   operations.
      >
      >   Bob . . .
      >
      >
      
      
Message 9
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      Rick:
      
      Thank you for taking the time to respond to the discussion of the broken
      tuning knob on the A200.  That certainly is good news about the part
      availability.  Too often, misunderstandings, half-truths and false
      information are repeated on the internet without question, to everyone's
      detriment.
      
      I will be contacting ICOM for a replacement part, and installing it myself,
      and probably blogging the process.
      
      I agree with your time estimate: about 10 minutes start to finish (1 hour
      minimum charge) seems right, based on my experience.  I am glad that ICOM
      will make this part available to owner-pilot-builders who have the savvy to
      effect this repair.  Thanks for clearing that up.  I own 4 different ICOM
      amateur and aviation radios, and am happy with them all.  Keep up the good
      work!
      
      -Bill Boyd
      
      On Fri, Aug 1, 2008 at 2:41 PM, Rick Waedekin
      <RickWaedekin@icomamerica.com>wrote:
      
      >  Good morning/ afternoon everyone.  I was forwarded a link to your blog
      > site and felt compelled to respond.  It appears there is a lot of
      > misinformation floating around about ICOM so I thought I would clear up a
      s
      > much as I could for you.
      >
      >
      > I would've posted this to your site, but I couldn't figure out how to do
      > so=85
      >
      >
      > 1)       The part needed to fix the busted knob is our part number
      > 0308670106 and anyone can call our parts department and buy one for $64.2
      7.
      > Our parts department contact information is listed on our website but her
      e
      > it is as well.
      >
      > Icom America Parts Department
      > (800) 346-0495
      > Monday - Friday, 8:00 AM-5:00 PM Pacific Time
      >
      > 2)       We have many Avionics Shops that could also get the part and fix
      > it for you.  Gulf/ Pacific Coast, Eastern Avionics, Aircraft Spruce,
      > American Avionics, Banyan just to name a few shops.  Plus, we have our
      > Service department here in Bellevue, WA as well as our regional service
      > center in Anderson, SC that could fix this for you as well.  All of this
      > information is right on our website as well.
      >
      > 3)       It only takes one hour to repair/ replace the rotary encoder on
      > the A200.
      >
      >
      > Obviously we'd rather have one of our dealers/ repair facilities fix this
      > problem as there are a lot of ribbon cables and such that if not treated
      > correctly can do even more damage to the unit, and wind up costing even m
      ore
      > money down the road.
      >
      >
      > On a final note, as a rule ICOM's parts department supports most of the
      > parts needed to fix our products for up to 10 years after the last date o
      f
      > manufacture.
      >
      >
      > I hope this cleared up some of the questions floating around.
      >
      >
      > Thanks for your support of ICOM products.
      >
      >
      > *Rick Waedekin |* National Sales Manager | *Icom America, Inc.*
      >
      > 2380 116th Ave NE | Bellevue, WA | 98004
      >
      >
      
Message 10
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  | 
      
      
| Subject:  | Re: FYI: Powergate | 
      
      
      At 09:21 AM 8/1/2008 -0500, you wrote:
      ><nuckolls.bob@cox.net>
      >
      >At 08:31 AM 7/30/2008 -0700, you wrote:
      >><emjones@charter.net>
      >>
      >>See: http://www.perfectswitch.com/downloads/relaybrochure.pdf
      
         Just got a data package from Perfect Switch on their
         "Power-Gate" products. I've combined all the images and
         files into a single .pdf at:
      
      http://tinyurl.com/59faul
      
         The information is fairly descriptive. The text of
         an accompanying e-mail stated that these are, for
         the moment, un-directional devices. This means that
         effects of the parasitic diode in their large array
         of Power FET devices will "backfeed" power to the source
         should the votlage on the load side become high enough.
         It also means that they're not ready to perform as a
         battery contactor with equally low resistance connection
         for electron flow both directions through the device.
      
         Prices for the current offerings are given on page
         5 of the file. Here we find that a relay suited for
         carrying starter currents will set you back over
         $300.
      
         I'm told by my local Gigavac rep that a sample contactor
         has been ordered for us to play with.
      
         Bob . . .
      
      
Message 11
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  | 
      
      
| Subject:  | Re: Z-19/RB Question | 
      
      
      At 11:33 AM 8/1/2008 -0700, you wrote:
      >
      >Bob,
      >
      >What I was saying is that I use the "alternate feed switch" (labeled 
      >"E-Buss") as the primary feed to the E-buss, sort of like an avionics 
      >master, and that the diode on the master is now a backup and as such, I 
      >need to make sure it hasn't failed leaving only one feed path available to 
      >my essential equipment. I do test the feed path, but I don't put it away 
      >until needed, as you say, because I feel having it on simplifies the 
      >process of load shedding (including the contactor and alternator field) in 
      >case of alternator failure (or ground ops). I chose this method because I 
      >don't want to risk inflight  re-booting of my EFIS and autopilot by 
      >flipping switches in the wrong order. That I don't have to do (admittedly 
      >easy) math with the .7 volt diode drop is gravy, not the deciding factor.
      >
      >It strikes me that, if one didn't mind having an extra switch, the diode 
      >could be eliminated as well, leaving the E-Buss as a separate entity from 
      >the main buss. The philosophy of having independent feed paths and being 
      >able to simply shed unnecessary loads would still be served.
      
         The diode was considered necessary and useful to eliminate
         the potential for having both switches closed at the same time
         and having the main bus take power through the e-bus alternate
         feed path . . . a bonus of using the diode IS the automatic
         switching of one feed path and elimination of the switch.
      
         Of course, how you choose to modify the system and its
         operation is a personal decision.
      
         Bob . . .
      
      
Message 12
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  | 
      
      
| Subject:  | Transpo V1200 regulator | 
      
      Okay, I tried looking at some old posts to help me figure out how to wire a
      regulator  I have but I think it just confused me more..
      
      
      I have a Transpo V1200 regulator for a high amp output Alternator aka:
      
      http://www.aeroelectric.com/Mfgr_Data/Regulators/Transpo/V1200_Transpo.pdf
      
      
      Question is what all connects to all the terminals listed?
      
      The label just shows:
      
      "I"
      
      "A"
      
      "S"
      
      "F"
      
      
      "Stator Output"  my guess is leave disconnected maybe use for testing ?
      
      
      "B-"  my guess is ground here..
      
      
      Can anybody find a manual on what goes where? Or more to the point how to
      incorporate it into the Z diagrams ?
      
      
      Thanks Jeff.
      
      
Message 13
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| Subject:  | Official AeroElectric-List FAQ (Frequently Asked Questions) | 
      
      
      Dear Listers,
      
      Please read over the AeroElectric-List Frequently Asked Questions (FAQ) below.
      The
      complete AeroElectric-List FAQ including the Usage Guidelines can be found at the
      following URL:
      
         http://www.matronics.com/FAQs/AeroElectric-List.FAQ.html
      
      Thank you,
      
      Matt Dralle
      Matronics Email List Administrator
      
      
      [ Note: This FAQ was designed to be displayed with a fixed width font such as
               Courier.  Proportional fonts will cause display formatting errors. ]
      
      
         This FAQ can also be viewed in HTML online at the following address:
         
                       http://www.matronics.com/FAQ/AeroElectric-List.htm
      
      
              ************************************************************
              ******* LIST POLICIES AND FREQUENTLY ASKED QUESTIONS *******
              ************************************************************
      
      
      PLEASE READ.  This document contains AeroElectric-List policies and information
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      running smoothly for all of us.
      
      
      ******************************************
      *** Quick Start Guide to List Features ***
      ******************************************
      
         There are many features available on the Matronics Email Lists and each
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      ****************************************
      
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            Look for the link "Image Resizer"
      
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      *******************
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      *******************
      
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        Now some caveats:
      
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      ****************************
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      *******************************
      *** List Member Information ***
      *******************************
      
         If you have not done so already, please email me your phone numbers and 
         paper mail address in the following format:
      
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                       Tower, CA 91234-1234
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         Please forward this information to the following email address:
      
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      ****************************************
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         You may view all List content on the Forums without any special login.
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         Subscribe to the respective Email List as described above to receive the
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      *********************************
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      *********************************
      
      In an attempt to make it easy to store and find structured and often accessed 
      information, Matronics has installed a Wiki at:
      
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      The Wiki allows individuals to create web pages to contain useful information 
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      While constructing pages for the Wiki is not difficult, some may not be 
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                      wiki-support@matronics.com
      
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      *********************
      *** List Archives ***
      *********************
      
         A file containing of all of the previous postings to the AeroElectric-List is
         available on line.  The archive file information is available via the 
         Web and FTP in a number of forms.  Each are briefly described below:
      
      
         * AeroElectric-List.FAQ 
      
                  - Latest version of the AeroElectric-List Frequently Asked Question
      
                    page (this document).
      
         * AeroElectric-Archive.digest.complete 
      
                  - Complete file with most of the email header info removed and 
                    page breaks inserted between messages.
      
         * AeroElectric-Archive.digest.vol-??  
      
                  - Same as the file above, but broken up into small sections that 
                    can more easily handled.
      
         * AeroElectric-Archive.digest.complete.zip 
      
                  - Same as the AeroElectric-Archive.digest.complete file above, but
      
                    in PKZIP format.  Use "binary" data transfer methods.
      
         * AeroElectric-Archive.digest.complete.Z 
      
                  - Same as the AeroElectric-Archive.digest.complete file above, but
      in 
                    UNIX compress format.  Use "binary" data transfer methods.
      
      
        Download Via FTP
        ----------------
      
         The archive file is available via anonymous FTP from ftp.matronics.com
         in the "/pub/Archives" directory.  It is updated daily and can be found in
         a number of formats as described above. (All filenames are case sensitive.)
      
                        ftp://ftp.matronics.com/pub/Archives
      
      
        Download Via Web
        ----------------
      
         The archives are also available via a web listing.  These can be found
         toward the bottom of the following web page:
      
                        http://www.matronics.com/archives
      
      
      ******************************************
      *** Complete List Web Archive Browsing ***
      ******************************************
      
         All messages posted to the AeroElectric-List are also available using the
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         in the List are indexed, and individual sub-archives can be browsed.
      
                        http://www.matronics.com/archive/archive-index.cgi?AeroElectric
      
      
      *****************************************
      **** High-Speed Archive Search Engine ***
      *****************************************
      
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      ****************************
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      ****************************
      
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         !! ==> Please including the following information with each submission:
      
                        1) Email Lists that they are related to.
                        2) Your Full Name.
                        3) Your Email Address.
                        4) One line Subject description.
                        5) Multi-line, multi-paragraph description of topic.
                        6-x) One-line Description of each photo or file
      
         Prior to public availability of the files and photos, each will be scanned
         for viruses.  Please also note that the process of making the files and
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         Following the availability of the new Photoshare, an email message will be
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      **************************
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      **************************
      
         A complete Matronics Email List Archive CD is available that contains
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      **********************************
      
         The Matronics Lists are run *completely* through the support of it members.
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      ******************************************************************************
                           AeroElectric-List Usage Guidelines
      ******************************************************************************
      
      The following details the official Usage Guidelines for the AeroElectric-List.
      You are encouraged to read it carefully, and to abide by the rules therein.
      Failure to use the AeroElectric-List in the manner described below may result 
      in the removal of the subscribers from the List.
      
      
      AeroElectric-List Policy Statement
      
      The purpose of the AeroElectric-List is to provide a forum of discussion for
      things related to this particular discussion group.  The List's goals
      are to serve as an information resource to its members; to deliver
      high-quality content; to provide moral support; to foster camaraderie
      among its members; and to support safe operation.  Reaching these goals 
      requires the participation and cooperation of each and every member of 
      the List.  To this end, the following guidelines have been established:
      
      
       - Please keep all posts related to the List at some level.  Do not submit
         posts concerning computer viruses, urban legends, random humor, long
         lost buddies' phone numbers, etc. etc.
      
       - THINK carefully before you write.  Ask yourself if your post will be
         relevant to everyone.  If you have to wonder about that, DON'T send it.
      
       - Remember that your post will be included for posterity in an archive
         that is growing in size at an extraordinary rate.  Try to be concise and
         terse in your posts.  Avoid overly wordy and lengthy posts and
         responses.
      
       - Keep your signature brief.  Please include your name, email address,
         aircraft type/tail number, and geographic location.  A short line
         about where you are in the building process is also nice.  Avoid
         bulky signatures with character graphics; they consume unnecessary
         space in the archive.
      
       - DON'T post requests to the List for information when that info is
         easily obtainable from other widely available sources.  Consult the
         web page or FAQ first.
      
       - If you want to respond to a post, DO keep the "Subject:" line of
         your response the same as that of the original post.  This makes it
         easy to find threads in the archive.
      
       - When responding, NEVER quote the *entire* original post in your
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         can not be overstated!
      
       - When the poster asks you to respond to him/her personally, DO NOT
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      -------
      
      
      [This is an automated posting.]
      
      do not archive
      
      
Message 14
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  | 
      
      
| Subject:  | Official AeroElectric-List Usage Guidelines | 
      
      
      Dear Listers,
      
      Please read over the AeroElectric-List Usage Guidelines below.  The complete
      AeroElectric-List FAQ including these Usage Guidelines can be found at the
      following URL:
      
         http://www.matronics.com/FAQs/AeroElectric-List.FAQ.html
      
      Thank you,
      
      Matt Dralle
      Matronics Email List Administrator
      
      
      ******************************************************************************
                           AeroElectric-List Usage Guidelines
      ******************************************************************************
      
      The following details the official Usage Guidelines for the AeroElectric-List.
      You are encouraged to read it carefully, and to abide by the rules therein.
      Failure to use the AeroElectric-List in the manner described below may result 
      in the removal of the subscribers from the List.
      
      
      AeroElectric-List Policy Statement
      
      The purpose of the AeroElectric-List is to provide a forum of discussion for
      things related to this particular discussion group.  The List's goals
      are to serve as an information resource to its members; to deliver
      high-quality content; to provide moral support; to foster camaraderie
      among its members; and to support safe operation.  Reaching these goals 
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      -------
      
      
      [This is an automated posting.]
      
      do not archive
      
      
 
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