AeroElectric-List Digest Archive

Thu 09/28/06


Total Messages Posted: 24



Today's Message Index:
----------------------
 
     1. 05:36 AM - Re: List: Stick Transfer function (glen matejcek)
     2. 05:37 AM - Re: Rotax 912S starter relay diode (Robert L. Nuckolls, III)
     3. 05:40 AM - Re: Lap solder or D-Sub Pins (Robert L. Nuckolls, III)
     4. 05:53 AM - Re: 500W Batt tester (Robert L. Nuckolls, III)
     5. 06:02 AM - Re: Best wiring techniques to use? (Robert L. Nuckolls, III)
     6. 06:26 AM - Re: Eaton Starter Contactor Website (Robert L. Nuckolls, III)
     7. 07:18 AM - Re: Whelen Strobes Blowing Fuses (Robert L. Nuckolls, III)
     8. 07:49 AM - Re: Whelen Strobes Blowing Fuses (Peter Braswell)
     9. 08:53 AM - A Proud Announcement (EuropaXSA276@aol.com)
    10. 09:25 AM - Re: A Proud Announcement (Hinde, Frank George (Corvallis))
    11. 10:40 AM - Z-13 Alternator and Pmag Question (drill_and_buck)
    12. 10:53 AM - Need 0.3 amps at 28v from a 14v system (Matthew Brandes)
    13. 11:46 AM - Re: Best wiring techniques to use? ()
    14. 01:10 PM - Re: Rotax 912S starter relay diode (billmileski)
    15. 02:09 PM - Re: Mogas versus 100LL (Mostly Off Topic)  (Jerry2DT@aol.com)
    16. 02:09 PM - Re: Mogas versus 100LL (Mostly Off Topic)  (Jerry2DT@aol.com)
    17. 02:52 PM - Re: Re: Mogas versus 100LL (Mostly Off Topic)  (Hinde, Frank George (Corvallis))
    18. 03:10 PM - Re: A Proud Announcement (A DeMarzo)
    19. 03:49 PM - Re: Re: Mogas versus 100LL (Mostly Off Topic)  (6440 Auto Parts)
    20. 06:37 PM - Re: Whelen Strobes Blowing Fuses (Robert L. Nuckolls, III)
    21. 06:53 PM - Re: Whelen Strobes Blowing Fuses (Peter Braswell)
    22. 07:04 PM - Grounding (Dennis Johnson)
    23. 08:55 PM - battery cables  (bob noffs)
    24. 09:13 PM - Re: battery cables  (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 05:36:43 AM PST US
    From: "glen matejcek" <aerobubba@earthlink.net>
    Subject: RE: List: Stick Transfer function
    --> AeroElectric-List message posted by: "glen matejcek" <aerobubba@earthlink.net> Hi Mark- >Next question. I am investigating how to swap all stick switch functions >from L to R (Infinity grip) by some reliable, safe means. About 8 wires minimum > >(4-way trim, CWS, PTT, gnd). I would prefer a simple switch as opposed to >using relays (4PDTx2) but I'm beginning to think there is no source for an 8PDT >switch. > >Any suggestions or am I barking up the wrong tree and there's a simpler way >to do this? > >THANKS! >Mark Phillips I've got similar objectives and somewhat different circumstances, as I've got MAC/RAC trim equipment in an RV-8. I believe that all the equipment functions the same though, IE they operate by switching to ground. I tried to come up with a practical, reliable way to avoid using the MAC/RAC trim relay$ to integrate the control functions of two sticks, but failed. They are just too perfect for the job of controlling one servo with two sets of control switches. The other issues I was concerned with were trim system failure leading to a trim runaway, and inappropriate operating of the switches in the back seat. This was addressed rather handily with one progressive DPDT switch near the throttle quadrant. The way my system is configured, my fwd PTT goes to ground uninterrupted. The ground for the fwd stick trim controls goes to one set of contacts on the switch, and the ground for all the rear stick functions goes to the other set of contacts on the same switch. The result is that when the progressive switch is in the up position, all functions are operative. In the center position, the rear stick is inop and the front is fully functional. In the down position the fwd stick trim functions, in addition to all the rear stick functions, are inop. This leaves the fwd stick PTT, A/P DISC, and EFIS engine page call up/dismiss functions available. FWIW- BTW, what is CWS? Surely it's not Control Wheel Steering, is it? Or did you get a deal on surplus Boeing parts ; - ) glen matejcek aerobubba@earthlink.net


    Message 2


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    Time: 05:37:39 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Rotax 912S starter relay diode
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 12:30 PM 9/27/2006 -0700, you wrote: >--> AeroElectric-List message posted by: "billmileski" <mileski@sonalysts.com> > >Hi, > >Does anyone know if the Rotax 912 series starter relay has a built-in >shunt diode? Don't know. If you've got access to a 'scope, it's easy to find out. Even easier to add a diode just for grins. Two diodes doesn't hurt a thing, no diodes is hard on starter switches. >I am considering adding a diode across my starter switch, Not across the switch, across the contactor coil. See http://aeroelectric.com/articles/spikecatcher.pdf > . . . but then I came across an application note from Tyco, regarding shunt diodes across their relays. Apparently a zener in series >with a diode is better, to allow the relay to develop some EMF, otherwise the opening dynamics can be somewhat thwarted. If so, the starter >relay can actually be more likely to fail to open, and/or life can be shortened. Interesting read at >http://relays.tycoelectronics.com/appnotes/app_pdfs/13c3264.pdf This document is an excellent example of poor decisions made on poor science. The title: "Coil Suppression Can Reduce Relay Life" certainly gets your attention. The writer goes to some effort to explain how coil suppression can have a profound effect on RELAY RELEASE TIME which is easy to demonstrate and explain. Then in the last 5 paragraphs on page one, launches into some assertions about the effects of a slowed decay of the magnetic field on contact separation speeds but no demonstrations or even a mathematical modeling of the event to support the assertions. This discussion came up on the List some months ago. I've excerpted portions of that discussion below: ------------------------- >Coil Suppression: > >MOVs are considered to be better than diodes, although they have higher >impedance. But MOVs typically have a limited lifetime. The lifetime issue controls when the MOV is stressed repeatedly to its maximum rated energy levels . . . in coil spike suppression, the energies are tiny by comparison and life-limits do not become an issue. >Diodes are not the best method today. Not even the second-, third-, or >fourth- best method. But in the 1960's they were the way to go. <snip> Measurements on my bench have failed to demonstrate the suggestion. A number of papers have been cited over the years, some written by some folks who work for big name companies like Tyco-Amp, Teledyne, etc. wherein authors have suggested that the readily observable effects of plain diodes on opening delay (no big deal in 99.99% of applications) directly translates to slower contact spreading velocity (extended arcing during contact break). Two separate conditions are in play. (1) slower rate of decay in the relay or contactor's coil current and (2) rate of decay in the magnetic attraction force as the moveable armature begins to separate from its seated position within the device. The diode has a profound effect on (1) but a small effect on (2). Most of the papers I've read accurately observed and discussed (1) and even did some measurements but then went on to improperly assume that similar effects would be noted for (2) as well. The trace at: http://www.aeroelectric.com/Pictures/Curves/704-1DelayNoDiode.gif Shows contact OPENING DELAY of an S704-1 plastic high current relay when no diode was present across the coil and the coil current was being interrupted by the "perfect switch". Note the expected coil spike on channel 2 and the opening delay of about 2.5 mS. You can see the arcing across spreading contacts if you look carefully at the falling trace on channel 1. http://www.aeroelectric.com/Pictures/Curves/704-1DelayWithDiode.gif This trace shows what happens when we use the plain-vanilla diode across the coil. Yes, OPENING DELAY goes up by a factor of 500% to about 12.5 mS. Now, let's go take a close look at the arcing phenomenon noted in the two traces above . . . http://www.aeroelectric.com/Pictures/Curves/704-1OpeningTimeNoDiode.gif . . . with no diode, a series of about 10 measurements produced an opening time (ARC DURATION) that averaged 210 uS. In the next trace . . . http://www.aeroelectric.com/Pictures/Curves/704-1OpeningTimeWithDiode.gif . . . the diode was put back on and we see an average of 230 uS ARC DURATION for an increase of about 10% I did similar experiments with other relays and did not formalize the data gathering but got similar results. Bottom line is that the use of the lowly diode for coil spike suppression does not deserve relegation to the dust bins of electronic history as a 5th-rate spike suppression technique. Unfortunately, some big names working for big companies have stubbed their toes on significant but error driven assumptions. The repeatable experiment has demonstrated otherwise. Continued use of diodes as suggested in the 'Connection and on many drawings posted to the website is not a recipe for failure. Substitution of a more "modern" technique will produce no observable effect on the service life of your relays and contactors. ------------------------ Demonstrable differences for contact spreading velocity and potential to arc for diodes versus any other choice are tiny. Relay and switch lives in industrial parlance is stated in the tens of thousands of cycles. There are few switches and relays in our airplanes that will get even 1,000 cycles in the lifetime of the airplane. Nonetheless, we suffer significant switch and contactor failures . . . mostly for environmental stresses over long periods of time . . . commonly known as old age. There's nothing inherently BAD about coil suppression techniques other than plain diodes but nothing overwhelmingly good about them either. Bottom line is use what ever technique suits your fancy but don't discount the lowly diode based on the assertions of folks who demonstrate one effect and then extrapolate a second effect without supporting data. Further, be especially wary of papers like the one cited above where prestige of either people or the companies they work for is the motivating force to do or not to do any particular thing. I've sat across the table many times with folks from big name companies attempting to deduce root cause of failures for their products on our products. When the problem is finally solved, it's all too often that we end up knowing more about the supplier's product than they do. Bob . . .


    Message 3


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    Time: 05:40:15 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Lap solder or D-Sub Pins
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 09:22 PM 9/27/2006 -0500, you wrote: >--> AeroElectric-List message posted by: "Emrath" <emrath@comcast.net> > >Thanks Bob, Just the encouragement I needed to go "experimenting" by cutting >off the existin connectors and getting the soldering iron going. >Marty I think you mentioned K wire in your original posting. You'll need the mini-torch and silver solder for those. But if you cut the existing connectors off, then replacing them with crimped-on terminals will get rid of the excess wire and replace the connectors with as good or better than supplied from the factory. Bob . . .


    Message 4


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    Time: 05:53:20 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: 500W Batt tester
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 07:35 AM 9/25/2006 -0700, you wrote: >--> AeroElectric-List message posted by: Christopher Stone ><rv8iator@earthlink.net> > >Bob et al.. > >FYI > >West Mountain Radio has a new CBA (computerized battery tester) capable of >loading to 500 watts. It doesn't appear on the website yet, but they are >advertising it in the model press. I have been using their CBA II (150W) >for the past year+ and have found it the best tool available for >generating battery discharge curves and managing the health of >rechargeable batterys. > >A 500 watt capable analyzer would allow simulation of battery out and/or >alternator out scenarios as well as full load testing of 40 amp >alternators. Plus much more! > >I am in no way affiliated with the manufacture, sale or distribution of >this product. I am just a very satisfied end user. > >Chris Stone I agree on the CBAII . . . I've got two of them! I've 'bugged' them from time to time about the output format of their software and even offered to do an "engineers version" to share with them if they'd give us the USB communications protocols for the CBAII but so far, no bites. However, they do offer comma de-limited export capability that I've been able to use to great advantage. It's a great tool for the money. Bob . . . --------------------------------------------------------- < What is so wonderful about scientific truth...is that > < the authority which determines whether there can be > < debate or not does not reside in some fraternity of > < scientists; nor is it divine. The authority rests > < with experiment. > < --Lawrence M. Krauss > ---------------------------------------------------------


    Message 5


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    Time: 06:02:05 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Best wiring techniques to use?
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 11:19 PM 9/24/2006 +0000, you wrote: >--> AeroElectric-List message posted by: <rparigor@suffolk.lib.ny.us> > >Need a bit of help to determine best wiring techniques to use. > >This is for a Europa XS/Rotax 914 and B+C SD20S/LR3C, start point for >schematic was Z13/8. > >Battery is 10 feet behind motor, Flaming River mechanical battery cut off >switch 3 feet ahead of battery aft side of passenger headrest. >http://www.flamingriver.com/index.cfm?ptype=article&article_id=22 > >1) I am looking to use #4 MIL-W-22759/16 Tefzel wire for battery and >ground. There will be approx a 3 foot run of unprotected wire to the >battery cut off switch. Is there any extra protection that would be >prudent to incorporate? No >Some sort of robust sleeve on 1 wire, or a fusible >link? Or just not worry about it (not run too close near anything that >conducts)? I have the heavy duty Rotax starter, supposedly draws less amps >than old style, old style starter draw was I think 60 amps, not sure what >momentary is. It's a plastic airplane . . . don't worry about it. >2) I need to somehow get power and ground to 2 fuel pumps, wingtip >Strobe/Position LEDs and pitch servo. The headrest is approx 6 feet closer >to the battery (14 foot round trip) compared to the firewall mounted >ground and main bus. If I put a mini power and ground bus in or near the >headrest, would I be negating the concept of single point ground? Would >stealing power from the NO side of the battery cut off likely cause any >noise or other problems? Or just make extra runs from firewall? Minimize the numbers of busses. Run from the firewall. >3) Would it be advisable to series the battery cut off with the negative >or positive? Reason? I don't have any science to back this up, but I read >that when making model electric aeroplane battery packs, if you need to >make one lead longer than the other, make the negative longer than the >positive, it can help with black wire disease (what I have always done)?? >Overall scheme, plenty more time will be spent with battery cutoff opened. Either way. >4) I will need to somehow break into the #4 battery wire not going to the >battery cut off switch. Instead of cutting the wire and putting on a lug >on each side, and screwing them back together along with an additional #10 >wire ring, could I carefully strip, lets say an inch of insulation off the >#4, and strip 3" off the #10, then strip back the #10 to 1" except for 2 >strands, then wrap the 2 strands over the 1" of #4 and 1" of #10 and >solder/heat shrink? I would use the adhesive lined heat shrink. That will cause some folks to roll their eyes back and mumble unkind things about you . . . but there's nothing wrong with the physics or failure modes and is probably a more reliable joint (low parts count, no threaded fasteners). >5) What is good practice to follow, the number of lugs I can stack on the >NO side of the battery cutoff switch stud? Depends on stud length. You need to see one full thread on the OFF-side of the nut when the joint is finished. >6) I forget the exact diameter of the NO side of the battery cutoff switch >stud, lets say it is 5/16". If lets say I wanted to stack a #4 and a >#10,is it acceptable to stack a ring terminal that has a smaller footprint >on top of one with a larger footprint? Or in this instance because loss of >this connection can cause loss of main and e-bus, use the same size lug, >make a brass insert and crimp/solder in the smaller wire? At the current levels you're dealing with, surface areas are not going to be an issue so much as joint make-up forces. Torque the nut down to about 1/2 the value recommended for steel of the same size/thread. >7) The Flaming River switch has copper threaded studs, came with a brass >nut and brass lock-washer. Would it be advisable to use a Phosphor bronze >star washer instead of the brass lock-washer? If the lockwasher is the typical automotive split-ring variety, pitch it an forget it. If it's an internal toothed lockwasher, leave it in the makeup of the joint but if you're running out of stud length, leave it off and use some non- permanent locking guckum on the nut. E-6000 adhesive works nice. It extrudes out of the hi-pressure contact areas between threads and nut but keeps the nut secure for vibration induced loosening. Finally, not so strong a grip as to keep the nut from being removed. Bob . . .


    Message 6


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    Time: 06:26:21 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: Eaton Starter Contactor Website
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 12:49 AM 9/24/2006 -0400, you wrote: >--> AeroElectric-List message posted by: <jlundberg@cox.net> > >Does anyone know the website for the Eaton Starter contactors??. I need >one for a Lyc IO-540. > >Thanks The catalog sheet for Eaton-CH 6041 series contactors can be found at: http://www.aeroelectric.com/Mfgr_Data/Contactors/Eaton_CH/6041SeriesPowerRelays.pdf Few folks stock these things. I used to get them through Carlton-Bates in Little Rock, AR. Bob . . . --------------------------------------------------------- < What is so wonderful about scientific truth...is that > < the authority which determines whether there can be > < debate or not does not reside in some fraternity of > < scientists; nor is it divine. The authority rests > < with experiment. > < --Lawrence M. Krauss > ---------------------------------------------------------


    Message 7


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    Time: 07:18:50 AM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Whelen Strobes Blowing Fuses
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 09:28 PM 9/12/2006 -0400, you wrote: >--> AeroElectric-List message posted by: "Peter Braswell" ><pbraswell@alterthought.com> > >Bob, >Easy enough to do! I'll give it a whirl and see what happens. And to >answer your question, yes the strobe work fine when it is working. > >Thanks! >Peter Peter, what have you discovered since we last talked about the blowing fuse problem? Bob . . .


    Message 8


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    Time: 07:49:48 AM PST US
    From: "Peter Braswell" <pbraswell@alterthought.com>
    Subject: Whelen Strobes Blowing Fuses
    --> AeroElectric-List message posted by: "Peter Braswell" <pbraswell@alterthought.com> Hey Bob! Thanks for wanting the follow up! I went flying the other night with a 15amp fuse as per your recommendation. Prior to blasting off, I cycled the strobes a few times with no problems. When I got back down the strobes were still flashing so I think that got it! And can I say how GREAT it is to have a flying airplane!!!?? I flew until the sun was just dipping below the horizon. The night was dead calm and my home airport is a great little 3200' foot sod strip. All that (and the flashing strobes) made for a very picturesque approach and landing!!! Doesn't get much better than that! Thanks! Peter -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Thursday, September 28, 2006 10:17 AM Subject: RE: AeroElectric-List: Whelen Strobes Blowing Fuses --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" --> <nuckollsr@cox.net> At 09:28 PM 9/12/2006 -0400, you wrote: >--> AeroElectric-List message posted by: "Peter Braswell" ><pbraswell@alterthought.com> > >Bob, >Easy enough to do! I'll give it a whirl and see what happens. And to >answer your question, yes the strobe work fine when it is working. > >Thanks! >Peter Peter, what have you discovered since we last talked about the blowing fuse problem? Bob . . .


    Message 9


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    Time: 08:53:51 AM PST US
    From: EuropaXSA276@aol.com
    Subject: A Proud Announcement
    On Wednesday, September 27, 2006 my son Brennan J. Skelly took his first sol o flight. The flight took place at 10:45 Central time at Grand Prairie Municipal Airport located in Grand Prairie Texas USA. The sky was a pristin e blue and the winds were light and variable. After a written examination and a few test runs, Brennan's instructor released him for solo. Brennan flew the pattern and made 2 perfect landings and =9Cone like his dad makes=9D. (Whatever that is supposed to mean!!) Brennan is age 19. He currently attends a local college and in 2007 he will transfer to North Dakota University to attend the Federal Aviation Administration Air Traffic Controller program. He works part time at Grand Prairie Municipal Airport with the very important duty of fueling the general aviati on fleet. He is also certified to =9CHot Fuel=9D the emergency hel icopters that are based at that location. In his off times he enjoys working in the shop with his father on the Europa XS project. Brennan represents the third generation of pilots for the Skelly family. Upo n completion of his flight he notified his 90 year old Grandfather James E. Skelly, who proudly flew in the European theater of W.W.II and later became a military flight instructor. Way to go son! Your father is very proud. Brian Skelly Europa XS TriGear #A276 North Texas USA You can see my build photos at: http://www.europaowners.org/BrianS


    Message 10


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    Time: 09:25:55 AM PST US
    Subject: A Proud Announcement
    From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com>
    Ahh yes a very proud moment indeed. Very well done! Frank Zenair Zodiac 400hours Rv7a 22 hours ________________________________ Brennan represents the third generation of pilots for the Skelly family. Upon completion of his flight he notified his 90 year old Grandfather James E. Skelly, who proudly flew in the European theater of W.W.II and later became a military flight instructor. Way to go son! Your father is very proud. Brian Skelly Europa XS TriGear #A276 North Texas USA You can see my build photos at: http://www.europaowners.org/BrianS


    Message 11


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    Time: 10:40:38 AM PST US
    Subject: Z-13 Alternator and Pmag Question
    From: "drill_and_buck" <mdraper@nww.com>
    --> AeroElectric-List message posted by: "drill_and_buck" <mdraper@nww.com> I am using Z-13 as a baseline to design my electrical system for my RV-8. I have read the Aeroelectric book and attended one of Bob's weekend seminars, but haven't yet quite grasped all the concepts. I would appreciate it if someone could help me better understand the rationale behind the alternator field circuit. In particular.. 1. What is the rationale behind using a fuselink AND a 5A breaker on the alternator field circuit? Wouldn't the breaker eliminate the need for a fuselink? 2. If the fuselink is optional, would it be practical to just use a 5A fuse rather than a breaker? On the P-Mag (self powered mag) circuit... 1. What is the benefit of wiring the P-Mags to the battery buss. Why not just wire the P-Mags to the main power bus. Thanks in advance for your replies.. Mike Draper RV-8 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=64522#64522


    Message 12


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    Time: 10:53:34 AM PST US
    From: "Matthew Brandes" <matthew@n523rv.com>
    Subject: Need 0.3 amps at 28v from a 14v system
    I have a KLN-89B, KX-155 and 209A indicator. I'd like to install the MidContinent GPS Annunciator to use but the 14 versions of these are scarce on the used market and both the new/used ones are pricey! I see 28v units all the time and they are a lot less. Is there a simple easy solution to power this 28v unit that draws 0.30amps from a 14v bus? I search through the archives and didn't find much. Matthew N523RV :: RV-9A :: 115 hours


    Message 13


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    Time: 11:46:00 AM PST US
    Subject: Re: Best wiring techniques to use?
    From: <rparigor@SUFFOLK.LIB.NY.US>
    --> AeroElectric-List message posted by: <rparigor@suffolk.lib.ny.us> Hello Bob "Need a bit of help to determine best wiring techniques to use." Much appreciate your input. Sincerely Ron Parigoris Do not archive


    Message 14


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    Time: 01:10:12 PM PST US
    Subject: Re: Rotax 912S starter relay diode
    From: "billmileski" <mileski@sonalysts.com>
    --> AeroElectric-List message posted by: "billmileski" <mileski@sonalysts.com> Thanks for the info, and the pdf reminding me that what I really wanted was a diode across the coil, not the switch. And I'll use a scope as you suggested if no protection seems to be already in place. Regards, Bill Read this topic online here: http://forums.matronics.com/viewtopic.php?p=64550#64550


    Message 15


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    Time: 02:09:44 PM PST US
    From: Jerry2DT@aol.com
    Subject: Re: Mogas versus 100LL (Mostly Off Topic)
    Excellent article on Ethanol in current Consumer Reports. A couple things for sure are that Ethanol has 30% less BTU's than Gasoline 125k btu/gal vs. 84.4), thereby translating to 32% less mileage per gal. Ethanol is cleaner, which I guess is why it is mandated in some parts. I track my car gas mileage very closely and get 8% less mpg when using a mix. The math doesn't come out quite right with the btu's, but it is a fact, at least for my car. It is alleged that Ethanol rots some seals, gaskets. My 1996 Honda motorcycle specifically disallows it's use. There is no way I'll ever use a mix of gas/ethanol in my aircraft. Superior also bans Ethanol btw, although encourages use of premium mogas for their XP360's... FWIW, .02, etc. Jerry Cochran From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> --> AeroElectric-List message posted by: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> Indeed yes are...but do you measure the RVP before you use it?...Even if the RVP is a little high you can ajust your flying to suit. As a bit of an aside I probably wouldn't store mogas for 6 months before using it. More of a question is wat if ethanol appears in the mix...i have an invite to phone Todd at Peterson for the low down on why not to use Ethanol...I'm not convinced on that one...at least not yet. More to come


    Message 16


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    Time: 02:09:44 PM PST US
    From: Jerry2DT@aol.com
    Subject: Re: Mogas versus 100LL (Mostly Off Topic)
    Excellent article on Ethanol in current Consumer Reports. A couple things for sure are that Ethanol has 30% less BTU's than Gasoline 125k btu/gal vs. 84.4), thereby translating to 32% less mileage per gal. Ethanol is cleaner, which I guess is why it is mandated in some parts. I track my car gas mileage very closely and get 8% less mpg when using a mix. The math doesn't come out quite right with the btu's, but it is a fact, at least for my car. It is alleged that Ethanol rots some seals, gaskets. My 1996 Honda motorcycle specifically disallows it's use. There is no way I'll ever use a mix of gas/ethanol in my aircraft. Superior also bans Ethanol btw, although encourages use of premium mogas for their XP360's... FWIW, .02, etc. Jerry Cochran From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> --> AeroElectric-List message posted by: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> Indeed yes are...but do you measure the RVP before you use it?...Even if the RVP is a little high you can ajust your flying to suit. As a bit of an aside I probably wouldn't store mogas for 6 months before using it. More of a question is wat if ethanol appears in the mix...i have an invite to phone Todd at Peterson for the low down on why not to use Ethanol...I'm not convinced on that one...at least not yet. More to come


    Message 17


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    Time: 02:52:31 PM PST US
    Subject: Re: Mogas versus 100LL (Mostly Off Topic)
    From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com>
    When i spoke to Superior they stated Vapour lock as the issue with ethanol mix...But when i asked if they really meant vapour lock or simply boiling of fuel in the injector lines ...Which is not vapour lock I did not get an answer. Secondly with my Airflow Performance system it can run on 100% ethanol if you so desire. I have high regard for Superior, don't get me wrong but there are MANY OWTs out there that one is forced to question. ECI states lead being a lubricant for valve seats as Gospel for example...I don't buy it because, 1 it sounds ridiculous and 2 there is more and more evidence to the contrary. Now in order to preserve the warranty (if there really is one) ECI demand that you use 100LL duting break in...OK for sure i will only start feeding in mogas after 25 hours or so...Not worth the risk. Soo..if you have a properly designed fuel system (my pumps are in the wingroots) I'm having a hard time understanding the objection to ethanol mixes...Apart from the fact we're getting short changed (lower grade fuel)to support our totally excessive farm production of course...:) Now it maybe the injector line boiling is so bad it s difficult to get the engine to run smooth...Definatly a possibility. I will phone Todd Peterson next week who has offered to fill me in (metaphorically speaking) on why ehtanol in mogas is a really bad thing....Not saying that he will be incorrect, just I don't understand why not at the moment. Frank Another 5 hours and i start filling gas cans...Non ethanol...for now..:) ________________________________ From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Jerry2DT@aol.com Sent: Thursday, September 28, 2006 2:05 PM Subject: AeroElectric-List: Re: Mogas versus 100LL (Mostly Off Topic) Excellent article on Ethanol in current Consumer Reports. A couple things for sure are that Ethanol has 30% less BTU's than Gasoline 125k btu/gal vs. 84.4), thereby translating to 32% less mileage per gal. Ethanol is cleaner, which I guess is why it is mandated in some parts. I track my car gas mileage very closely and get 8% less mpg when using a mix. The math doesn't come out quite right with the btu's, but it is a fact, at least for my car. It is alleged that Ethanol rots some seals, gaskets. My 1996 Honda motorcycle specifically disallows it's use. There is no way I'll ever use a mix of gas/ethanol in my aircraft. Superior also bans Ethanol btw, although encourages use of premium mogas for their XP360's... FWIW, .02, etc. Jerry Cochran From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> --> AeroElectric-List message posted by: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> Indeed yes are...but do you measure the RVP before you use it?...Even if the RVP is a little high you can ajust your flying to suit. As a bit of an aside I probably wouldn't store mogas for 6 months before using it. More of a question is wat if ethanol appears in the mix...i have an invite to phone Todd at Peterson for the low down on why not to use Ethanol...I'm not convinced on that one...at least not yet. More to come


    Message 18


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    Time: 03:10:42 PM PST US
    From: "A DeMarzo" <planepubs@ev1.net>
    Subject: Re: A Proud Announcement
    Well done! Congrats! On 09/28/2006 10:49:13 AM, europaxsa276@aol.com wrote: > On Wednesday, September 27, 2006 my son Brennan J. Skelly took his first > solo flight. The flight took place at 10:45 Central time at Grand Prairie > Municipal Airport located in Grand Prairie Texas USA. The sky was a > pristine blue and the winds were light and variable. > > After a written examination and a few test runs, Brennan's instructor released him for solo. Brennan flew the pattern and made 2 perfect landings and "one like his dad makes". (Whatever that is supposed to mean!!) > > Brennan is age 19. He currently attends a local college and in 2007 he will transfer to North Dakota University to attend the Federal Aviation Administration Air Traffic Controller program. He works part time at Grand Prairie Municipal Airport with the very important duty of fueling the general aviation fleet. He is also certified to "Hot Fuel" the emergency helicopters that are based at that location. In his off times he enjoys working in the shop with his father on the Europa XS project. > > Brennan represents the third generation of pilots for the Skelly family. Upon completion of his flight he notified his 90 year old Grandfather James E. Skelly, who proudly flew in the European theater of W.W.II and later became a military flight instructor. > > Way to go son! Your father is very proud. >


    Message 19


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    Time: 03:49:01 PM PST US
    From: "6440 Auto Parts" <sales@6440autoparts.com>
    Subject: Re: Mogas versus 100LL (Mostly Off Topic)
    Frank did you go to an AFS seminar ? If so was it worth it ? If not where did you get the info that their system will run 100% ethanol ? I have'nt found much real info on their website. Randy ----- Original Message ----- From: Hinde, Frank George (Corvallis) To: aeroelectric-list@matronics.com Sent: Thursday, September 28, 2006 4:48 PM Subject: RE: AeroElectric-List: Re: Mogas versus 100LL (Mostly Off Topic) When i spoke to Superior they stated Vapour lock as the issue with ethanol mix...But when i asked if they really meant vapour lock or simply boiling of fuel in the injector lines ...Which is not vapour lock I did not get an answer. Secondly with my Airflow Performance system it can run on 100% ethanol if you so desire. I have high regard for Superior, don't get me wrong but there are MANY OWTs out there that one is forced to question. ECI states lead being a lubricant for valve seats as Gospel for example...I don't buy it because, 1 it sounds ridiculous and 2 there is more and more evidence to the contrary. Now in order to preserve the warranty (if there really is one) ECI demand that you use 100LL duting break in...OK for sure i will only start feeding in mogas after 25 hours or so...Not worth the risk. Soo..if you have a properly designed fuel system (my pumps are in the wingroots) I'm having a hard time understanding the objection to ethanol mixes...Apart from the fact we're getting short changed (lower grade fuel)to support our totally excessive farm production of course...:) Now it maybe the injector line boiling is so bad it s difficult to get the engine to run smooth...Definatly a possibility. I will phone Todd Peterson next week who has offered to fill me in (metaphorically speaking) on why ehtanol in mogas is a really bad thing....Not saying that he will be incorrect, just I don't understand why not at the moment. Frank Another 5 hours and i start filling gas cans...Non ethanol...for now..:) ------------------------------------------------------------------------- ----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Jerry2DT@aol.com Sent: Thursday, September 28, 2006 2:05 PM To: aeroelectric-list@matronics.com Subject: AeroElectric-List: Re: Mogas versus 100LL (Mostly Off Topic) Excellent article on Ethanol in current Consumer Reports. A couple things for sure are that Ethanol has 30% less BTU's than Gasoline 125k btu/gal vs. 84.4), thereby translating to 32% less mileage per gal. Ethanol is cleaner, which I guess is why it is mandated in some parts. I track my car gas mileage very closely and get 8% less mpg when using a mix. The math doesn't come out quite right with the btu's, but it is a fact, at least for my car. It is alleged that Ethanol rots some seals, gaskets. My 1996 Honda motorcycle specifically disallows it's use. There is no way I'll ever use a mix of gas/ethanol in my aircraft. Superior also bans Ethanol btw, although encourages use of premium mogas for their XP360's... FWIW, .02, etc. Jerry Cochran From: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> --> AeroElectric-List message posted by: "Hinde, Frank George (Corvallis)" <frank.hinde@hp.com> Indeed yes are...but do you measure the RVP before you use it?...Even if the RVP is a little high you can ajust your flying to suit. As a bit of an aside I probably wouldn't store mogas for 6 months before using it. More of a question is wat if ethanol appears in the mix...i have an invite to phone Todd at Peterson for the low down on why not to use Ethanol...I'm not convinced on that one...at least not yet. More to come matronics.com/Navigator?AeroElectric-List


    Message 20


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    Time: 06:37:55 PM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Whelen Strobes Blowing Fuses
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 10:43 AM 9/28/2006 -0400, you wrote: >--> AeroElectric-List message posted by: "Peter Braswell" ><pbraswell@alterthought.com> > > >Hey Bob! Thanks for wanting the follow up! > >I went flying the other night with a 15amp fuse as per your recommendation. >Prior to blasting off, I cycled the strobes a few times with no problems. >When I got back down the strobes were still flashing so I think that got it! > >And can I say how GREAT it is to have a flying airplane!!!?? I flew until >the sun was just dipping below the horizon. The night was dead calm and my >home airport is a great little 3200' foot sod strip. All that (and the >flashing strobes) made for a very picturesque approach and landing!!! >Doesn't get much better than that! Okay, this experiment says that you're not suffering from a hard fault but more likely an average energy (perhaps punctuated with once-per-flash peak) draw that slowly weakens the fuse. It would be REALLY cool to get some current traces off your system. You're okay with leaving the 15A fuse in place and I wouldn't worry about up-sizing the wire. If you ever come through Wichita, I'd love to put hook some test equipment to your airplane. Bob . . .


    Message 21


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    Time: 06:53:56 PM PST US
    From: "Peter Braswell" <pbraswell@alterthought.com>
    Subject: Whelen Strobes Blowing Fuses
    --> AeroElectric-List message posted by: "Peter Braswell" <pbraswell@alterthought.com> Bob, Thanks! You got it! I'll make it a point to stop should I get out that far! Peter -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Thursday, September 28, 2006 9:34 PM Subject: RE: AeroElectric-List: Whelen Strobes Blowing Fuses --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" --> <nuckollsr@cox.net> At 10:43 AM 9/28/2006 -0400, you wrote: >--> AeroElectric-List message posted by: "Peter Braswell" ><pbraswell@alterthought.com> > > >Hey Bob! Thanks for wanting the follow up! > >I went flying the other night with a 15amp fuse as per your recommendation. >Prior to blasting off, I cycled the strobes a few times with no problems. >When I got back down the strobes were still flashing so I think that got it! > >And can I say how GREAT it is to have a flying airplane!!!?? I flew >until the sun was just dipping below the horizon. The night was dead >calm and my home airport is a great little 3200' foot sod strip. All >that (and the flashing strobes) made for a very picturesque approach and landing!!! >Doesn't get much better than that! Okay, this experiment says that you're not suffering from a hard fault but more likely an average energy (perhaps punctuated with once-per-flash peak) draw that slowly weakens the fuse. It would be REALLY cool to get some current traces off your system. You're okay with leaving the 15A fuse in place and I wouldn't worry about up-sizing the wire. If you ever come through Wichita, I'd love to put hook some test equipment to your airplane. Bob . . .


    Message 22


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    Time: 07:04:46 PM PST US
    From: "Dennis Johnson" <pinetownd@volcano.net>
    Subject: Grounding
    It's good that you're exercising the gray-matter on this topic . . . know that taking all EIS grounds to either forward or aft firewall grounds is an good move. Hi Bob, Thanks for the answer! By the way, I love the Metcal soldering iron you recommended. I'm soldering up high density 65 pin HD-Sub connectors today and need all the help I can get. Thanks, Dennis Johnson do not archive


    Message 23


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    Time: 08:55:44 PM PST US
    From: "bob noffs" <icubob@newnorth.net>
    Subject: battery cables
    hi all, i am starting the wiring of my plane with the battery cables. from what i can get from bobs book i should keep the pos. and. neg. cables from the battery together, especially thru the cabin area, until they get firewall forward. then terminate the neg. at the crankcase with a jumper cable from crankcase to the ground block on the firewall. have i got this right? thanks in advance. bob noffs


    Message 24


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    Time: 09:13:51 PM PST US
    From: "Robert L. Nuckolls, III" <nuckollsr@cox.net>
    Subject: Re: battery cables
    --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckollsr@cox.net> At 10:52 PM 9/28/2006 -0500, you wrote: >hi all, i am starting the wiring of my plane with the battery cables. from >what i can get from bobs book i should keep the pos. and. neg. cables from >the battery together, especially thru the cabin area, until they get >firewall forward. then terminate the neg. at the crankcase with a jumper >cable from crankcase to the ground block on the firewall. have i got this >right? thanks in advance. If you have a metal airplane, local grounding of the battery IS an option. See: http://aeroelectric.com/articles/Battery_Grounds/Battery_Grounds.html If you choose to bring battery (-) forward, then tie it off on the firewall ground block thru bolt. Take a jumper from the same bolt forward to the crankcase. This is illustrated in Z-15, View A of: http://aeroelectric.com/articles/Rev11/AppZ_R11J.pdf Bob . . .




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