AeroElectric-Archive.digest.vol-ky

March 19, 2012 - April 02, 2012



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________________________________________________________________________________
From: "John Cammarano" <jcappraiser(at)sbcglobal.net>
Subject: Re: Aviation crimp terminals.
Date: Mar 19, 2012
Thanks Bob - Great helpful info as usual. Johnny From: Robert L. Nuckolls, III Sent: Monday, March 19, 2012 7:14 AM Subject: RE: AeroElectric-List: Aviation crimp terminals. At 03:42 PM 3/18/2012, you wrote: Johnny, It's a very good idea to do that- however, there are times that it is not required. The shrink wrap (by which I think you mean heat shrink), properly applied, provides a great stress reliever to the wire/crimp joint. Generally I apply three layers of heat shrink- a long thin one first and then two successively thicker ones, where the last layer goes over the insulation of the crimp and then onto the two layers on the wire, so that there are graduated layers of material that absorb vibration and provide stress relief. I do this in areas where the wire does not immediately go into a bundle that will support it from vibration. Where you have a wire that can immediately be supported you do not need this stress relief. It's important to make a distinction here between what has been euphemistically called 'aviation' terminals . . . like the AMP Pre-Insulated Diamond Grip or PIDG terminal above and 'those other' terminals like . . . The PIDG terminal is a one-stop solution to wire termination that provides both gas-tight electrical connection between metals of terminal and wire PLUS mechanical support immediately adjacent to the point were the wire strands exit the crimped connection. This is described in the article at . . . http://aeroelectric.com/articles/terminal.pdf Those 'other' terminals can be applied with equal quality crimps but they are not fitted with the extra pieces of metal and plastic that provides support. This style of terminal is generally found in the few places on the airplane where FAT wires get bolted to typically larger, terminal studs. One methodology for using these terminals on the OBAM aircraft is illustrated here . . . http://aeroelectric.com/articles/AlumWire/AlumWire.html and here . . . http://aeroelectric.com/articles/big_term.pdf Interestingly enough, FAT wire strands are not so prone to failure due to flexing of at the crimp/solder joint. I've seen some fat wire terminal failures at where the terminal flag broke off between the stud and the connector barrel. The wires are often stiffer than the terminal that attaches them! So it's a good idea not to cantilever long runs of FAT wire off the stud on say alternator b-leads and starters. One can finish of the installation of such terminals by covering the barrel and wire junction with heat shrink . . . or even the heavier, double-walled stuff. In the grand scheme of things, mechanical benefits to the termination are minimal. But it DOES look nicer. The point to be made here is that adding any sort of mechanical support to a wire terminated with a PIDG style device is unnecessary. The 'aviation' terminals are the gold-standard for wire termination in all venues that demand the-best-we-know-how-to-do of which airplanes is a small segment. Adding shrink to a soldered or crimped FAT wire termination is more cosmetic than useful. In the earliest editions of the 'Connection I suggested that a builder could use solder- on terminals common to the electronics industry. Here the termination WILL indeed benefit from an addition of heat-shrink. But in the grand scheme of things, even the most frugal builder will find that the savings in labor and materials for solder+shrink on small wires is probably more than offset by buying the-best-we-know-how-do-to terminals and installing them with the appropriate tool. Go PIDG where you can for 22-10AWG wires. Then accomplish due consideration for support of FAT wires on engines where useful support is offered by the terminal PLUS some mechanical feature adjacent to the point where the terminal drops onto a stud. Using super-flex wire (like welding cable) on batteries is a prophylactic against vibration induced stresses on the battery's typically small attach bolts and/or lead connection tabs. Bob . . . ________________________________________________________________________________
Date: Mar 19, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna
At 02:58 PM 3/19/2012, you wrote: >cheers mike and bob > >Dose the L angle length have any affect on reception as it just says >convenient on the drawing. > >Mark That piece is a mounting bracket that fastens the antenna to the tip-rib. It's dimensions have no appreciable effect on performance as long as all other dimensions are not altered. Bob . . . ________________________________________________________________________________
Date: Mar 19, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna
At 02:58 PM 3/19/2012, you wrote: >cheers mike and bob > >Dose the L angle length have any affect on reception as it just says >convenient on the drawing. > >Mark > > >Beautiful 3 Bedroom 2 Bathroom villa to rent in Orlando, Florida ><http://www.obeo.com/Public/Viewer/Default.aspx?ID=321207>http://www.obeo.com/Public/Viewer/Default.aspx?ID=321207 >Check out our virtual tour >01582 529820 Emma and Mark Harris > > >---------- >From: wynaire(at)citlink.net >To: aeroelectric-list(at)matronics.com >Subject: Re: AeroElectric-List: Re: wingtip vor antenna >Date: Sun, 18 Mar 2012 15:44:35 -0600 > >Bob, >Thanks for the Sunday surprise (VOR antenna diagram). Looks like I >may be building "a spare VOR ant" for the Lancair, as well. What does the tip-rib look like? Keep in mind that the Bob Archer VOR wing tip VOR antenna was designed for RV's . . . aluminum wing with aluminum tip rib . . . and a Fiberglas tip cover. The antenna is a highly distorted, quarter-wave radiator with a gamma-match feed line attachment. The quarter-wave antenna needs to work against a substantial RF ground. When the antenna is up in the air, ground is provided by a suite of "radials". On an airplane, the 1/4 wave comm antenna is grounded against structure or the aircraft's skin. If the proposed installation is not onto an aluminum airplane, the antenna's performance versus that which has been demonstrated on RV's (and other metal airplanes) is degraded. Too much? Don't know without trying it. But if it's a 'spare', maybe performance isn't a big issue. Just be aware that it WILL be different . . . your in-flight observations (perhaps being able to quickly switch between antennas) would be VERY interesting. Bob . . . ________________________________________________________________________________
Date: Mar 19, 2012
From: jdabney(at)rice.edu
Subject: Re: wingtip vor antenna
Bob, Do you have dimensions for an Archer-style comm antenna for composite planes? Jim Quoting "Robert L. Nuckolls, III" : > At 02:58 PM 3/19/2012, you wrote: >> cheers mike and bob >> >> Dose the L angle length have any affect on reception as it just >> says convenient on the drawing. >> >> Mark >> >> >> Beautiful 3 Bedroom 2 Bathroom villa to rent in Orlando, Florida >> <http://www.obeo.com/Public/Viewer/Default.aspx?ID=321207>http://www.obeo.com/Public/Viewer/Default.aspx?ID=321207 >> Check out our virtual tour >> 01582 529820 Emma and Mark Harris >> >> >> >> ---------- >> From: wynaire(at)citlink.net >> To: aeroelectric-list(at)matronics.com >> Subject: Re: AeroElectric-List: Re: wingtip vor antenna >> Date: Sun, 18 Mar 2012 15:44:35 -0600 >> >> Bob, >> Thanks for the Sunday surprise (VOR antenna diagram). Looks like I >> may be building "a spare VOR ant" for the Lancair, as well. > > What does the tip-rib look like? Keep in mind that the > Bob Archer VOR wing tip VOR antenna was designed for > RV's . . . aluminum wing with aluminum tip rib . . . > and a Fiberglas tip cover. > > The antenna is a highly distorted, quarter-wave radiator > with a gamma-match feed line attachment. The quarter-wave > antenna needs to work against a substantial RF ground. When > the antenna is up in the air, ground is provided by a suite > of "radials". On an airplane, the 1/4 wave comm antenna is > grounded against structure or the aircraft's skin. > > If the proposed installation is not onto an aluminum airplane, > the antenna's performance versus that which has been demonstrated > on RV's (and other metal airplanes) is degraded. Too much? Don't > know without trying it. But if it's a 'spare', maybe performance > isn't a big issue. Just be aware that it WILL be different . . . > your in-flight observations (perhaps being able to quickly switch > between antennas) would be VERY interesting. > > > Bob . . . ________________________________________________________________________________
Date: Mar 19, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna
At 08:00 PM 3/19/2012, you wrote: > >Bob, > >Do you have dimensions for an Archer-style comm antenna for composite planes? > >Jim No. In fact, the dimensions for RV wing tip VOR antenna were published in Vans Airforce newsletter. But from the description I deduce that it's the same design as the VOR except trimmed for the higher frequency. It' wouldn't be hard to craft one. Of course, it's still primarily horizontal antenna but certainly would perform better than a rubber duck in the cockpit on a hand held. Just shorten the length values by 11% to get you into the Comm frequency range. Bob . . . ________________________________________________________________________________
Date: Mar 20, 2012
From: Sam Staton <pj260(at)bellsouth.net>
Subject: Archer-Style Antenna
Bob - It doesn't look like the Archer-type antenna diagram came through. All I can see is the emacs symbol, even on the html version. Is the diagram posted on your site anywhere? I would like to build one, but need to see the diagram. Thanks! Sam Staton ________________________________________________________________________________
Date: Mar 20, 2012
Subject: Re: white residue on solder
From: bob noffs <icubob(at)gmail.com>
the residue came off with carb cleaner, [like you soak a carb in] and lacquer thinner. between the two it came off clean. bob noffs On Sat, Mar 17, 2012 at 1:02 AM, David Lloyd wrote: > ** > ..use a little rubbing compound or similar and scrub with a toothbrush or > similar. The brass has to brightened anyway to do a good solder touch > up.... > D > > > ----- Original Message ----- > *From:* bob noffs > *To:* aeroelectric list > *Sent:* Friday, March 16, 2012 4:52 PM > *Subject:* AeroElectric-List: white residue on solder > > hi all, > i made a brass float for my fuel level indicator using solder. one area > soldered has a white residue [maybe from resin] after being submerged in av > gas 6 months. not all soldered areas have it. i could have easily used 2 > different solders. i want to get into a small area on the float and make a > repair. anyone know a solvent, liquid that would remove the chalky residue? > it is a very thin layer and no threat to my fuel system but i want to get a > clean area for a good bond. > thanks, bob noffs > > * > > href="http://www.matronics.com/Navigator?AeroElectric-List">http://www.matronics.com/Navigator?AeroElectric-List > href="http://forums.matronics.com">http://forums.matronics.com > href="http://www.matronics.com/contribution">http://www.matronics.com/c* > > * > > * > > ________________________________________________________________________________
Date: Mar 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Archer-Style Antenna
At 04:43 AM 3/20/2012, you wrote: > >Bob - > It doesn't look like the Archer-type antenna diagram came > through. All I can see is the emacs symbol, even on the html > version. Is the diagram posted on your site anywhere? I would like > to build one, but need to see the diagram. Thanks! Goto: http://www.matronics.com/forums/viewtopic.php?t=89235 Bob . . . ________________________________________________________________________________
Date: Mar 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna
At 08:00 PM 3/19/2012, you wrote: > >Bob, > >Do you have dimensions for an Archer-style comm antenna for composite planes? > >Jim It occurs to me that you might be asking about the antennas that go into the vertical fin. I've not seen any of those. Bob . . . ________________________________________________________________________________
Subject: Re: wingtip vor antenna
From: Mark Harris <harrismarkr(at)hotmail.com>
Date: Mar 20, 2012
Cheers Bob Looks like a job for the weekend Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 19 Mar 2012, at 22:18, "Robert L. Nuckolls, III" wrote: > > At 02:58 PM 3/19/2012, you wrote: >> cheers mike and bob >> >> Dose the L angle length have any affect on reception as it just says convenient on the drawing. >> >> Mark > > That piece is a mounting bracket that fastens > the antenna to the tip-rib. It's dimensions have > no appreciable effect on performance as long as > all other dimensions are not altered. > > > Bob . . . > > > > > ________________________________________________________________________________
Subject: ELT Antenna
Date: Mar 20, 2012
From: "Rasmussen, Robert CAPT USFF, N3 OTRC" <robert.rasmussen(at)navy.mil>
Greetings All, Two questions: 1. Any problem crafting my own ELT antenna for install in an RV8 tail fairing, per http://www.aeroelectric.com/articles/Antennas/DIY_Comm_Ant/DIY_Comm.html instructions? 2. What is EMACS! Thanks, Raz ________________________________________________________________________________
Date: Mar 20, 2012
From: Ed Holyoke <bicyclop(at)pacbell.net>
Subject: Re: ELT Antenna
Have to look at your ELT installation instructions. The ELT is TSOed and might require that you use their antenna. Ed Holyoke On 3/20/2012 2:35 PM, Rasmussen, Robert CAPT USFF, N3 OTRC wrote: > Greetings All, > Two questions: > 1. Any problem crafting my own ELT antenna for install in an RV8 tail fairing, per http://www.aeroelectric.com/articles/Antennas/DIY_Comm_Ant/DIY_Comm.html instructions? > > 2. What is EMACS! > > Thanks, > Raz ________________________________________________________________________________
Date: Mar 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna
At 02:18 PM 3/20/2012, you wrote: > >Cheers Bob > >Looks like a job for the weekend Do you have access to an antenna analyzer or at least an SWR meter? Bob . . . ________________________________________________________________________________
Date: Mar 20, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: ELT Antenna
At 04:35 PM 3/20/2012, you wrote: >Greetings All, >Two questions: >1. Any problem crafting my own ELT antenna for install in an RV8 >tail fairing, per >http://www.aeroelectric.com/articles/Antennas/DIY_Comm_Ant/DIY_Comm.html >instructions? Functionally, yes . . . as long as it's a VHF only ELT. If it's a dual band device, the antenna has special features to offer performance on both frequencies. As Ed mentioned, you might have some bureaucratic briar patches to negotiate too. >2. What is EMACS! It's a placeholder that my email client inserts for embedded figures. Your e-mail client may object to displaying the figure and displays the placeholder. You can get the 'complete' posting my going to the http://matronics.com/forums and viewing the thread there. The figures can be downloaded too and placed on your own computer as you see useful or necessary. It's a bit of a quandary . . . it's useful to illustrate a posting with embedded images so that they are displayed in place with the descriptive text . . . as opposed to making them attachments or linking to an uploaded image on the website. But some email clients don't handle my embedded images well. What e-mail client are you using? Bob . . . ________________________________________________________________________________
From: "John Cammarano" <jcappraiser(at)sbcglobal.net>
Subject: Transponder
Date: Mar 20, 2012
Can anyone tell me if there is such a thing as a "Portable transponder". I have a small antique airplane with no electrical system & would often like to have a transponder but I don't really want to add a small battery. I don't mind adding the small transponder type antenna. I am trying to find out if there is a transponder out there powered by it's own rechargeable batteries - like a handheld comm radio or a portable GPS. Any info here would be very much appreciated. Thanks. Johnny ________________________________________________________________________________
Subject: Re: Transponder
From: Stein Bruch <stein(at)steinair.com>
Date: Mar 20, 2012
I'm not familiar with such an animal....Though you may be able to rig someth ing up using one of the newer lightweight low power devices like a Trig. Cheers, Stein On Mar 20, 2012, at 10:51 PM, "John Cammarano" w rote: > Can anyone tell me if there is such a thing as a "Portable transponder". I have a small antique airplane with no electrical system & would often like t o have a transponder but I don't really want to add a small battery. I don't mind adding the small transponder type antenna. I am trying to find out if t here is a transponder out there powered by it's own rechargeable batteries - like a handheld comm radio or a portable GPS. Any info here would be very m uch appreciated. Thanks. Johnny > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= > ________________________________________________________________________________
Date: Mar 21, 2012
From: Doug Ilg <doug.ilg(at)verizon.net>
Subject: Re: Transponder
If you don't like or can't use the info you get here, try asking that quest ion on a ballooning forum.- I have seen things like that cobbled together for balloons (try to find a balloon with an electrical system! :-).- I t hink you're in a "roll your own" situation, here.- As I recall, they were just normal panel mount transponders and encoders with smallish 12V SLA ba tteries in makeshift boxes - no real magic.=0A=0A=0AI can't remember whethe r the ones I've seen were in hot air or gas balloons, so you might want to target both kinds in your search.=0A=0AGood luck!=0A=0A-=0ADoug Ilg=0AGru mman Tiger N74818, College Park-Airport (KCGS), Maryland=0AChallenger II LSS LW (N641LG-reserved)-- kit underway at Laurel Suburban (W18)=0A=0A -=0A=0A=0A=0A>________________________________=0A> From: John Cammarano < jcappraiser(at)sbcglobal.net>=0A>To: aeroelectric-list(at)matronics.com =0A>Sent: Tuesday, March 20, 2012 11:51 PM=0A>Subject: AeroElectric-List: Transponde r=0A> =0A>=0A>Can anyone tell me if there is such a thing as a =0A"Portable transponder". I have a small antique airplane with no electrical =0Asystem & would often like to have a transponder but I don't really want to =0Aadd a small battery. I don't mind adding the small transponder type antenna. I =0Aam trying to find out if there is a transponder out there powered by it 's own =0Arechargeable batteries - like a handheld comm radio or a portable GPS. Any info =0Ahere would be very much appreciated. Thanks. =0AJohnny=0A > ________________________________________________________________________________
From: <bakerocb(at)cox.net>
Subject: Transponder
Date: Mar 21, 2012
3/21/2012 Hello John, See this web site: http://www.kinetic.co.uk/last.php Note that a true portable transponder for use in the U. S may be a real tough problem to solve because of the TSO requirements. Also note the requirements of 14 CFR 91.413. The sailplane people work in this arena -- just google transponder for sailplanes. Here is one source: http://www.soaringsafety.org/prevention/Guide-to-transponders-in-sailplanes-2010B.pdf 'OC' Baker Says: "The best investment we can make is the time and effort to gather and understand knowledge." ============================================================== From: "John Cammarano" <jcappraiser(at)sbcglobal.net> Subject: AeroElectric-List: Transponder Can anyone tell me if there is such a thing as a "Portable transponder". I have a small antique airplane with no electrical system & would often like to have a transponder but I don't really want to add a small battery. I don't mind adding the small transponder type antenna. I am trying to find out if there is a transponder out there powered by it's own rechargeable batteries - like a handheld comm radio or a portable GPS. Any info here would be very much appreciated. Thanks. Johnny ________________________________________________________________________________
From: "John Cammarano" <jcappraiser(at)sbcglobal.net>
Subject: Re: Transponder
Date: Mar 21, 2012
Thanks Doug. Johnny From: Doug Ilg Sent: Wednesday, March 21, 2012 5:09 AM Subject: Re: AeroElectric-List: Transponder If you don't like or can't use the info you get here, try asking that question on a ballooning forum. I have seen things like that cobbled together for balloons (try to find a balloon with an electrical system! :-). I think you're in a "roll your own" situation, here. As I recall, they were just normal panel mount transponders and encoders with smallish 12V SLA batteries in makeshift boxes - no real magic. I can't remember whether the ones I've seen were in hot air or gas balloons, so you might want to target both kinds in your search. Good luck! Doug Ilg Grumman Tiger N74818, College Park Airport (KCGS), Maryland Challenger II LSS LW (N641LG reserved) - kit underway at Laurel Suburban (W18) ------------------------------------------------------------------------- ----- From: John Cammarano <jcappraiser(at)sbcglobal.net> To: aeroelectric-list(at)matronics.com Sent: Tuesday, March 20, 2012 11:51 PM Subject: AeroElectric-List: Transponder Can anyone tell me if there is such a thing as a "Portable transponder". I have a small antique airplane with no electrical system & would often like to have a transponder but I don't really want to add a small battery. I don't mind adding the small transponder type antenna. I am trying to find out if there is a transponder out there powered by it's own rechargeable batteries - like a handheld comm radio or a portable GPS. Any info here would be very much appreciated. Thanks. Johnny ________________________________________________________________________________
From: "John Cammarano" <jcappraiser(at)sbcglobal.net>
Subject: Re: Transponder
Date: Mar 21, 2012
Thanks!! - great info. Johnny -------------------------------------------------- From: <bakerocb(at)cox.net> Sent: Wednesday, March 21, 2012 5:20 AM Subject: AeroElectric-List: Transponder > > 3/21/2012 > > Hello John, See this web site: > > http://www.kinetic.co.uk/last.php > > Note that a true portable transponder for use in the U. S may be a real > tough problem to solve because of the TSO requirements. Also note the > requirements of 14 CFR 91.413. > > The sailplane people work in this arena -- just google transponder for > sailplanes. Here is one source: > > http://www.soaringsafety.org/prevention/Guide-to-transponders-in-sailplanes-2010B.pdf > > > 'OC' Baker Says: "The best investment we can make is the time and effort > to gather and understand knowledge." > > ============================================================== > > From: "John Cammarano" <jcappraiser(at)sbcglobal.net> > Subject: AeroElectric-List: Transponder > > Can anyone tell me if there is such a thing as a "Portable transponder". > I have a small antique airplane with no electrical system & would often > like to have a transponder but I don't really want to add a small > battery. I don't mind adding the small transponder type antenna. I am > trying to find out if there is a transponder out there powered by it's > own rechargeable batteries - like a handheld comm radio or a portable > GPS. Any info here would be very much appreciated. Thanks. Johnny > > > ________________________________________________________________________________
Subject: Re: Transponder
From: Robert Borger <rlborger(at)mac.com>
Date: Mar 21, 2012
Hi John, Look at Microair. I know they have packages specifically for sailplane operations. Probably Becker, Garrecht and Trig as well. Becker and Microair being the lightest. Unfortunately, none of these are inexpensive. But then, I don't know of any inexpensive transponder. Blue skies & tailwinds, Bob Borger Europa XS Tri, Rotax 914, Airmaster C/S Prop. Little Toot Sport Biplane, Lycoming Thunderbolt AEIO-320 EXP 3705 Lynchburg Dr. Corinth, TX 76208-5331 Cel: 817-992-1117 rlborger(at)mac.com On Mar 21, 2012, at 8:00 AM, John Cammarano wrote: Thanks!! - great info. Johnny -------------------------------------------------- From: <bakerocb(at)cox.net> Sent: Wednesday, March 21, 2012 5:20 AM Subject: AeroElectric-List: Transponder > > 3/21/2012 > > Hello John, See this web site: > > http://www.kinetic.co.uk/last.php > > Note that a true portable transponder for use in the U. S may be a real tough problem to solve because of the TSO requirements. Also note the requirements of 14 CFR 91.413. > > The sailplane people work in this arena -- just google transponder for sailplanes. Here is one source: > > http://www.soaringsafety.org/prevention/Guide-to-transponders-in-sailplanes-2010B.pdf > > > 'OC' Baker Says: "The best investment we can make is the time and effort to gather and understand knowledge." ________________________________________________________________________________
Subject: Re: AeroElectric-List Digest: 11 Msgs - 03/20/12
Date: Mar 21, 2012
From: "James Meade" <jnmeade(at)southslope.net>
Portable transponder http://www.lxavionics.co.uk/portables.htm ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 21, 2012
THE INSTRUCTIONS CALL FOR A 22"LENGTH AND THAT IS GOOD FOR THE OLD 121MhZ ELT. The new ETL operate close to 400 mHz therefore should have a length just over 7". I'm sure Bob can give us the practical length. Noel -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Rasmussen, Robert CAPT USFF, N3 OTRC Sent: March 20, 2012 7:05 PM Subject: AeroElectric-List: ELT Antenna Greetings All, Two questions: 1. Any problem crafting my own ELT antenna for install in an RV8 tail fairing, per http://www.aeroelectric.com/articles/Antennas/DIY_Comm_Ant/DIY_Comm.html instructions? 2. What is EMACS! Thanks, Raz ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 21, 2012
It sure would be... but for amateur aircraft you might be able to use your own antenna. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Ed Holyoke Sent: March 20, 2012 10:18 PM Subject: Re: AeroElectric-List: ELT Antenna Have to look at your ELT installation instructions. The ELT is TSOed and might require that you use their antenna. Ed Holyoke On 3/20/2012 2:35 PM, Rasmussen, Robert CAPT USFF, N3 OTRC wrote: Greetings All, Two questions: 1. Any problem crafting my own ELT antenna for install in an RV8 tail fairing, per http://www.aeroelectric.com/articles/Antennas/DIY_Comm_Ant/DIY_Comm.html instructions? 2. What is EMACS! Thanks, Raz ________________________________________________________________________________
Subject: Re: wingtip vor antenna
From: Mark Harris <harrismarkr(at)hotmail.com>
Date: Mar 21, 2012
Bob I can probably loan a swr meter Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 21 Mar 2012, at 01:50, "Robert L. Nuckolls, III" wrote: > > At 02:18 PM 3/20/2012, you wrote: >> >> Cheers Bob >> >> Looks like a job for the weekend > > Do you have access to an antenna analyzer or > at least an SWR meter? > > > Bob . . . > > > > > ________________________________________________________________________________
Date: Mar 21, 2012
From: Tim Andres <tim2542(at)sbcglobal.net>
Subject: Annunciator lights
Hey gang! I built an annunciator panel using these LED's: http://tinyurl.com/85r8duf Now that Im flying I find they are failing almost weekly. I need to replace them or fix the problem. They incorporate an integral resistor and are rated at 12V. I'm looking for a more durable replacement, maybe something that could be retrofitted into the existing lens as the led and resistor will slide out the back side. Any ideas welcome! Thanks, Tim ________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Annunciator lights
Date: Mar 21, 2012
I built an annunciator panel using these LED's: http://tinyurl.com/85r8duf Now that Im flying I find they are failing almost weekly. I need to replace them or fix the problem. You have LEDs rated for 3-12V and you are running them at 14+ volts. The current flow is too high with this higher voltage and this is most likely why they are failing. If you really like these indicators, you could put in series resistors, or put in lights with a higher voltage rating. Roger ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Re: wingtip vor antenna - SWR Meter
Date: Mar 21, 2012
Can this radio shack be used for aviation comm radios? http://www.radioshack.com/product/index.jsp?productId 36239 (at < $40, the price is sure right) IIRC, CB's are around 27 Mhz & airplane radios operate 118-136 Mhz. Is that a problem? -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Mark Harris Sent: Wednesday, March 21, 2012 12:11 Subject: Re: AeroElectric-List: Re: wingtip vor antenna Bob I can probably loan a swr meter Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 21 Mar 2012, at 01:50, "Robert L. Nuckolls, III" wrote: > > At 02:18 PM 3/20/2012, you wrote: >> >> Cheers Bob >> >> Looks like a job for the weekend > > Do you have access to an antenna analyzer or > at least an SWR meter? > > > Bob . . . > > > > > ________________________________________________________________________________
Date: Mar 21, 2012
Subject: Annunciator lights
From: rparigor(at)suffolk.lib.ny.us
I incorporated a number of Pep Boys LEDs in my panel. The reason I like them is they are slightly longer than a normal LED of that diameter. They are sold LEDs that can be used with 12 volts. The resistors they are using are too small, way too fragile, they didn't clean them before soldering, they did a very poor job soldering and the wire they use just doesn't solder that well. Net is I had several fail on the bench, some the solder joint failed, some the solder joint was high resistance and some the resistor broke. I still like the LEDs, so I just put my own resistor and wires on them and all is well. You can have a look at Hosfelt electronics for LEDs, or www.besthongkong.com if you want to buy a lot of stuff. You don't have to put the resistor inside your annunciator, it can go anywhere along the circuit. Doing the trick where you take a resistor with a leg to the left and a leg to the right, now you take a wire coming from the right, pass the resistor and solder to the left leg, then take a wire coming from the left, pass the resistor and connect it to the right and cover with a piece of heat shrink works very nice. I don't have any pics with clear shrink tubing, but here's a diode in series:http://www.europaowners.org/main.php?g2_itemId=82005&g2_imageViewsIndex=1 Here's a resistor in series: http://www.europaowners.org/main.php?g2_itemId=82008&g2_imageViewsIndex=1 Ron Parigoris ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: wingtip vor antenna - SWR Meter
Date: Mar 21, 2012
Yes, it is a problem the diodes in this meter are not nearly fast enough to break the RF (Radio Frequency) of VHF into digital segments needed to measure SWR. This unit is usable for frequencies 30 mHz and below. You may find a serviceable meter on eBay. If you buy a Bird Wattmeter make sure the element for 100-250 mHz comes with it. Noel -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Jeff Luckey Sent: March 21, 2012 8:04 PM Subject: AeroElectric-List: Re: wingtip vor antenna - SWR Meter --> Can this radio shack be used for aviation comm radios? http://www.radioshack.com/product/index.jsp?productId 36239 (at < $40, the price is sure right) IIRC, CB's are around 27 Mhz & airplane radios operate 118-136 Mhz. Is that a problem? -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Mark Harris Sent: Wednesday, March 21, 2012 12:11 Subject: Re: AeroElectric-List: Re: wingtip vor antenna Bob I can probably loan a swr meter Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 21 Mar 2012, at 01:50, "Robert L. Nuckolls, III" wrote: > > At 02:18 PM 3/20/2012, you wrote: >> >> Cheers Bob >> >> Looks like a job for the weekend > > Do you have access to an antenna analyzer or at least an SWR meter? > > > Bob . . . > > > > > ________________________________________________________________________________
Date: Mar 21, 2012
Subject: ELT Antenna
From: Kelly McMullen <kellym(at)aviating.com>
The minimum for use of ELTs is to demonstrate that the complete system meets the TSO. Good luck with doing that with a roll your own antenna of unknown impedance and SWR. ELTs and transponders are two items on OBAM aircraft that must comply with the TSO. Noel wrote: It sure would be... but for amateur aircraft you might be able to use your own antenna. Noel *From:* owner-aeroelectric-list-server(at)matronics.com [mailto: owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of *Ed Holyoke *Sent:* March 20, 2012 10:18 PM *To:* aeroelectric-list(at)matronics.com *Subject:* Re: AeroElectric-List: ELT Antenna Have to look at your ELT installation instructions. The ELT is TSOed and might require that you use their antenna. ________________________________________________________________________________
Date: Mar 21, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna - SWR Meter
At 05:42 PM 3/21/2012, you wrote: > >Yes, it is a problem the diodes in this meter are not nearly fast enough to >break the RF (Radio Frequency) of VHF into digital segments needed to >measure SWR. This unit is usable for frequencies 30 mHz and below. >You may find a serviceable meter on eBay. If you buy a Bird Wattmeter make >sure the element for 100-250 mHz comes with it. The Bird products are the gold standard for RF wattmeters. A few months ago we had some discussion on the List about the HF SWR meters common to CB radio frequencies and below. These are not suited to VHF as their sampled transmission line is too long with respect to a wavelength at the frequencies of interest for VHF. They tend to give 'good' readings to poor antennas. We also had some discussions about this device: Emacs! Which you can get off eBay for about $60 postage paid. http://tinyurl.com/7cl4bba I purchased one of these and found it a quite good value. Reasonably accurate for power readings down into the 100 milliwatt range. The one I have here on my bench is spoken for and will be out of here next week . . . but the folks offering it on eBay have plenty more. Be sure to get two N-Male/BNC-Female adapters. Emacs! http://tinyurl.com/6m7ujmw These are about $2.50 each postage paid. Bob . . . ________________________________________________________________________________
From: "Don" <dsvs(at)ca.rr.com>
Subject: Source for Bakelite - 1/32" thick
Date: Mar 21, 2012
Package is on the way via Fedex. Open from the bottom marked open this side. -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Sunday, March 18, 2012 8:23 AM Subject: RE: AeroElectric-List: Source for Bakelite - 1/32" thick At 11:09 PM 3/17/2012, you wrote: > >Bob, >I have one that has the wrong cap on it. I talked to Bob Archer and he told >me thet the cap belongs on one of his dipole ant rather than on the >monopole that it is installed on. He sent me a replacement cap that I have >not installed yet. I can ship the entire thing to you for the experiment. >You will also notice that the "Bakelite is different on each cap" Send me an >address via the email address that shows with my name. Interesting! You can send the stuff to me at P.O. Box 130, Medicine Lodge, KS 67104-0130 or if you need to go UPS, then 209 Curry Lane Bob . . . ________________________________________________________________________________
Date: Mar 21, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Annunciator lights
At 03:55 PM 3/21/2012, you wrote: > >Hey gang! >I built an annunciator panel using these LED's: >http://tinyurl.com/85r8duf > >Now that Im flying I find they are failing almost weekly. I need to >replace them or fix the problem. They incorporate an integral >resistor and are rated at 12V. I'm looking for a more durable >replacement, maybe something that could be retrofitted into the >existing lens as the led and resistor will slide out the back side. What colors are you needing? Can you send me one of these fixtures . . . or at least take some good pix of the disassembled hardware as supplied. LEDs are not generally very fragile. Are you sure it's the LED that's failing and not the resistor? Some years ago we had some discussion about LED fragility and life vs. intensity here on the List. I took issue with a few readers who cited 'not to exceed' ratings for LEDs lest they depart for the happy glowing ground. I took a 10mm LED rated at 30 mA and wired it to a wall-wart biased up at about 4x that rating. I plugged it into an outlet in my garage and left it. You could see rather well in a darkened garage from the emitted light. Over a year later, I took it off the wall still illuminated. I didn't measure it's light output to see if it degraded but it certainly didn't go into gross failure. For use in annunciators where the lights are OFF most of the time, it might be a good idea to over-drive the LEDs in the interest of sun-light viewable performance. There are some honk'n LEDs available. I bought some 10mm reds and greens from this guy for a courtroom, table-top demonstrator . . . http://tinyurl.com/7jlgymk Very adequate for getting one's attention in a well lit courtroom. This seller http://tinyurl.com/7n75xu2 has some killer whites rated at 1W. These might do what you want depending on the ability of your caps to set the color when illuminated with white led. This much power in an LED probably calls for some heat-sinking . . . but you may find that you can run them a lot cooler and still get the necessary light. Bob . . . ________________________________________________________________________________
Date: Mar 21, 2012
From: Tim Andres <tim2542(at)sbcglobal.net>
Subject: Re: Annunciator lights
On 3/21/2012 5:46 PM, Robert L. Nuckolls, III wrote: > At 03:55 PM 3/21/2012, you wrote: >> >> >> Hey gang! >> I built an annunciator panel using these LED's: >> http://tinyurl.com/85r8duf >> >> Now that Im flying I find they are failing almost weekly. I need to >> replace them or fix the problem. They incorporate an integral >> resistor and are rated at 12V. I'm looking for a more durable >> replacement, maybe something that could be retrofitted into the >> existing lens as the led and resistor will slide out the back side. > > What colors are you needing? Can you send me one > of these fixtures . . . or at least take some good > pix of the disassembled hardware as supplied. Thanks Bob! I'll have to check if its the resistors that failed next time I get to the hangar but I noticed some of the on-line LED/resistor calculators call for a 1/2 w resistor and the ones installed in the fixtures look like 1/8w. I'll report back but have already bought new LEDs to fix them with and in fact found some blinking ones to boot that I'll use on my OP light. Thanks, Tim ________________________________________________________________________________
Subject: Stobes
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Mar 22, 2012
Here's more work for Bob to do in his "free" time. I have seen many questions on how to quiet strobes and would like to make the following observation: Having a central strobe power pack and running long wires to the wingtips (or to the rim of your flying saucer) is a recipe for RFI/EMI. A much more sensible design is to have the capacitors and trigger coil, located at the strobe tube. Strobe synchronization is simple to achieve. Noise would be gone. Whelen actually makes remote power packs, but at a price that is affordable only to Wall Street hedge fund managers. So a DIY version of a lighter weight "distributed" replacement for the standard Whelen strobe power pack would be a good solution to noise. Estimated weight savings 2 pounds. Not trivial. I have designed LED strobes in this fashion. Only position-light power wiring to the wingtip is required. This design merely pulses the synchronization to fire the strobes. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369131#369131 ________________________________________________________________________________
Date: Mar 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Annunciator lights
>Thanks Bob! I'll have to check if its the resistors that failed next >time I get to the hangar but I noticed some of the on-line >LED/resistor calculators call for a 1/2 w resistor and the ones >installed in the fixtures look like 1/8w. I'll report back but have >already bought new LEDs to fix them with and in fact found some >blinking ones to boot that I'll use on my OP light. One caveat on blinking LEDs . . . they're not very bright. When you're designing annunciators for airplanes, your dynamic range for ambient lighting is huge . . . especially for a bubble canopy airplane. I've used blinking LEDs in SERIES with high intensity devices with some success. But the most elegant approach for attention getting is to have a dedicated hardware flasher for the LED. It can be pretty simple: Emacs! This little flasher board made with surface mount components can be as small as .4" on a side, maybe even smaller. If you find that you need to over-drive an LED to meet your illumination design goals (e.g. say 50mA from a 14v source) the series resistor would be something on the order of 10/.05 or 200 ohms. 10 Volts dropped at 50 mA is 500 milliwatts . . . so using a 1W resistor would not be a bad idea for keeping surface temperatures down. If you've had failures of the COTS components then it doesn't much matter whether it was due to resistor or lamp failure . . . the events demand evaluation and modification of the design to achieve a useful level of confidence. Bob . . . ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 22, 2012
In that case if even on an OBAM aircraft the ELT and transponder must be installed or signed off by a certified AME (Canada) or A&P (U.S.) Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: March 21, 2012 8:26 PM Subject: RE: AeroElectric-List: ELT Antenna The minimum for use of ELTs is to demonstrate that the complete system meets the TSO. Good luck with doing that with a roll your own antenna of unknown impedance and SWR. ELTs and transponders are two items on OBAM aircraft that must comply with the TSO. Noel wrote: It sure would be... but for amateur aircraft you might be able to use your own antenna. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Ed Holyoke Sent: March 20, 2012 10:18 PM Subject: Re: AeroElectric-List: ELT Antenna Have to look at your ELT installation instructions. The ELT is TSOed and might require that you use their antenna. ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: wingtip vor antenna - SWR Meter
Date: Mar 22, 2012
Reading the page on this meter I assume it is not a good meter for use on RF below 100mHz. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: March 21, 2012 9:38 PM Subject: RE: AeroElectric-List: Re: wingtip vor antenna - SWR Meter At 05:42 PM 3/21/2012, you wrote: Yes, it is a problem the diodes in this meter are not nearly fast enough to break the RF (Radio Frequency) of VHF into digital segments needed to measure SWR. This unit is usable for frequencies 30 mHz and below. You may find a serviceable meter on eBay. If you buy a Bird Wattmeter make sure the element for 100-250 mHz comes with it. The Bird products are the gold standard for RF wattmeters. A few months ago we had some discussion on the List about the HF SWR meters common to CB radio frequencies and below. These are not suited to VHF as their sampled transmission line is too long with respect to a wavelength at the frequencies of interest for VHF. They tend to give 'good' readings to poor antennas. We also had some discussions about this device: Emacs! Which you can get off eBay for about $60 postage paid. http://tinyurl.com/7cl4bba I purchased one of these and found it a quite good value. Reasonably accurate for power readings down into the 100 milliwatt range. The one I have here on my bench is spoken for and will be out of here next week . . . but the folks offering it on eBay have plenty more. Be sure to get two N-Male/BNC-Female adapters. Emacs! http://tinyurl.com/6m7ujmw These are about $2.50 each postage paid. Bob . . . ________________________________________________________________________________
Date: Mar 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Stobes
At 08:18 AM 3/22/2012, you wrote: > >Here's more work for Bob to do in his "free" time. > >I have seen many questions on how to quiet strobes and would like to >make the following observation: > >Having a central strobe power pack and running long wires to the >wingtips (or to the rim of your flying saucer) is a recipe for >RFI/EMI. A much more sensible design is to have the capacitors and >trigger coil, located at the strobe tube. Strobe synchronization is >simple to achieve. Noise would be gone. As you've noted, there are several designs qualified for TC aircraft where the power conditioning is adjacent to the strobe tube. But I would offer that centralized supplies are also qualified, i.e. have passed DO-160 conducted and radiated emissions. So if installed with attention to good practice for treatment of shields, they should present no greater noise problem in an OBAM aircraft than they do in a TC aircraft. >Whelen actually makes remote power packs, but at a price that is >affordable only to Wall Street hedge fund managers. So a DIY version >of a lighter weight "distributed" replacement for the standard >Whelen strobe power pack would be a good solution to noise. >Estimated weight savings 2 pounds. Not trivial. Those are slick . . . but they're a relatively low volume product in comparison with the central supply configuration and they take up more room in what might be a more crowded space. Hence the higher cost that is not well tolerated in the SE propeller driven market. All the strobes on turbine aircraft have local power supplies but as you've noted, these are breathtakingly expensive. >I have designed LED strobes in this fashion. Only position-light >power wiring to the wingtip is required. This design merely pulses >the synchronization to fire the strobes. What kind of voltages/currents and duty cycles are involved? I've seen some LED anti-collision protects offered to HBC while I was still there but folks who showed them to me were unable or reluctant to discuss design details. What's the architecture for wiring up large arrays of LED's. The tail strobe I saw had about 36 leds in it. The guy thought it was 4 strings of 9 each. At 4 volts per led in an overdriven pulse mode, one comes to believe that a pulsed, 36 volt constant current supply is used. What approach has been most attractive in your experience? EMC issues for these supplies is a bit simpler. There's little probability of 'output noise' due to flashing and the operating frequency of the switchmode power supply is generally much higher . . . hence easier to filter . . . assuming the designer recognizes the need for a filter. We discovered this lower level design goal in the Luxeon power supplies that folks have been using in their wingtips. I've sold perhaps 50 filtered supplies over the past 4-5 years and perhaps half that number of filter boards for folks who already had supply modules. Bob . . . ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Annunciator lights
Date: Mar 22, 2012
Bob: The specs say 240Kmcd@300m=8BA . What exactly is a Kmcd? I have some ideas but none seems to fit unless this lamp will blister paint at ten feet.. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: March 21, 2012 10:17 PM Subject: Re: AeroElectric-List: Annunciator lights At 03:55 PM 3/21/2012, you wrote: Hey gang! I built an annunciator panel using these LED's: http://tinyurl.com/85r8duf Now that Im flying I find they are failing almost weekly. I need to replace them or fix the problem. They incorporate an integral resistor and are rated at 12V. I'm looking for a more durable replacement, maybe something that could be retrofitted into the existing lens as the led and resistor will slide out the back side. What colors are you needing? Can you send me one of these fixtures . . . or at least take some good pix of the disassembled hardware as supplied. LEDs are not generally very fragile. Are you sure it's the LED that's failing and not the resistor? Some years ago we had some discussion about LED fragility and life vs. intensity here on the List. I took issue with a few readers who cited 'not to exceed' ratings for LEDs lest they depart for the happy glowing ground. I took a 10mm LED rated at 30 mA and wired it to a wall-wart biased up at about 4x that rating. I plugged it into an outlet in my garage and left it. You could see rather well in a darkened garage from the emitted light. Over a year later, I took it off the wall still illuminated. I didn't measure it's light output to see if it degraded but it certainly didn't go into gross failure. For use in annunciators where the lights are OFF most of the time, it might be a good idea to over-drive the LEDs in the interest of sun-light viewable performance. There are some honk'n LEDs available. I bought some 10mm reds and greens from this guy for a courtroom, table-top demonstrator . . . http://tinyurl.com/7jlgymk Very adequate for getting one's attention in a well lit courtroom. This seller http://tinyurl.com/7n75xu2 has some killer whites rated at 1W. These might do what you want depending on the ability of your caps to set the color when illuminated with white led. This much power in an LED probably calls for some heat-sinking . . . but you may find that you can run them a lot cooler and still get the necessary light. Bob . . . ________________________________________________________________________________
Date: Mar 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Annunciator lights
At 02:12 PM 3/22/2012, you wrote: >Bob: > > >The specs say 240Kmcd@300m=8BA .=C2 What exactly >is a Kmcd?=C2 I have some ideas but none seems to >fit unless this lamp will blister paint at ten feet.. > > It's a bit of silliness . . . an mCd is a milli-candella. Or 1/1000th of one candella http://en.wikipedia.org/wiki/Candela 240,000 mCandelas reduces down to 240 Candelas, the "K" and "m" wipe each other out. Bob . . . ________________________________________________________________________________
Date: Mar 22, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: wingtip vor antenna - SWR Meter
At 01:52 PM 3/22/2012, you wrote: >Reading the page on this meter I assume it is not a good meter for >use on RF below 100mHz. It's accuracy will degrade as you depart the manufacturer's specified range of performance. If you buy a 'slug' for a Bird wattmeter Emacs! It is characterized for a power level and a range of frequencies for which it will meet the manufacturer's specs for accuracy. The 'Red Dot' SWR meter is simply a power meter with a 'fixed slug'. Bob . . . ________________________________________________________________________________
Date: Mar 22, 2012
From: Kelly McMullen <kellym(at)aviating.com>
Subject: Re: ELT Antenna
Who installs it has nothing to do whether it complies. It simply must be installed in compliance with the manufacturer's instructions, which ensure TSO compliance. In theory the DAR inspecting the aircraft should check that, but are not likely to look too closely. The person doing the condition inspection annually must also ensure compliance with the test requirements in Part 91. On 3/22/2012 11:09 AM, Noel Loveys wrote: > > In that case if even on an OBAM aircraft the ELT and transponder must > be installed or signed off by a certified AME (Canada) or A&P (U.S.) > > Noel > > *From:*owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of > *Kelly McMullen > *Sent:* March 21, 2012 8:26 PM > *To:* aeroelectric-list(at)matronics.com > *Subject:* RE: AeroElectric-List: ELT Antenna > > The minimum for use of ELTs is to demonstrate that the complete system > meets the TSO. Good luck with doing that with a roll your own antenna > of unknown impedance and SWR. ELTs and transponders are two items on > OBAM aircraft that must comply with the TSO. > > Noel wrote: > > It sure would be... but for amateur aircraft you might be able to use > your own antenna. > > Noel > > *From:*owner-aeroelectric-list-server(at)matronics.com > > [mailto:owner-aeroelectric-list-server(at)matronics.com > ] *On Behalf Of > *Ed Holyoke > *Sent:* March 20, 2012 10:18 PM > *To:* aeroelectric-list(at)matronics.com > > *Subject:* Re: AeroElectric-List: ELT Antenna > > Have to look at your ELT installation instructions. The ELT is TSOed > and might require that you use their antenna. > > * * > * * > ** > ** > ** > ** > ** > *http://www.matronics.com/Navigator?AeroElectric-List* > ** > ** > *http://forums.matronics.com* > ** > ** > ** > *http://www.matronics.com/contribution* > ** > * * > * > > > * ________________________________________________________________________________
Subject: Re: ELT Antenna
From: Tim Andres <tim2542(at)sbcglobal.net>
Date: Mar 22, 2012
I just had mine inspected by the FAA for A/W cert. and the issue never came u p at all and I do have a non TSO 'd antenna on the transponder. FWIW, I thin k that's about the norm . I know of several others with the same experience. Tim Sent from my iPad On Mar 22, 2012, at 11:09 AM, "Noel Loveys" wrote: > In that case if even on an OBAM aircraft the ELT and transponder must be i nstalled or signed off by a certified AME (Canada) or A&P (U.S.) > > Noel > > From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelect ric-list-server(at)matronics.com] On Behalf Of Kelly McMullen > Sent: March 21, 2012 8:26 PM > To: aeroelectric-list(at)matronics.com > Subject: RE: AeroElectric-List: ELT Antenna > > The minimum for use of ELTs is to demonstrate that the complete system mee ts the TSO. Good luck with doing that with a roll your own antenna of unknow n impedance and SWR. ELTs and transponders are two items on OBAM aircraft th at must comply with the TSO. > > Noel wrote: > It sure would be... but for amateur aircraft you might be able to use your own antenna. > > Noel > > From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelect ric-list-server(at)matronics.com] On Behalf Of Ed Holyoke > Sent: March 20, 2012 10:18 PM > To: aeroelectric-list(at)matronics.com > Subject: Re: AeroElectric-List: ELT Antenna > > Have to look at your ELT installation instructions. The ELT is TSOed and m ight require that you use their antenna. > > > http://www.matronics.com/Navigator?AeroElectric-List > http://forums.matronics.com > http://www.matronics.com/contribution > > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= > ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 22, 2012
In this country any appliance on a certified aircraft with certain exceptions has to be installed by or checked by a certified AME ( aircraft maintenance engineer ) and the installation has to be documented in the airframe log book and noted if there is a separate log book for the appliance. One of the things I do not like about the new ELT is that aircraft cannot borrow another ELT while one is out having scheduled service done. In the past the AMO I worked for had a "loaner" ELT that we would put in aircraft so they wouldn't have to fly without one... Which is legal for up to 90 days. In fact even a licensed AME is not allowed to change the batteries on an ELT it has to be done by an approved Avionics tech or an approved avionics shop. Amateur built aircraft are another quintal of fish... They don't even have to carry an ELT. Mind I don't know anyone who is stupid enough to fly this land without one. Noel -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: March 22, 2012 9:06 PM Subject: Re: AeroElectric-List: ELT Antenna --> Who installs it has nothing to do whether it complies. It simply must be installed in compliance with the manufacturer's instructions, which ensure TSO compliance. In theory the DAR inspecting the aircraft should check that, but are not likely to look too closely. The person doing the condition inspection annually must also ensure compliance with the test requirements in Part 91. On 3/22/2012 11:09 AM, Noel Loveys wrote: > > In that case if even on an OBAM aircraft the ELT and transponder must > be installed or signed off by a certified AME (Canada) or A&P (U.S.) > > Noel > > *From:*owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] *On Behalf Of > *Kelly McMullen > *Sent:* March 21, 2012 8:26 PM > *To:* aeroelectric-list(at)matronics.com > *Subject:* RE: AeroElectric-List: ELT Antenna > > The minimum for use of ELTs is to demonstrate that the complete system > meets the TSO. Good luck with doing that with a roll your own antenna > of unknown impedance and SWR. ELTs and transponders are two items on > OBAM aircraft that must comply with the TSO. > > Noel wrote: > > It sure would be... but for amateur aircraft you might be able to use > your own antenna. > > Noel > > *From:*owner-aeroelectric-list-server(at)matronics.com > > [mailto:owner-aeroelectric-list-server(at)matronics.com > ] *On Behalf Of > *Ed Holyoke > *Sent:* March 20, 2012 10:18 PM > *To:* aeroelectric-list(at)matronics.com > > *Subject:* Re: AeroElectric-List: ELT Antenna > > Have to look at your ELT installation instructions. The ELT is TSOed > and might require that you use their antenna. > > * * > * * > ** > ** > ** > ** > ** > *http://www.matronics.com/Navigator?AeroElectric-List* > ** > ** > *http://forums.matronics.com* > ** > ** > ** > *http://www.matronics.com/contribution* > ** > * * > * > > > * ________________________________________________________________________________
From: <bakerocb(at)cox.net>
Subject: Fw: Portable Transponder
Date: Mar 22, 2012
3/2/2012 Hello John Cammarano, I hope that this helps solve your problem. 'OC' Baker ================================================================= From: "John Delafield" <john.delafield(at)lxavionics.co.uk> Sent: Thursday, March 22, 2012 4:15 PM Subject: RE: Portable Transponder > Dear Sir, > > We assemble the transponder box using a certified TT 21 or 22 which has > FAA > approval so no worries there. The entire box is not approved by anyone > but > as it is portable I do not think it necessary anyway. > > The altitude encoder is built in to the transponder and it meets the new > 25ft spacing requirement. > > I am pretty sure for your application that you would not need the very > expensive hand made leather case that we normally provide and not having > this would reduce the price to you by about $200. > > Lead time for delivery would be a few weeks. > > I very much hope that we can help you, > > All the best, > > John Delafield > LX avionics Ltd > 07850 950349/01865 374125 > www.lxavionics.co.uk > Company Number 4417407 Registered in England and Wales > VAT GB 793 1777 86 > Registered address (NOT FOR BUSINESS): 30 St Giles, Oxford > ====================================================== From: bakerocb(at)cox.net [mailto:bakerocb(at)cox.net] > Sent: 22 March 2012 15:42 > To: johnd(at)lxavionics.co.uk > Subject: Portable Transponder > > 3/22/2012 > > Hello John, We are seeking a portable airtraffic radar transponder for use > in a small homebuilt (no electrical power) fixed wing airplane in the US. > Your products seen here: > > http://www.lxavionics.co.uk/portables.htm > > appear to offer a solution. > > I have two questions: > > 1) How is the information normally provided to a transponder by an > altitude > encoder for automatic altitude information transmission by the transponder > provided for in your products? > > 2) Are you aware of any regulatory reason (TSO or inspection requirements) > that would make your products not be acceptable for use in the United > States? > > Thanks for your help, > > 'OC' Baker Says: "The best investment we can make is the time and effort > to > gather and understand knowledge." > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 22, 2012
Subject: Re: ELT Antenna
Good Evening Noel, What country are you discussing? In the USA, every airline pilot regularly flies without an ELT. Personally, I would be happy to do so if it were not an FAA requirement. I do not feel one whit more secure since we were forced to install the ELT. There are a lot of ways to let folks know when and if you need assistance. I think each pilot should be able to make that decision himself or herself. Happy Skies, Old Bob In a message dated 3/22/2012 8:36:50 P.M. Central Daylight Time, noelloveys(at)yahoo.ca writes: --> AeroElectric-List message posted by: "Noel Loveys" In this country any appliance on a certified aircraft with certain exceptions has to be installed by or checked by a certified AME ( aircraft maintenance engineer ) and the installation has to be documented in the airframe log book and noted if there is a separate log book for the appliance. One of the things I do not like about the new ELT is that aircraft cannot borrow another ELT while one is out having scheduled service done. In the past the AMO I worked for had a "loaner" ELT that we would put in aircraft so they wouldn't have to fly without one... Which is legal for up to 90 days. In fact even a licensed AME is not allowed to change the batteries on an ELT it has to be done by an approved Avionics tech or an approved avionics shop. Amateur built aircraft are another quintal of fish... They don't even have to carry an ELT. Mind I don't know anyone who is stupid enough to fly this land without one. Noel ________________________________________________________________________________
From: "The Kuffels" <kuffel(at)cyberport.net>
Subject: Re: ELT Antenna
Date: Mar 22, 2012
Old Bob says: << Noel, .. What country are you discussing? >> His email address is Canada. His description fits what little I know of Canada's regulatory environment. << I do not feel one whit more secure since we were forced to install the ELT. >> This sentiment conflicts with my direct, personal experience. In Alaska in the 1970s when ELTs were first forced upon us, the false activation rate (especially in very cold weather) and the failure to activate rate (mostly due to poor antenna placement) was depressing. Still ELTs managed to save lives, including mine. The newer GPS augmented 406 MHz system is much more effective, quickly providing a location measured in meters. << There are a lot of ways to let folks know when and if you need assistance. >> Disagree. My Alaska crash occurred about 150 miles from any human habitation. My Idaho mountain crash was over in 15 sec. In the meantime, I was a little busy to let anyone know anything. Although I was flying with two other aircraft, they were unable to get our accurate location to Search & Rescue. Our cell phone got through to 911 long enough to let them know there were survivors but not long enough to provide our accurate location. Our 121.5 MHz ELT gave them a location 5 miles in error. But when they got in the neighborhood the ELT did help a little in narrowing our location. The moral, I want as many ways as possible to ask for assistance and help Search & Rescue determine our location. << I think each pilot should be able to make that decision himself or herself. >> Of course, this is a political statement not an aviation safety statement of fact. But given human nature, mandates are not always bad. Sort of like forced automobile liability insurance. Tom Kuffel ________________________________________________________________________________
Subject: Re: Stobes
From: "stearman456" <warbirds(at)shaw.ca>
Date: Mar 23, 2012
What is the advantage to having local power supplies for your strobe lights vs a single, central,power supply - or vice versa? The two strobe systems I'm considering are identical (lights, output) apart from three power supplies vs one. Dan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369203#369203 ________________________________________________________________________________
From: <bakerocb(at)cox.net>
Subject: ELT Antenna
Date: Mar 23, 2012
3/23/2012 Hello Noel Loveys, Thank you for your inputs on this subject, but in the interest of stamping out hearsay, gossip, and rumors regarding experimental amateur built aircraft I'd like to point out that some of your comments are just not applicable in the USA. The following statements that you wrote are not correct in the USA: 1) "In that case if even on an OBAM aircraft the ELT and transponder must be installed or signed off by a certified AME (Canada) or A&P (U.S.)" 2) "One of the things I do not like about the new ELT is that aircraft cannot borrow another ELT while one is out having scheduled service done." 3) "...so they wouldn't have to fly without one... Which is legal for up to 90 days." Note that the regulatory requirements for having an ELT in a US registered civil aircraft operating in the US, and the circumstances permitted for flying without an ELT installed, are contained in 14 CFR 91.207. That section is too long and complicated to be copied, or even extracted in this posting. It may be accessed here: http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=e13e8f64d66f124a79dbd562cbe93f0b&rgn=div8&view=text&node=14:2.0.1.3.10.3.7.4&idno=14 4) "In fact even a licensed AME is not allowed to change the batteries on an ELT it has to be done by an approved Avionics tech or an approved avionics shop." 5) "Amateur built aircraft are another quintal of fish... They don't even have to carry an ELT." They do in the USA in accordance with 14 CFR 91.207. Thanks for your help in posting accuracy. 'OC' Baker Says: "The best investment we can make is the time and effort to gather and understand knowledge." ============================================================= From: "Noel Loveys" <noelloveys(at)yahoo.ca> Subject: RE: AeroElectric-List: ELT Antenna In that case if even on an OBAM aircraft the ELT and transponder must be installed or signed off by a certified AME (Canada) or A&P (U.S.) Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: March 21, 2012 8:26 PM Subject: RE: AeroElectric-List: ELT Antenna The minimum for use of ELTs is to demonstrate that the complete system meets the TSO. Good luck with doing that with a roll your own antenna of unknown impedance and SWR. ELTs and transponders are two items on OBAM aircraft that must comply with the TSO. Noel wrote: It sure would be... but for amateur aircraft you might be able to use your own antenna. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Ed Holyoke Sent: March 20, 2012 10:18 PM Subject: Re: AeroElectric-List: ELT Antenna Have to look at your ELT installation instructions. The ELT is TSOed and might require that you use their antenna. ========================================================= From: "Noel Loveys" <noelloveys(at)yahoo.ca> Subject: RE: AeroElectric-List: ELT Antenna In this country any appliance on a certified aircraft with certain exceptions has to be installed by or checked by a certified AME ( aircraft maintenance engineer ) and the installation has to be documented in the airframe log book and noted if there is a separate log book for the appliance. One of the things I do not like about the new ELT is that aircraft cannot borrow another ELT while one is out having scheduled service done. In the past the AMO I worked for had a "loaner" ELT that we would put in aircraft so they wouldn't have to fly without one... Which is legal for up to 90 days. In fact even a licensed AME is not allowed to change the batteries on an ELT it has to be done by an approved Avionics tech or an approved avionics shop. Amateur built aircraft are another quintal of fish... They don't even have to carry an ELT. Mind I don't know anyone who is stupid enough to fly this land without one. Noel ________________________________________________________________________________
Subject: Re: Jabiru 3300 Over Voltage
From: "user9253" <fran4sew(at)banyanol.com>
Date: Mar 23, 2012
Rich, Did you ever solve the high voltage problem? Did you try adding a robust ground lead from regulator case to ship's single point ground as Bob Nuckolls suggested? Or was the regulator bad? I am curious to know the answer. Joe -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369217#369217 ________________________________________________________________________________
Date: Mar 23, 2012
Subject: Re: Stobes
From: Jared Yates <email(at)jaredyates.com>
The remote units are likely going to be a heavier installation, and they will require some sort of mechanism for synchronization if there is to be any. On Fri, Mar 23, 2012 at 8:05 AM, stearman456 wrote: > > What is the advantage to having local power supplies for your strobe > lights vs a single, central,power supply - or vice versa? The two strobe > systems I'm considering are identical (lights, output) apart from three > power supplies vs one. > > Dan > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=369203#369203 > > ________________________________________________________________________________
From: BobsV35B(at)aol.com
Date: Mar 23, 2012
Subject: Re: ELT Antenna
Good Morning Tom, I not only know very little about Canada, but also do not know much about figuring out from where a message is sent. I carefully worded my answer to make it clear that I did not know. Glad that it worked for you, but we could make similar statements about the advisability of having two engines and/or two pilots. I do NOT feel that regulations should force me to do things which I do not wish to do. That is political! I fly almost entirely within the Contiguous Forty Eight. Long before the ELT was forced upon us, I made a practice of carrying a portable radio with which I could ask for help if needed. (An early Bayside was my choice at the time.) I continue to carry a portable radio and I always carry IFR charts so I can be sure of getting on a frequency that is being heavily monitored in the area over which I am flying. Since 911, we are required to monitor guard if possible, but that has not always been so. The ELT has a terrible record. An accurate flight plan posted with a friend or the FAA has shown to have much a better success rate. I think my way is better, but it should be my choice! I would suggest carrying a nice new PLB. (I actually carry one in my flight bag, but that is beside the point.) The big thing is that it should be my decision, not the decision of a bureaucrat in Washington and that IS Political! The airliners do not carry an ELT. Why should I? Happy Skies, Old Bob In a message dated 3/22/2012 11:48:40 P.M. Central Daylight Time, kuffel(at)cyberport.net writes: Old Bob says: << Noel, .. What country are you discussing? >> His email address is Canada. His description fits what little I know of Canada's regulatory environment. << I do not feel one whit more secure since we were forced to install the ELT. >> This sentiment conflicts with my direct, personal experience. In Alaska in the 1970s when ELTs were first forced upon us, the false activation rate (especially in very cold weather) and the failure to activate rate (mostly due to poor antenna placement) was depressing. Still ELTs managed to save lives, including mine. The newer GPS augmented 406 MHz system is much more effective, quickly providing a location measured in meters. << There are a lot of ways to let folks know when and if you need assistance. >> Disagree. My Alaska crash occurred about 150 miles from any human habitation. My Idaho mountain crash was over in 15 sec. In the meantime, I was a little busy to let anyone know anything. Although I was flying with two other aircraft, they were unable to get our accurate location to Search & Rescue. Our cell phone got through to 911 long enough to let them know there were survivors but not long enough to provide our accurate location. Our 121.5 MHz ELT gave them a location 5 miles in error. But when they got in the neighborhood the ELT did help a little in narrowing our location. The moral, I want as many ways as possible to ask for assistance and help Search & Rescue determine our location. << I think each pilot should be able to make that decision himself or herself. >> Of course, this is a political statement not an aviation safety statement of fact. But given human nature, mandates are not always bad. Sort of like forced automobile liability insurance. Tom Kuffel ________________________________________________________________________________
Date: Mar 23, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Expanded horizons for the List?
From: rayj <raymondj(at)frontiernet.net> Subject: Marketing suggestion Greetings Bob, As a member of your list I have benefited greatly from the exchanges centered around aircraft electrical system design and operation. I expect to start on my plane this summer and will, I'm sure, be asking questions about my specific build. We're all Looking forward to being of assistance! The reason I write it to let you know how valuable the information on the list has been to me in the design and wiring of my boat's electrical system. The parallels between aircraft and boats are many. Wood, Al, and composite construction. 12V operation and the need to be frugal with available power. A host of expensive instruments. A strong desire for robust and reliable operation. A fire at sea or the loss of power in bad weather, while not quite as threatening as the same events in an aircraft, will still make for a bad day. Corrosion is a bigger problem in boats. I don't know if you have considered expanding into this market but I wanted to let you know how much overlap there is. I have been involved in boating on and off since my teen years and held a Coast Guard O.U.P.V. license for the the Great Lakes, Inland Waterway, and Navigable Rivers for 10 years. There is a great "giving away" of knowledge happening everywhere. One notable endeavor can be viewed at http://www.khanacademy.org/ The AeroElectric List is a mature institution with a lot of talents on board. It's unlikely that we achieve the standing of Khan Academy but then, you never know. I've been pondering this phenomenon and exploring ways that I might expand my participation. I even have a new tablet and video capture program I'm learning to use. So Ray, your suggestion is more timely than you know. Your point is well taken and I would point out that except for the devices unique to aircraft (transponders and altitude encoders) most of what we discuss here is common to the full range of vehicles, each with it's own mission, design goals and environmental stresses. In airplanes we may be talking about the range from ultra-lights to LA-IVP with all the goodies. On wheels it might be dirt-bikes to an off-road working or rescue machine. Then of course, there are things that float. The nice thing is that the laws of physics and the conveniences of modern materials are applicable everywhere. Further, there are many techniques and design situations that are common in all vehicular disciplines. Corrosion for airplanes based near oceans is just as vexing as aboard a boat. I have no objections to owner/operators of other vehicles joining us here on the List. There's a lot of opportunity for a cross-pollination between interests (indeed, my first flyable GPS was purchased from a BoatUS catalog!). Please encourage anyone with vehicular electrics questions (or discoveries to share) to join us here on the List. While airplanes brought us all together in the first place, herding electrons gives us cause to stay together. I would make that suggestion to all other List members as well. We could expand that offer to the younger 'students of the electrical arts' as well. The way you add value to knowledge is to expand on its utilization. The best ideas in the universe have no value until somebody puts them to good use . . . Once again, thanks for the work you do on the list. My pleasure sir. Bob . . . ________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Expanded horizons (automotive question)
Date: Mar 23, 2012
Let me be the first with the "Expanded Horizons" to ask an automotive question regarding fault code readers. I have a 1996 GMC Sonoma, Similar to the Chevrolet S-10. My brake line rusted through and dumped the brake fluid, resulting in air entering the ABS unit. After bleeding the ABS module I still have the ABS light illuminated. Brakes seem to work fine but no ABS. I purchased an inexpensive code reader, but it seems that this works on almost all GM vehicles starting at 1996, but would you believe, not mine! Anyone have experience with this problem, including how to fix it, and where I might, if needed, get a code reader? Any help appreciated. ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 23, 2012
We here north of the 49th must have an ELT on every certified aircraft as part of the MEL (minimum equipment list) ELTs are allowed to be removed for normal scheduled maintenance or whenever the unit does not pass inspection. The units may be removed for repair that usually means replacement of the batteries (C size on the old ELTs) for a period not to exceed 90 days. Even though our countries are close in many ways one major difference is the fact we have enormous tracts of totally desolate land and flying over that kind of territory without some kind of back up is totally crazy. As I said the one part, aside of huge cost, I don't like about the 406mHz Elts is the fact they are all digitally assigned to a specific aircraft and there is no vehicle in place that allows the owner to swap one out. It is also illegal to install one into an aircraft that it is not assigned to. In my mind the should have a loaned code available that AMOs, FBOs and the like can put in aircraft while service is being done on the original ELT. Years ago a bizjet went off the end of the runway at Churchill Falls, Labrador, in a snowstorm. For some reason the local tower thought the plane had overshot and gone on to an alternate airport but because of the terrain decided to start a search immediately. Within hours it became apparent they did the right thing because a check with other airports in range of the plane turned up negative. They searched the area for two weeks by helicopter and snowmobile. No results. Six months later a landing plane noticed a glint on the glide path and reporte4d it to the tower. They had found the jet. The passengers all froze to death. The ELT of that plane had been legally removed for scheduled maintenance. Had it been there all the passengers and crew would have been saved. While it is true that today we have all sorts of GPS and digital phones sometimes it is still better to have the tried and true systems as a backup. While I agree that today there are more modes of following aircraft it does give some comfort to have the ELT as a backup. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of BobsV35B(at)aol.com Sent: March 23, 2012 1:05 AM Subject: Re: AeroElectric-List: ELT Antenna Good Evening Noel, What country are you discussing? In the USA, every airline pilot regularly flies without an ELT. Personally, I would be happy to do so if it were not an FAA requirement. I do not feel one whit more secure since we were forced to install the ELT. There are a lot of ways to let folks know when and if you need assistance. I think each pilot should be able to make that decision himself or herself. Happy Skies, Old Bob In a message dated 3/22/2012 8:36:50 P.M. Central Daylight Time, noelloveys(at)yahoo.ca writes: In this country any appliance on a certified aircraft with certain exceptions has to be installed by or checked by a certified AME ( aircraft maintenance engineer ) and the installation has to be documented in the airframe log book and noted if there is a separate log book for the appliance. One of the things I do not like about the new ELT is that aircraft cannot borrow another ELT while one is out having scheduled service done. In the past the AMO I worked for had a "loaner" ELT that we would put in aircraft so they wouldn't have to fly without one... Which is legal for up to 90 days. In fact even a licensed AME is not allowed to change the batteries on an ELT it has to be done by an approved Avionics tech or an approved avionics shop. Amateur built aircraft are another quintal of fish... They don't even have to carry an ELT. Mind I don't know anyone who is stupid enough to fly this land without one. Noel ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: ELT Antenna
Date: Mar 23, 2012
Here in Newfoundland we have forced liability insurance too. The one law I don't agree with is the seatbelt law and I onluy disagree with that one for open cars that do not have roll bars. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of The Kuffels Sent: March 23, 2012 2:15 AM Subject: Re: AeroElectric-List: ELT Antenna Old Bob says: << Noel, .. What country are you discussing? >> His email address is Canada. His description fits what little I know of Canada's regulatory environment. << I do not feel one whit more secure since we were forced to install the ELT. >> This sentiment conflicts with my direct, personal experience. In Alaska in the 1970s when ELTs were first forced upon us, the false activation rate (especially in very cold weather) and the failure to activate rate (mostly due to poor antenna placement) was depressing. Still ELTs managed to save lives, including mine. The newer GPS augmented 406 MHz system is much more effective, quickly providing a location measured in meters. << There are a lot of ways to let folks know when and if you need assistance. >> Disagree. My Alaska crash occurred about 150 miles from any human habitation. My Idaho mountain crash was over in 15 sec. In the meantime, I was a little busy to let anyone know anything. Although I was flying with two other aircraft, they were unable to get our accurate location to Search & Rescue. Our cell phone got through to 911 long enough to let them know there were survivors but not long enough to provide our accurate location. Our 121.5 MHz ELT gave them a location 5 miles in error. But when they got in the neighborhood the ELT did help a little in narrowing our location. The moral, I want as many ways as possible to ask for assistance and help Search & Rescue determine our location. << I think each pilot should be able to make that decision himself or herself. >> Of course, this is a political statement not an aviation safety statement of fact. But given human nature, mandates are not always bad. Sort of like forced automobile liability insurance. Tom Kuffel ________________________________________________________________________________
Date: Mar 23, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons (automotive question)
At 12:55 PM 3/23/2012, you wrote: > > >Let me be the first with the "Expanded Horizons" to ask an automotive >question regarding fault code readers. > >I have a 1996 GMC Sonoma, Similar to the Chevrolet S-10. My brake line >rusted through and dumped the brake fluid, resulting in air entering the ABS >unit. After bleeding the ABS module I still have the ABS light illuminated. >Brakes seem to work fine but no ABS. I purchased an inexpensive code >reader, but it seems that this works on almost all GM vehicles starting at >1996, but would you believe, not mine! Anyone have experience with this >problem, including how to fix it, and where I might, if needed, get a code >reader? Any help appreciated. A 'tad' bit outside the herding of electrons but I think you can find legacy code readers on eBay. It seems likely that with contaminated electronics, the device is probably toast and needs replacement. If push comes to shove, you can pay the tariff for a local read of the codes . . . but it will probably confirm what seems most likely. Bob . . . ________________________________________________________________________________
From: Tim Perry <tperry(at)lvtofly.com>
Subject: Re: Stobes
Date: Mar 23, 2012
Advantage is less noise from the high voltage lines running the length of yo ur airplane. Also your strobes are independent of one another, if you loos e one power supply your other strobes still work. Tim Perry On Mar 23, 2012, at 12:16 PM, Jared Yates wrote: > The remote units are likely going to be a heavier installation, and they w ill require some sort of mechanism for synchronization if there is to be any . > > On Fri, Mar 23, 2012 at 8:05 AM, stearman456 wrote: > > What is the advantage to having local power supplies for your strobe light s vs a single, central,power supply - or vice versa? The two strobe systems I'm considering are identical (lights, output) apart from three power suppl ies vs one. > > Dan > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=369203#369203 > > > > > > > > ========== > -List" target="_blank">http://www.matronics.com/Navigator?AeroElectric-L ist > ========== > http://forums.matronics.com > ========== > le, List Admin. > ="_blank">http://www.matronics.com/contribution > ========== > > > > > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= > ________________________________________________________________________________
From: <bakerocb(at)cox.net>
Subject: Re: ELT Antenna
Date: Mar 23, 2012
3/23/2012 Hello Noel, Thank you for your most courteous reply. You wrote: "New 406 mHz. ELTs are identified to specific aircraft in specific configuration." This is a very important point that you make. Each of those ELT's is also identified to a specific Owner/Operator of that specific aircraft and to a specific Primary and Alternate 24-Hour Emergency Contact associated with that specific ELT and aircraft along with communication information for all of those individuals. See here: http://www.nmea.org/Assets/elt%20406%20registration%20and%20renewal.pdf The purpose of that contact information is to permit rapid communication with one of those individuals should an emergency signal be received by a satellite to confirm that the signal is not a false alarm. Also note that it is possible on that form to submit a Change of ELT Information or Ownership and to do it fairly quickly online at: www.beaconregistration.noaa.gov This would permit a fairly flexible and timely means of swapping a 406 Mhz ELT from one aircraft to another if that became a need and one complied with all provisions of the registration requirements. 'OC' Baker Says: "The best investment we can make is the time and effort to gather and understand knowledge." =================================================== From: "Noel Loveys" <noelloveys(at)yahoo.ca> Sent: Friday, March 23, 2012 2:35 PM Subject: RE: ELT Antenna > My apologies sometimes I forget that most people on the lists are not > Canadian and there are several differences in our aviation procedures. > > In Canada an aircraft flown commercially must have an ELT on board. > However > I'm not sure it has to be turned on. An ELT may be removed for servicing > for up to 90 days. > > New 406 mHz. ELTs are identified to specific aircraft in specific > configuration. One of the new ELT cannot be taken out of one aircraft and > put in another. The identifier code on the ELT is "Married "to a specific > airplane. My understanding is if a large plane is converted from > passenger > to cargo it must be refitted with a new ELT as there is no vehicle to do > this. > > I do like to keep up with what is going on south of the 49th so I will > have > a look through your link and at the same time I'll have another look > through > CARs, Canada's equivalent to FARs. > > Thank you. > > Noel ________________________________________________________________________________
Subject: Re: Stobes
From: "stearman456" <warbirds(at)shaw.ca>
Date: Mar 24, 2012
tperry(at)lvtofly.com wrote: > Advantage is less noise from the high voltage lines running the length of your airplane. Also your strobes are independent of one another, if you loose one power supply your other strobes still work. That makes sense - the kit with the three power supplies is slightly more expensive but I can afford the weight of the extra units. Flying an airplane with noisy strobes has always driven me nuts in the past. Any advice on building the ultimate in quiet strobe installations (Whelen A 490A,TS,CF Power Supplies) appreciated. Dan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369286#369286 ________________________________________________________________________________
Subject: Re: Stobes
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Mar 24, 2012
Bob N. saiys: > I would offer that centralized > supplies are also qualified, i.e. have passed DO-160 > conducted and radiated emissions. So if installed with > attention to good practice for treatment of shields, > they should present no greater noise problem in an > OBAM aircraft than they do in a TC aircraft. I agree Bob, but the basic EMC rule of fixing the noise at its source is a good one, and this points in the direction of putting the HV very close to the strobe tubes. If a standard installation works well, that does not mean a global shift in design is unwise, particularly if some particular design has problems. Bob N. says: > All the strobes on turbine aircraft have local power > supplies but as you've noted, these are breathtakingly > expensive. This is interesting Bob. I wonder if there are some additional design forces at work here? > What kind of voltages/currents and duty cycles > are involved? I've seen some LED anti-collision > protects offered to HBC while I was still there but > folks who showed them to me were unable or reluctant > to discuss design details. > > What's the architecture for wiring up large arrays > of LED's. The tail strobe I saw had about 36 leds > in it. The guy thought it was 4 strings of 9 each. > At 4 volts per led in an overdriven pulse mode, > one comes to believe that a pulsed, 36 volt constant > current supply is used. What approach has been most > attractive in your experience? Bob, I try to stay away from boosted switch-mode LED supplies of any sort. The reason for these (one presumes) is that common lighting is often in strings that make difficult parallel wiring, or that parallel lights demand higher currents, which in some instances is difficult to achieve. But having only 12-28 voltage "Luminaries" allows designs of large parallelism. But this is simple on a PCB. My discontinued (but fabulous) LED position light was 4 strings of 3 (70 mA) LEDs. My LED tail light is a single beefy 1200 mA LED with a linear LM317 regulator. Totally EMC silent.* > I've sold perhaps 50 filtered supplies over the past 4-5 years > and perhaps half that number of filter boards for > folks who already had supply modules. > Bob . . . *As an aside. These supplies were Luxdrive Power Pucks (I don't think Luxeon is involved). You are to be congratulated on quieting these demons. I gave up and dissolved away the potting to examine the PCB. The design was quite clearly laid out by someone who had never taken a Kimmel Gerke course. I toyed with the notion of redesigning the device, but finally sold my shelf full of them on Ebay, converted all my designs to linears, and washed my hands of it. Some data and comments: The Whelen strobe anti-collision power supply output nominal is 550V. This fact alone would make distributed supplies a good design choice. Separate supplies at the tubes should theoretically weigh less if the supporting structure and wiring is included, but the comparison is hard to glean from the published Whelen data. Whelen has one spearate strobe supply that says "cannot be synchronized", which is weird when you understand how little it takes to do so. My "vapor-ware" design uses a parallel string of two RED leds. Oddly, the FAA has had a long love affair with neon tubes since the 1930s, so red is a permissible color and red LEDs have the highest efficiency. (But the human visual response is best at 555 nm yellow green...the color under the African jungle canopy). Xenon blue-white strobes are easy to make. (A side note for your kid's science project...Radon should make great flash tubes..unfortunately all radon isotopes are radioactive.) But I digress.... My design uses an array of red LEDs for 12V, and a parallel array of 4 for 28V. powered by small local supercaps (hey, why not?). Each LED "strobe lamp" is basically pulsed on and off and synchronized by a central circuit the size of a postage stamp. The power to the LED strobes is the same as the position lights. I would gladly publish the circuit but it is incomplete...as is my Glastar, which I'd better start working on. My electro-whizzie work has slowed down since I spend much of my time selling switch guards. NASCAR is also a big market. See attached. (The Redbull team was so secret at first I thought they had to be spooks!) -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369288#369288 Attachments: http://forums.matronics.com//files/redbull_2_156.jpg ________________________________________________________________________________
Subject: Re: Expanded horizons for the List?Marketing suggestion
From: Terry Watson <terry(at)tcwatson.com>
Date: Mar 24, 2012
Bob, I was so pleased to see you mention the Khan Academy. It is a great example - as is your aeroelectric list - of the extraordinary but becoming ordinary benefits of modern information technology. To you and those of your readers who might want to avoid being blind-sided by the accelerating rate of change of our probable future, I want to recommend a new book: "Abundance: The Future is Better Than You Think", by Peter Diamandis. I don't think I have read anything in the 32 years since Alvin Toffler's "The Third Wave" that made me more excited and optimistic about the near future. To add a note of credibility to the Abundance book for aeroelectric list subscribers, Peter Diamandis is the man who created the X prize that inspired Paul Allen to finance Burt Rutan to put the first private astronauts into space. He has gone on to create other X prizes which you will read about in the book. What's so amazing is how rapidly the very high bar set for the prizes is being achieved. Just Google "Abundance" and you will find links to the book's website and to Amazon if you want to read reviews or buy it. Terry RV-8A stalled Seattle ________________________________________________________________________________
Subject: Re: wingtip vor antenna
From: Mark Harris <harrismarkr(at)hotmail.com>
Date: Mar 24, 2012
Hi Bob Just another quick question I fabricated the parts for the VOR antenna today.is it ok to alocrom the parts before assembly and then would paint etch prime be ok ,I would bear the connection points. Thanks Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 21 Mar 2012, at 01:50, "Robert L. Nuckolls, III" wrote: > > At 02:18 PM 3/20/2012, you wrote: >> >> Cheers Bob >> >> Looks like a job for the weekend > > Do you have access to an antenna analyzer or > at least an SWR meter? > > > Bob . . . > > > > > ________________________________________________________________________________
Subject: Re: Expanded horizons for the List?Marketing suggestion
From: "nuckollsr" <bob.nuckolls(at)aeroelectric.com>
Date: Mar 24, 2012
Thank you for the recommendation. I'll get it. Speaking of "abundance', I'm finding it easy to be overwhelmed by the quantity and scope of good data available off the 'net for the time and effort to download . . . THEN comes the investment of time to absorb it. I had seen some of Milton Friedman's work in 10 minute chunks . . . but somebody turned me on to "Free to Choose" in 10 segments and downloadable from YouTube. I captured all the videos and now need to get them watched. I think I may strip off the audio so I can listen to them in the car. I do spend a lot of time on the road these days. Dr. Dee turned me onto Kahn. She too has an intense interest in the video mini-lecture technique. There are a few important points in her statistics classes that are common stumbling blocks for some students. While fully willing to explain the material again, students who are already on board are not too happy about 'back tracking'. We've decided to do some mini-lectures on those sicking points that can be accessible to any Bethany student 24/7. The hope is that these productions will bring the lagging students up at their own speed/convenience, provide good review for the rest, and make progress in the class room match the syllabus. We have similar situations here on the List in what has been called 'frequently asked questions'. An exciting 'new' concept, at least for me. Once I'm comfortable with the mechanics of production and we have Dr. Dee's most pressing needs addressed, I'll be looking for suggestions from folks here on the List for topics to be 'canned' in a similar fashion. Thanks for the tip! Bob . . . Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369311#369311 ________________________________________________________________________________
From: "Neal George" <n8zg(at)att.net>
Subject: Re: Expanded horizons for the List?Marketing suggestion
Date: Mar 24, 2012
Bob - care to share that link? neal -----Original Message----- From: nuckollsr I had seen some of Milton Friedman's work in 10 minute chunks . . . but somebody turned me on to "Free to Choose" in 10 segments and downloadable from YouTube. Bob . . . ________________________________________________________________________________
Subject: Re: Expanded horizons for the List?Marketing suggestion
From: Terry Watson <terry(at)tcwatson.com>
Date: Mar 25, 2012
Bob, Thanks for the heads up about Free to Choose. I have the book and remember the series. I will look on the web for the programs to see them again. As educators, you and Dr. Dee will not be as surprised as I was with the section on education in the Abundance book. It seems there is a huge desire in kids no matter their location or social status to learn, which is driving this digitization of learning and making it so universally available. One of the to me unexpected aspects of the book is the emphasis on the "bottom billion" of the six billion or so people on the planet. They will have perhaps the most dramatic improvement in their lives, but the rest of us will have the huge benefit of this until now untapped brain power. As for learning while driving, I have an older iPod mounted in my car, loaded with lecture courses from the company named The Great Courses, formerly known as The Teaching Company. I have bought about dozens of college-level courses from them over the years. For the most part they are excellent. I would be smarter if I had a longer commute! My apologies to those not interested for dragging the discussion off course. Terry ________________________________________________________________________________
Subject: Re: Expanded horizons for the List?Marketing suggestion
From: "nuckollsr" <bob.nuckolls(at)aeroelectric.com>
Date: Mar 25, 2012
Sure Neal, http://tinyurl.com/876dxqe There will be some similar but unrelated links pop up but what you're looking for are parts 1 thru 10 of a 10-part series. I have the series captured on a CD. If you'd like to bypass the downloading process, drop me a direct email with an address. I'll send you a copy. That applies to anyone on the List who would like to exploit the genius of a great teacher. Terry, I'm not so sure we're 'off topic' here. I've been doing this q&a work for over 23 years. I started on Avsig back when Compuserve was king. As I look back over this experience, I recall quantum jumps in technology. Within the state of our 'art' we had adaptations of lightweight automotive alternators to legacy architectures. We exploited the rise of the RG battery. We witnessed the demise of the vacuum pump. GPS systems that cost us $30K a pop in 1985 begat $200 hand-helds that would let us fly custom 'non-precision' approaches with 10x the accuracy of anything the FAA chose to call 'non-precision'. Electronic ignition has evolved through a number of iterations to become quite commonplace and very affordable. We enjoyed the rise of the glass cockpit. All manner of software driven tools found their way into the cockpit which added to our confidence and competence as pilots. Those are the highlights I can think of a the moment. What about the next 20 years? I don't see any really bright stars on the horizon. Lithium batteries are lurking in the wings but nothing really confidence building happening there yet. We have tremendous tools for stuffing a lot of 'kitchen sink' features into our panel mounted toys . . . but what kinds of things do we see that will make quantum jump performance in our airplanes? Will they go still faster on less fuel? Be lighter and easier to build? Less expensive? Maybe, but it's not clear to me now. Okay, what is our role here on the List to ease the way and/or expand the horizons of then next 20 years intake of new enthusiasts? What kind of resource can we build for that kid that stands at the bottom of the driveway peering into the open garage door with wonder at the machine which is slowly coming into being? It's obvious that pubic education is providing fewer tools, fewer examples of simple-ideas, fewer demonstrations of recipes for success that go into successful completion and competent operation of an OBAM aircraft. So that's the core of my thoughts right now. What SHOULD this List look like 20 years from now . . . and can we make it happen? Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369330#369330 ________________________________________________________________________________
From: "Neal George" <n8zg(at)att.net>
Subject: Re: Expanded horizons for the List?Marketing suggestion
Date: Mar 25, 2012
Thanks Bob - I just re-read the previous. Now my face is all red... :) I'm really not too lazy to do a simple search - just completely missed the YouTube reference. neal ________________________________________________________________________________
From: "Bill Bradburry" <bbradburry(at)bellsouth.net>
Subject: Re: Expanded horizons for the List?Marketing suggestion
Date: Mar 25, 2012
I have been trying to figure out how to download the "Free to Choose" videos to my computer. Bob mentioned that he had done it. Does anyone know how he accomplished that? Bill B -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of nuckollsr Sent: Saturday, March 24, 2012 9:42 PM Subject: AeroElectric-List: Re: Expanded horizons for the List?Marketing suggestion Thank you for the recommendation. I'll get it. Speaking of "abundance', I'm finding it easy to be overwhelmed by the quantity and scope of good data available off the 'net for the time and effort to download . . . THEN comes the investment of time to absorb it. I had seen some of Milton Friedman's work in 10 minute chunks . . . but somebody turned me on to "Free to Choose" in 10 segments and downloadable from YouTube. I captured all the videos and now need to get them watched. I think I may strip off the audio so I can listen to them in the car. I do spend a lot of time on the road these days. Dr. Dee turned me onto Kahn. She too has an intense interest in the video mini-lecture technique. There are a few important points in her statistics classes that are common stumbling blocks for some students. While fully willing to explain the material again, students who are already on board are not too happy about 'back tracking'. We've decided to do some mini-lectures on those sicking points that can be accessible to any Bethany student 24/7. The hope is that these productions will bring the lagging students up at their own speed/convenience, provide good review for the rest, and make progress in the class room match the syllabus. We have similar situations here on the List in what has been called 'frequently asked questions'. An exciting 'new' concept, at least for me. Once I'm comfortable with the mechanics of production and we have Dr. Dee's most pressing needs addressed, I'll be looking for suggestions from folks here on the List for topics to be 'canned' in a similar fashion. Thanks for the tip! Bob . . . Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369311#369311 ________________________________________________________________________________
Date: Mar 25, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons for the List?Marketing
suggestion At 06:20 PM 3/25/2012, you wrote: > > >I have been trying to figure out how to download the "Free to Choose" videos >to my computer. Bob mentioned that he had done it. Does anyone know how he >accomplished that? You need the youtube downloader. Here's one good source http://tinyurl.com/68o7jqn Bob . . . ________________________________________________________________________________
From: "Bill Bradburry" <bbradburry(at)bellsouth.net>
Subject: Re: Expanded horizons for the List?Marketing
suggestion
Date: Mar 25, 2012
Thanks. Bob! Bill B _____ From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Sunday, March 25, 2012 8:00 PM Subject: RE: AeroElectric-List: Re: Expanded horizons for the List?Marketing suggestion At 06:20 PM 3/25/2012, you wrote: I have been trying to figure out how to download the "Free to Choose" videos to my computer. Bob mentioned that he had done it. Does anyone know how he accomplished that? You need the youtube downloader. Here's one good source http://tinyurl.com/68o7jqn Bob . . . ________________________________________________________________________________
Date: Mar 26, 2012
Subject: Re: ELT Antenna
From: Richard Girard <aslsa.rng(at)gmail.com>
Two points for clarification. ELT's, per 91.207, are required in airPLANES, not in airCRAFT. That's why my E-LSA airplane has one but my E-LSA Weight Shift Control aircraft (i.e. Trike) does not. " (a) Except as provided in paragraphs (e) and (f) of this section, no person may operate a U.S.-registered civil airplane unless=97 " Exempted per 91.207 f (9) " Aircraft equipped to carry not more than one person". And yes, I see how the waters are muddied by the use of airplane in the "Thou shalt" section of the rule, and aircraft in the "Thou may not" in the list of exemptions. Thank goodness my DAR understood the rule. Rick Girard On Fri, Mar 23, 2012 at 7:36 AM, wrote: > > 3/23/2012 > > Hello Noel Loveys, Thank you for your inputs on this subject, but in the > interest of stamping out hearsay, gossip, and rumors regarding experiment al > amateur built aircraft I'd like to point out that some of your comments a re > just not applicable in the USA. > > The following statements that you wrote are not correct in the USA: > > 1) "In that case if even on an OBAM aircraft the ELT and transponder must > be > installed or signed off by a certified AME (Canada) or A&P (U.S.)" > > 2) "One of the things I do not like about the new ELT is that aircraft > cannot > borrow another ELT while one is out having scheduled service done." > > 3) "...so they wouldn't have to fly without one... Which is legal for up > to 90 > days." > > Note that the regulatory requirements for having an ELT in a US registere d > civil aircraft operating in the US, and the circumstances permitted for > flying without an ELT installed, are contained in 14 CFR 91.207. That > section is too long and complicated to be copied, or even extracted in th is > posting. It may be accessed here: > > http://ecfr.gpoaccess.gov/cgi/**t/text/text-idx?c=ecfr&sid=** > e13e8f64d66f124a79dbd562cbe93f**0b&rgn=div8&view=text&node=14:** > 2.0.1.3.10.3.7.4&idno=14<http://ecfr.gpoaccess.gov/cgi/t/text/text-idx? c=ecfr&sid=e13e8f64d66f124a79dbd562cbe93f0b&rgn=div8&view=text&node =14:2.0.1.3.10.3.7.4&idno=14> > > 4) "In fact even a licensed AME is not allowed to change the batteries on > an ELT > it has to be done by an approved Avionics tech or an approved avionics > shop." > > 5) "Amateur built aircraft are another quintal of fish... They don't eve n > have > to carry an ELT." > > They do in the USA in accordance with 14 CFR 91.207. > > Thanks for your help in posting accuracy. > > 'OC' Baker Says: "The best investment we can make is the time and effort > to gather and understand knowledge." > > ======================== ======**================== ============**= > > > From: "Noel Loveys" <noelloveys(at)yahoo.ca> > Subject: RE: AeroElectric-List: ELT Antenna > > In that case if even on an OBAM aircraft the ELT and transponder must be > installed or signed off by a certified AME (Canada) or A&P (U.S.) > > > Noel > > From: owner-aeroelectric-list-**server(at)matronics.com<owner-aeroelectric-l ist-server(at)matronics.com> > [mailto:owner-aeroelectric-**list-server(at)matronics.com] > On Behalf Of Kelly > McMullen > Sent: March 21, 2012 8:26 PM > Subject: RE: AeroElectric-List: ELT Antenna > > > The minimum for use of ELTs is to demonstrate that the complete system > meets > the TSO. Good luck with doing that with a roll your own antenna of unknow n > impedance and SWR. ELTs and transponders are two items on OBAM aircraft > that > must comply with the TSO. > > > Noel wrote: > > It sure would be... but for amateur aircraft you might be able to use you r > own antenna. > > > Noel > > > From: owner-aeroelectric-list-**server(at)matronics.com<owner-aeroelectric-l ist-server(at)matronics.com> > [mailto:owner-aeroelectric-**list-server(at)matronics.com] > On Behalf Of Ed > Holyoke > Sent: March 20, 2012 10:18 PM > Subject: Re: AeroElectric-List: ELT Antenna > > > Have to look at your ELT installation instructions. The ELT is TSOed and > might require that you use their antenna. > > ======================== ======**================== ========= > > From: "Noel Loveys" <noelloveys(at)yahoo.ca> > Subject: RE: AeroElectric-List: ELT Antenna > > > In this country any appliance on a certified aircraft with certain > exceptions has to be installed by or checked by a certified AME ( aircraf t > maintenance engineer ) and the installation has to be documented in the > airframe log book and noted if there is a separate log book for the > appliance. > One of the things I do not like about the new ELT is that aircraft cannot > borrow another ELT while one is out having scheduled service done. In th e > past the AMO I worked for had a "loaner" ELT that we would put in aircraf t > so they wouldn't have to fly without one... Which is legal for up to 90 > days. > In fact even a licensed AME is not allowed to change the batteries on an > ELT > it has to be done by an approved Avionics tech or an approved avionics > shop. > Amateur built aircraft are another quintal of fish... They don't even ha ve > to carry an ELT. Mind I don't know anyone who is stupid enough to fly th is > land without one. > > Noel > > =====**=================== ===========**= /www.matronics.com/Navigator?AeroElectric-List> =====**=================== ===========**= =====**=================== ===========**= com/contribution> =====**=================== ===========**= > > -- Zulu Delta Mk IIIC Thanks, Homer GBYM It isn't necessary to have relatives in Kansas City in order to be unhappy. - Groucho Marx ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Re: Expanded horizons for the List?Marketing suggestion
Date: Mar 26, 2012
Yogi Berra might have said "It's hard to predict the future because it hasn't happened yet", but as far as I know, he didn't. We don't know precisely what the challenges and opportunities of the future will be, but we can get a pretty good idea of them by listening to the experts. We do know that the rate of change is accelerating; we do know that big problems have a way of attracting smart people with big ideas, and we do know that there will be unexpected problems and unexpected discoveries. And we know that right now we have unprecedented power to communicate, and that that power will only increase. When I watch a Khan Academy video lesson, I can easily imagine a series of Bob Nuckolls Aeroelectric Academy videos - short and very informal, presented exactly like you would do sitting next to an interested kid with sketch paper and colored pens. Diagrams would be free hand, as would graphs. Informal - that's what keeps it from being intimidating. They would start with the most basic concepts of electronics and build up an appreciation and understanding, just like you do in your classes and here on the Aeroelectric list. The point is to keep it from becoming a Big Deal - no fancy productions - just Bob Nuckolls telling us about electronics in five to ten minute bites. Over time, there would become a library of these. When someone asked a question that lent itself to the format, your answer would become another lesson that could be located by a search of the data base of lessons. You seem to have become highly successful giving away your knowledge, but there is a value here that is worth paying for. But my guess is that when you think of a kid in Pakistan or Fiji or China who has dreamed of flying ever since he saw his first small airplane, you will want him to have whatever knowledge you can give him. Here are a few web addresses that might give your subscribers an idea of what we are talking about: Khan Academy: http://www.khanacademy.org/ Peter Diamandis: Abundance is our future: "The cell phone in your pocket is a million times cheaper and a thousand times faster than the supercomputer of the '70's." http://www.ted.com/talks/peter_diamandis_abundance_is_our_future.html About ten minutes into this 16 minute TED talk, you will see what autonomous air traffic control might be like: : http://www.ted.com/talks/vijay_kumar_robots_that_fly_and_cooperate.html The TED talks are a great place to visit regularly to get a fresh perspective on the world we live in. Terry ________________________________________________________________________________
Subject: Re: Source for Bakelite - 1/32" thick
From: "Alfio" <longeron(at)gmail.com>
Date: Mar 27, 2012
harrismarkr(at)hotmail.co wrote: > Hi Alfio > > I am planning on doing the same do you have a drawing with the required dimensions on.The drawing I have dose not have the dimensions. > > Thanks > > Mark > Here are some dimensions (enclosed jpg), though some dimension information is still missing for the gamma match. I will probably just borrow an SWR meter and 'play'. Thanks for all that responded. I'll be looking for paper phenolic xxx since it has low dielectric loss at high frequencies. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369400#369400 Attachments: http://forums.matronics.com//files/plans24bit_304.jpg ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons for the List?Marketing
suggestion At 12:06 AM 3/27/2012, you wrote: The point is to keep it from becoming a Big Deal no fancy productions just Bob Nuckolls telling us about electronics in five to ten minute bites. Exactly. When discussing this with professional college level teachers, I often get what appears to be some degree of skepticism in their response, "Yeah, but what about 'quality' of the education?" My answer is, "The presentations are for simple-ideas. Deduction of presentation of fact. Any one item taken by itself can be explained by a willing presenter of any degree or credential. The information being offered can be taken up by any willing and able listener. The study and sharing of simple ideas has no rigorous demand upon what we often call 'quality'. It needs only to be true and well explained. If one considers legacy offerings for traditional institutions of learning, success for their endeavors is measured by how well simple-ideas have be taken up by students in a manner that makes them potential ingredients that go into recipes for success. Sadly, I think the institutions of learning have built a sort of firewall between themselves as disseminators of ingredients (books and calculators) and the chefs (hammers-n-saws) who turn those ideas into useful products. Using the KhanProcess to augment the classroom presentation increases likelihood of acquisition and retention of ingredients by students of every learning-rate which gives the teacher more time to talk about recipes. I had only the most rudimentary grasp of this process when I started the 'Connection . . . but intuitively I knew that it was insufficient to put out a simple cookbook, Wire it up like this and trust me . . . it will work". That's why the 'Connection is mostly ingredients topped off with only one chapter of recipes at the back of the book. Further, issues of 'quality' are easier to address. Throughout our formal education experience, we're offered x-thousand simple- ideas. Your PhD is awarded when you demonstrate a mastery of those ideas. The really neat thing about the KhanProcess is that the source of those ideas can be any willing/able presenter or teacher without having an deleterious impact on legacy notions of 'quality'. Some teachers I've talked to get that far away look of appreciative contemplation, others remain skeptical. Given the apparent value and rate of growth for the KhanProcess, even skeptics might do well to consider exploitation of these new tools. Another neat feature of productions by KhanProcess is that one's students might revisit the 'classroom' years hence for a review and the teacher might never know it. But the fact that a student remembers where they were introduced to those ingredients before can come back for a memory jump-start is a huge asset to that individual's successes later. I've suggested to some college administrators that these presentations could be a real adjunct marketing tool for their school struggling to bring in and retain students. Suppose learning requirements for say 10% of their total credit hours could be achieved on line at no cost other than the student's performance. Further, they could take the course as many times as they wanted to raise the grade. But credit for those courses would not be awarded until the other 90% was completed at the usual tariff and expenditure of time in the classroom. This seems to be a good way to get a student invested in achieving the desired outcome for graduation. Having semester worth of high level achievement to capstone their transcript seems like pretty powerful incentive to get-er-done. Over time, there would become a library of these. When someone asked a question that lent itself to the format, your answer would become another lesson that could be located by a search of the data base of lessons. You seem to have become highly successful giving away your knowledge, but there is a value here that is worth paying for. But my guess is that when you think of a kid in Pakistan or Fiji or China who has dreamed of flying ever since he saw his first small airplane, you will want him to have whatever knowledge you can give him. That's the idea . . . or at least I think it is. It's coming together in a plan for a series of activities that sure make sense to me today. Nothing ventured, nothing gained. I'm going to stir the pot see if it still makes sense a few years from now. Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Source for Bakelite - 1/32" thick
>Here are some dimensions (enclosed jpg), though some dimension >information is still missing for the gamma match. I will probably >just borrow an SWR meter and 'play'. > >Thanks for all that responded. I'll be looking for paper phenolic >xxx since it has low dielectric loss at high frequencies. Here's a little clearer image that I think is adequately dimensioned. http://www.matronics.com/forums/viewtopic.php?t=89235 Bob . . . ________________________________________________________________________________
Subject: Re: Source for Bakelite - 1/32" thick
From: "Alfio" <longeron(at)gmail.com>
Date: Mar 27, 2012
Thanks Bob. I have that one as well. I am still looking for some dimensions on the gamma match though. The gap is identified, but not how far it is from the wingtip support for instance. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369417#369417 ________________________________________________________________________________
Date: Mar 27, 2012
Subject: Re: Expanded horizons for the List?Marketing suggestion
From: Bill <wtrooper(at)gmail.com>
> At 12:06 AM 3/27/2012, you wrote: > > The point is to keep it from becoming a Big Deal ' no fancy productions ' > just Bob Nuckolls telling us about electronics in five to ten minute bite s. > Annie Leonard's "Story Of Stuff" is a fine example of brevity and VERY simple production values. Note: Pay attention to the method, the message may be strong medicine for some. http://www.storyofstuff.org/movies-all/story-of-stuff/ Bill SF bay area ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons for the List?Marketing
suggestion >It is easy to confuse the quality of the presentation, which can be >easily be shown to and judged by others and the quality of the >knowledge transfer, which is not as easily judged. But who is the ultimate arbiter of quality? If I enroll in some formal class, is my grade in that class the true reflection of value or 'quality'. As student, I think I have to be the final judge as to the value received (knowledge) for value given ($time$ and $tuition$). There have been hundreds of studies on retention rates for material offered in the legacy student- classroom-professor setting. For the time and dollars it costs to go to college, one is prompted to re-assess return on investment. But when you sit down with a well crafted KhanProcess presentation, what demands are made of the investor? Who is to decide whether the efforts 'invested' have a satisfactory return? Certainly the instructor is completely out of the loop. Of 1500 or so folks who receive the List messages every day, there are only a few dozens of 'active' participants . . . but I would think that the remainder would un-subscribe if they did not find value in watching those conversations go by. >College professors are as prone to be attracted to shiny things as >anyone else. Sure, but this isn't about professors of any stripe, it's about packaging useful information into formats that are free of intimidation, expenses bordering on predatory and a pedantic focus on getting a grade/sheepskin. >I think to try to engage with the formal educational system during >the startup of your endeavor will add nothing and present addition problems. I haven't the least interest in engaging the formal education system. I've offered some observations and links to what appears to be a bright educational star coming over the horizon . . . but whether or not 'they' take the process any further has no implications for anything I propose to do. I DO have an interest in seeing my wife's employer do well . . . for obvious reasons. She will be experimenting with these tools for her own purposes and then promoting them to the rest of the faculty. Any risk for "presenting additional problems" is not a clear. I think problems burdening most institutions are generated from within and perhaps too deeply entrenched. >Create the mechanism to transfer the knowledge from you to the >motivated learner, and the knowledge will be spread. If academia >finds it useful and not a threat to it's paradigm, perhaps they will use it. Exactly! >For me the value of resources like Kahn Academy is access to the >knowledge without being subjected to foibles academia. Right on again . . . which goes to my assertion of problems being mostly generated from within. >I am currently watching the Calculus presentations. They are a good >example of the simple tools that are necessary to convey profound knowledge. Yes . . . yet nobody has made any demands upon you nor taken it upon themselves to assess the 'quality' of your outcome. If you're not happy with your experience, no doubt you'll discontinue the activity. If you are pleased with the outcome then the return on investment can be nothing but good. Talk about win-win. Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: David <ainut(at)knology.net>
Subject: Re: Expanded horizons for the List?Marketing
suggestion Mr. Nuckolls, don't forget curiosity and the sheer joy of learning. David M. Robert L. Nuckolls, III wrote: > > > >> It is easy to confuse the quality of the presentation, which can be >> easily be shown to and judged by others and the quality of the >> knowledge transfer, which is not as easily judged. > > But who is the ultimate arbiter of quality? If I > enroll in some formal class, is my grade in that > class the true reflection of value or 'quality'. > As student, I think I have to be the final judge > as to the value received (knowledge) for value > given ($time$ and $tuition$). > > There have been hundreds of studies on retention > rates for material offered in the legacy student- > classroom-professor setting. For the time and dollars > it costs to go to college, one is prompted to re-assess > return on investment. <<>> ________________________________________________________________________________
Subject: Latest Revision of Z-13/8 ???
From: "idleup" <matt(at)mattandmel.com>
Date: Mar 27, 2012
What is the latest revision of Z drawing 13/8? I found one Rev. Q which I know is old, and another Rev. R that is dated 11/18/10 but it is watermarked with the word "PRELIMINARY". Is that the latest version? if not, where do I get it? Thanks, Matt Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369442#369442 ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Source for Bakelite - 1/32" thick
At 11:09 AM 3/27/2012, you wrote: > >Thanks Bob. I have that one as well. I am still looking for some >dimensions on the gamma match though. The gap is identified, but not >how far it is from the wingtip support for instance. > > Did a little autocad layout and found that the top capacitor plate doesn't come all the way to the end of the capacitor di-electric. Given that it's a 60-60-60 triangle with an inside dim of 5.00 inches, the details come out something like this: http://tinyurl.com/7jatp88 Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons for the List?Marketing
suggestion At 06:45 PM 3/27/2012, you wrote: > >Mr. Nuckolls, don't forget curiosity and the sheer joy of learning. Oh . . . yeah . . . their IS that! Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Latest Revision of Z-13/8 ???
At 08:19 PM 3/27/2012, you wrote: > >What is the latest revision of Z drawing 13/8? I found one Rev. Q >which I know is old, and another Rev. R that is dated 11/18/10 but >it is watermarked with the word "PRELIMINARY". Is that the latest >version? if not, where do I get it? OOPS! You caught me! The preliminary tag should have been removed from the .pdf a long time ago. I've updated both the .dwg and .pdf files to revision R. Thanks for the heads up! Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Expanded horizons for the List?Marketing
suggestion At 07:03 PM 3/27/2012, you wrote: Greetings Bob, . . . this is what lead me to advocate for you avoiding academia. Understand and agree . . . not hoping to develop any institutional alliances. But I do have a personal interest in Dr. Dee's endeavors as well. In the teacher/learner system both judge the quality by the transfer of knowledge. The student invests $time$ based on the premise that the credential will yield a better quality of life in the future, regardless of whether or not the knowledge is acquired or retained. A discussion of possible changes and their consequences to the university/student system would be a list unto it's self. You got that right! I question whether defining it as "your wife's employer" rather than as "the formal education system" changes whether or not it's a duck. Understand . . . but even the most disciplined skeptic can suffer hope. And she is a dedicated teacher who puts her students first. I hope however you choose to develop your knowledge transfer methodology, you will keep the teacher/learner system as a viable part. Absolutely. I think it has worked for me and noteworthy individuals have exploited the tools to take the concept to new heights. Pretty exciting stuff. I think we are in agreement my friend. Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: David <ainut(at)knology.net>
Subject: Re: Expanded horizons for the List?Marketing
suggestion It's the only reason I still go to school at age 57. David M. Robert L. Nuckolls, III wrote: > > > At 06:45 PM 3/27/2012, you wrote: >> >> Mr. Nuckolls, don't forget curiosity and the sheer joy of learning. > > Oh . . . yeah . . . their IS that! > > > Bob . . . > > -- I DO have a reasonable expectation of privacy in my cell phone and everywhere else. In fact, gubmnt,I insist upon it. ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: HID lighting observations
I'm still waiting to get into the lab to do some quantitative testing on some HID light kits. In the mean time, I've installed a pair on my Kia mini-van. I've observed the following: The lights generate noticeable but not overwhelming noise in the AM broadcast band during the warm up phase. About 30 seconds. Don't hear it after the lamps are warmed up. The kits I have generate a strong transient of some variety onto the bus when first turned on. If I have the cruise control engaged at the time, it drops off line. I have to shut the engine off completely to get the cruise control to reset and wake up. This sort of event isn't even watched for under DO-160 explorations. I'll have to set up on the bench to capture and quantify this characteristic. But in the mean time, be aware that a turn-on transient MIGHT manifest in erratic behavior of some micro-processor based electro-whizzies in your airplane. If any such events are identified and repeatable, I'd like to know about them. Bob . . . ________________________________________________________________________________
Date: Mar 27, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Source for Bakelite - 1/32" thick
At 11:09 AM 3/27/2012, you wrote: Thanks Bob. I have that one as well. I am still looking for some dimensions on the gamma match though. The gap is identified, but not how far it is from the wingtip support for instance. Did a little Autocad layout and found that the top capacitor plate doesn't come all the way to the end of the capacitor di-electric. Given that it's a 60-60-60 triangle with an inside dim of 5.00 inches, the details come out something like this: Just discovered that I had the elements of the gamma-match swapped end for end in the drawing. Here's the corrected version. http://tinyurl.com/7wol3jx Bob . . . ________________________________________________________________________________
Subject: Re: Source for Bakelite - 1/32" thick
From: "Alfio" <longeron(at)gmail.com>
Date: Mar 28, 2012
nuckolls.bob(at)aeroelect wrote: > At 11:09 AM 3/27/2012, you wrote: > > Did a little Autocad layout and found that the top > capacitor plate doesn't come all the way to the end > of the capacitor di-electric. Given that it's > a 60-60-60 triangle with an inside dim of 5.00 > inches, the details come out something like this: > > > http://tinyurl.com/7wol3jx (http://tinyurl.com/7wol3jx) > > Bob . . . Just what I was looking for. Thanks. Alfio Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369456#369456 ________________________________________________________________________________
Subject: Re: Source for Bakelite - 1/32" thick
From: "racerjerry" <gki(at)suffolk.lib.ny.us>
Date: Mar 28, 2012
Be careful when substituting non-reinforced plastic material for Micarta sheet. Often, you will need a phenolic laminate material with resin impregnated layers of linen cloth to provide support and to preserve electrical spacings at elevated temperatures. Many non-reinforced plastics will begin to flow when heated. Impregnated cloth or paper will maintain some electrical spacing even when charred. Aircraft Spruce still sells Grade L (linen base) phenolic sheet 1/16 and thicker, which is the generic equivalent of Micarta. -------- Jerry King Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369466#369466 ________________________________________________________________________________
Date: Mar 28, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Source for Bakelite - 1/32" thick
At 10:29 AM 3/28/2012, you wrote: > >Be careful when substituting non-reinforced >plastic material for Micarta sheet. Often, you >will need a phenolic laminate material with >resin impregnated layers of linen cloth to >provide support and to preserve electrical >spacings at elevated temperatures. Many >non-reinforced plastics will begin to flow when >heated. Impregnated cloth or paper will >maintain some electrical spacing even when charred. > >Aircraft Spruce still sells Grade L (linen >base) phenolic sheet 1/16 and thicker, which >is the generic equivalent of Micarta. Good thoughts. At least this case doesn't raise critical questions as to structural integrity. The parts being joined are exceedingly light. The substitution problem here is two-fold. Structural as you've correctly deduced PLUS electrical. The insulating material is the dielectric for a high frequency capacitor that is expected to TUNE out some reactive components of the gamma-match elements. A List member is sending me a store-bought antenna. I'll mount it on a ground plane and get some SWR data. Then I'll measure the VALUE of the as-purchased capacitor. Then we'll have a basis for evaluating the electrical qualities of any proposed substitution. I'm thinking that we can fabricate the struts, insulator and capacitor from a single piece of double-sided etched circuit board material. I have lots of the material to play with and can pretty easily test it against the store bought design for optimal dimensions. In fact, I'm considering a 'mod' to the design that uses a variable capacitor soldered down to the ECB material . . . which must be adjusted but it's pretty easy to do with the ship's comm transmitter or a hand held and an SWR meter. Bob . . . ________________________________________________________________________________
Date: Mar 28, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
Thanks to List member van Saten, we've got some better details for a DIY wingtip VOR antenna. See: http://tinyurl.com/6v5gvhx It seems that the sketch I was working from years ago was either not up to date or in error. The insulator turns out to be either glass or cloth filled phenolic, 0.062 inches thick. The measured value of an off-the-shelf gamma-match capacitor is 34 pf @ 1 KHz. I think the data above will get the builder closer to a workable example of this particular antenna. Thanks Don! Your antenna will be back in the mail today. Bob . . . ________________________________________________________________________________
From: "Don" <dsvs(at)ca.rr.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
Date: Mar 28, 2012
Bob, Did you install the new cap or jhust test it by itself? -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, March 28, 2012 1:48 PM Subject: AeroElectric-List: Re: Wingtip VOR antenna . . . a clearer picture --> Thanks to List member van Saten, we've got some better details for a DIY wingtip VOR antenna. See: http://tinyurl.com/6v5gvhx It seems that the sketch I was working from years ago was either not up to date or in error. The insulator turns out to be either glass or cloth filled phenolic, 0.062 inches thick. The measured value of an off-the-shelf gamma-match capacitor is 34 pf @ 1 KHz. I think the data above will get the builder closer to a workable example of this particular antenna. Thanks Don! Your antenna will be back in the mail today. Bob . . . ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
Date: Mar 28, 2012
Bob, Thanks for this drawing. It gives me a general idea of what this thing is - I could almost build one from it... A few more dimensions would be very helpful. (or else I'll have to get out my trig calculator) My wish list: 1. Explicit dimensions for length of each piece 2. A label for each piece. For us antenna ignoramuses (or is that ignorami?) I cannot differentiate between the "antenna" and "ground strut". 3. Call-out fastenings and their positions. Are they critical? (e.g. can I substitute a #4 machine-screw & nut instead of a 3/32 dia. aluminum rivet or a #6 screw or a #8, etc?) 4. Some very explicit instructions about how to connect the feed line: a. how to prepare the shield (I'm assuming a coax feed line) b. type of wire terminals (or is it soldered?) c. or can a coax connecter be installed on the antenna 5. How is the structure mounted in the airplane? How did you measure the capacitance? As someone who knows nada about RF, a spec like X pf at Y freq fascinates me.. Thx, Jeff Luckey -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, March 28, 2012 12:48 Subject: AeroElectric-List: Re: Wingtip VOR antenna . . . a clearer picture Thanks to List member van Saten, we've got some better details for a DIY wingtip VOR antenna. See: http://tinyurl.com/6v5gvhx It seems that the sketch I was working from years ago was either not up to date or in error. The insulator turns out to be either glass or cloth filled phenolic, 0.062 inches thick. The measured value of an off-the-shelf gamma-match capacitor is 34 pf @ 1 KHz. I think the data above will get the builder closer to a workable example of this particular antenna. Thanks Don! Your antenna will be back in the mail today. Bob . . . ________________________________________________________________________________
Date: Mar 28, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
At 07:45 PM 3/28/2012, you wrote: Bob, Thanks for this drawing. It gives me a general idea of what this thing is - I could almost build one from it... A few more dimensions would be very helpful. (or else I'll have to get out my trig calculator) Or lay it out on a sheet of paper. Agreed, my dimensioning would get me a strong reprimand from the checkers at the last place I did any drawings for production release. That would have been Electro-Mech about 30 years ago! My wish list: 1. Explicit dimensions for length of each piece They're pretty much there . . . 2. A label for each piece. For us antenna ignoramuses (or is that ignorami?) I cannot differentiate between the "antenna" and "ground strut". Do some research on how this antenna is mounted to the the airplane. The ground strut attaches to the tip rib of an all metal airplane. 3. Call-out fastenings and their positions. Are they critical? (e.g. can I substitute a #4 machine-screw & nut instead of a 3/32 dia. aluminum rivet or a #6 screw or a #8, etc?) 4. Some very explicit instructions about how to connect the feed line: a. how to prepare the shield (I'm assuming a coax feed line) b. type of wire terminals (or is it soldered?) c. or can a coax connecter be installed on the antenna 5. How is the structure mounted in the airplane? I hesitate to do highly detailed instructions on Bob Archer's product. The amount of information I do offer is intended as a guide for exploration. The first principal of experimental aircraft is education. If I were to craft such a product, it would indeed feature a captive coax connector. The 'sketches' I offered are intended to get you into the ball-park - not to replicate Bob's product. How did you measure the capacitance? As someone who knows nada about RF, a spec like X pf at Y freq fascinates me.. I have a LRC meter that displays inductance, resistance and capacitance on a digital display. Really useful. http://tinyurl.com/8ygt4mq If that meter had not been at hand, I would have wound a small coil of wire, hooked it across the unknown capacitance, taken a resonance reading, added some known capacitance and taken another reading. You can do this with a 'grid dip' meter. The one I have is about 50 years old http://tinyurl.com/6s875rp but probably the best one ever made. It's good to 1% of reading or better. Suggest you get a sheet of paper and make a full scale drawing of the finished assembly and the component pieces. Strike up some conversation with others here on the List about the various questions of techniques you have cited. I think the dimensions given will bound your options. You're going to become a wingtip VOR antenna expert . . . or at least a guy who has "been there, done that." I think there's enough data there to get you off to a good, low risk start. Bob . . . ________________________________________________________________________________
Date: Mar 28, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
At 06:23 PM 3/28/2012, you wrote: > >Bob, >Did you install the new cap or jhust test it by itself? No, just measured it free and took some dimensions. Found that the .31" and 5.0" dimensions in my earlier sketches were in error. Bob . . . ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
Date: Mar 28, 2012
I apparently mis-understood the purpose of your posting. I thought it was to provide complete instructions & how-to. (and I thought it was a little odd that there were omissions, since your documentation is usually hyper-meticulous) >From what you've provided, one can certainly deduce the remaining dimensions. However I still need help on nomenclature. The ground strut is the horizontal 1.5 in wide piece shown at the bottom of your drawing. Is that correct? I was wondering about how Mr. Archer played into this situation. I, too, have some level of discomfort simply copying his design, and I believe that this antenna is available for < $100. At that price, it hardly pays to do-it-yourself except as an educational exercise. Also, I'm interested in connecting a coax connector directly to the antenna. Do you feel comfortable elaborating on that topic? -Jeff -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Wednesday, March 28, 2012 17:41 Subject: RE: AeroElectric-List: Re: Wingtip VOR antenna . . . a clearer picture At 07:45 PM 3/28/2012, you wrote: Bob, Thanks for this drawing. It gives me a general idea of what this thing is - I could almost build one from it... A few more dimensions would be very helpful. (or else I'll have to get out my trig calculator) Or lay it out on a sheet of paper. Agreed, my dimensioning would get me a strong reprimand from the checkers at the last place I did any drawings for production release. That would have been Electro-Mech about 30 years ago! My wish list: 1. Explicit dimensions for length of each piece They're pretty much there . . . 2. A label for each piece. For us antenna ignoramuses (or is that ignorami?) I cannot differentiate between the "antenna" and "ground strut". Do some research on how this antenna is mounted to the the airplane. The ground strut attaches to the tip rib of an all metal airplane. 3. Call-out fastenings and their positions. Are they critical? (e.g. can I substitute a #4 machine-screw & nut instead of a 3/32 dia. aluminum rivet or a #6 screw or a #8, etc?) 4. Some very explicit instructions about how to connect the feed line: a. how to prepare the shield (I'm assuming a coax feed line) b. type of wire terminals (or is it soldered?) c. or can a coax connecter be installed on the antenna 5. How is the structure mounted in the airplane? I hesitate to do highly detailed instructions on Bob Archer's product. The amount of information I do offer is intended as a guide for exploration. The first principal of experimental aircraft is education. If I were to craft such a product, it would indeed feature a captive coax connector. The 'sketches' I offered are intended to get you into the ball-park - not to replicate Bob's product. How did you measure the capacitance? As someone who knows nada about RF, a spec like X pf at Y freq fascinates me.. I have a LRC meter that displays inductance, resistance and capacitance on a digital display. Really useful. http://tinyurl.com/8ygt4mq If that meter had not been at hand, I would have wound a small coil of wire, hooked it across the unknown capacitance, taken a resonance reading, added some known capacitance and taken another reading. You can do this with a 'grid dip' meter. The one I have is about 50 years old http://tinyurl.com/6s875rp but probably the best one ever made. It's good to 1% of reading or better. Suggest you get a sheet of paper and make a full scale drawing of the finished assembly and the component pieces. Strike up some conversation with others here on the List about the various questions of techniques you have cited. I think the dimensions given will bound your options. You're going to become a wingtip VOR antenna expert . . . or at least a guy who has "been there, done that." I think there's enough data there to get you off to a good, low risk start. Bob . . . ________________________________________________________________________________
From: "Jeff Luckey" <JLuckey(at)pacbell.net>
Subject: Should I Buy an SWR Meter?
Date: Mar 28, 2012
Bob, I'm building an RV7A and I'm into electronics. Should I buy an SWR meter? I know it can help me optimize the antenna systems for my com transmitters and I enjoy geeking-out on things like this. Can an SWR meter help w/ the setup of VOR receivers as well. Can it help me w/ the installation of the Bob Archer antenna for VOR? (I thought that SWR was used primarily for measurements w/ transmitters). Is there a "Big Dummies Guide to Antenna Theory" book available? I'd like to squelch some of my ignorance in this area. (so many questions, so little time.) Thanks, Jeff Luckey Direct Connection Systems www.DCSIT.com 949-645-8832 ________________________________________________________________________________
From: Dave Saylor <dave.saylor.aircrafters(at)gmail.com>
Date: Mar 28, 2012
Subject: Re: HID lighting observations
Well, to date I've sent in a G530 for a screen failure, AFS EFIS for a power supply failure (pretty dramatic), and 3 Garmin 696s, though to be fair, one was an out-of-the-box failure so not possibly due to transients. The 696s were for a bad screen and failure to boot. Since I had to pay for the 530 repair anyway, I opened up the box to peek inside. There was a burnt piece of something laying in the bottom of the chassis. Not good. I let the professionals deal with that one. So I haven't had the best of luck with the "delicate" avionics. I do have suppression diodes on all the contactors, and after the EFIS failure I double checked each one for function and installation. Everything was wired correctly. --Dave Saylor On Tue, Mar 27, 2012 at 9:13 PM, Robert L. Nuckolls, III wrote: > > > I'm still waiting to get into the lab to do some > quantitative testing on some HID light kits. In > the mean time, I've installed a pair on my Kia > mini-van. I've observed the following: > > The lights generate noticeable but not overwhelming > noise in the AM broadcast band during the warm up > phase. About 30 seconds. Don't hear it after the > lamps are warmed up. > > The kits I have generate a strong transient of some > variety onto the bus when first turned on. If I have > the cruise control engaged at the time, it drops off > line. I have to shut the engine off completely to > get the cruise control to reset and wake up. > > This sort of event isn't even watched for under DO-160 > explorations. I'll have to set up on the bench to capture > and quantify this characteristic. > > But in the mean time, be aware that a turn-on transient > MIGHT manifest in erratic behavior of some micro-processor > based electro-whizzies in your airplane. If any such events > are identified and repeatable, I'd like to know about them. > > > Bob . . . > > ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
At 10:45 PM 3/28/2012, you wrote: I apparently mis-understood the purpose of your posting. I thought it was to provide complete instructions & how-to. (and I thought it was a little odd that there were omissions, since your documentation is usually hyper-meticulous) >From what you've provided, one can certainly deduce the remaining dimensions. However I still need help on nomenclature. The ground strut is the horizontal 1.5 in wide piece shown at the bottom of your drawing. Is that correct? Yes. Your position light wires route up the foreward blade of the antenna and then aft to the light fixture location. http://tinyurl.com/7kmfery I was wondering about how Mr. Archer played into this situation. I, too, have some level of discomfort simply copying his design, and I believe that this antenna is available for < $100. At that price, it hardly pays to do-it-yourself except as an educational exercise. You got it! If you were going to build and sell these, I suspect he might be miffed. If you were to design and sell a better one, that's the nature of free market competition. But if you can make this a learning experience, I'm sure he's good with that. Also, I'm interested in connecting a coax connector directly to the antenna. Do you feel comfortable elaborating on that topic? http://tinyurl.com/7k8nryk http://tinyurl.com/73jowsp Bob . . . ________________________________________________________________________________
From: "Thomas Johnson" <trj03(at)ca.rr.com>
Subject: re: HID lighting observations
Date: Mar 28, 2012
> But in the mean time, be aware that a turn-on transient > MIGHT manifest in erratic behavior of some micro-processor > based electro-whizzies in your airplane. If any such events > are identified and repeatable, I'd like to know about them. When I upgraded from halogen to HID lights several years ago I had a problem with this. My own design PIC based wig-wag controller no longer worked at all. I found that the HID lights had a huge inrush current each time they switched on. I tried a few fixes and got the best results by running the HID power and ground wires together through a 1/2=9D dia X 1=9D long ferrite core. Using two in series worked even better. The first time I tested the ferrites I used a split half type because it is easier to pop on and off in different locations. While I was watching the scope I noticed a new, fairly loud clicking sound coming from the HID controller area. It turned out to be the split ferrite half's snapping together each time power came on. That is some serious energy transfer! Tom Johnson ________________________________________________________________________________
Date: Mar 29, 2012
From: paul wilson <pwmac(at)sisna.com>
Subject: Re SWR Meter?
Some input I use my meter to check from time to time to verify all is well. This link has info on the meters <http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579>http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 The one I use is an MFJ-862 It has 2 needles for Forward and Reflected and will read watts for both. This is a low price unit, definately not a high, but had OK reviews. I have no idea if one can still buy it? PaulW ________________________________________________________________________________
Date: Mar 29, 2012
From: Harley <harley(at)AgelessWings.com>
Subject: Re: Re SWR Meter?
Paul... Yep, still available...(a little more than you probably paid for it): www.mfjenterprises.com/Product.php?productid=MFJ-862 Harley > I use my meter to check from time to time to verify all is well. > This link has info on the meters > http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 > > > The one I use is an MFJ-862 It has 2 needles for Forward and > Reflected and will read watts for both. This is a low price > unit, definately not a high, but had OK reviews. I have no idea > if one can still buy it? > PaulW ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Re SWR Meter?
At 08:07 AM 3/29/2012, you wrote: >Some input > >I use my meter to check from time to time to verify all is well. >This link has info on the meters ><http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579>http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 > > >The one I use is an MFJ-862 It has 2 needles for Forward and >Reflected and will read watts for both. This is a low price unit, >definately not a high, but had OK reviews. I have no idea if one can >still buy it? >PaulW I found one offered here: http://tinyurl.com/6m8zrru Given it's rather complex set of features (rear panel calibration pots) and low price ($16) I'm wondering if they don't have an inventory that they'd REALLY like to get rid of. MFJ is usually pretty good stuff and this item does claim to cover VHF but I'm not convinced that this is a good buy. I'm tempted to order one at this price just to take it apart for a looksee . . . If you'd like to compare your personal item with a set of BIRD measurements, I'd be pleased to do the work. I'll pay return postage. Bob . . . ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Re SWR Meter?
OOPS! Stubbed my toe on that one. The price I latched onto was for the DC power supply, the instrument itself sells for about $70. ----------------------------------------------------- At 08:07 AM 3/29/2012, you wrote: Some input I use my meter to check from time to time to verify all is well. This link has info on the meters http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 The one I use is an MFJ-862 It has 2 needles for Forward and Reflected and will read watts for both. This is a low price unit, definately not a high, but had OK reviews. I have no idea if one can still buy it? PaulW I found one offered here: http://tinyurl.com/6m8zrru Given it's rather complex set of features (rear panel calibration pots) and low price ($16) I'm wondering if they don't have an inventory that they'd REALLY like to get rid of. MFJ is usually pretty good stuff and this item does claim to cover VHF but I'm not convinced that this is a good buy. I'm tempted to order one at this price just to take it apart for a looksee . . . If you'd like to compare your personal item with a set of BIRD measurements, I'd be pleased to do the work. I'll pay return postage. Bob . . . ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Should I Buy an SWR Meter?
At 10:52 PM 3/28/2012, you wrote: Bob, I=92m building an RV7A and I=92m into electronics. Should I buy an SWR meter? I know it can help me optimize the antenna systems for my com transmitters and I enjoy geeking-out on things like this. Just how MUCH do you enjoy it? I have two shops and a large inventory of tools and materials . . . MOST of which has not been touched in months to perhaps decades. NEED? Obviously small. Potential for addressing a design goal? Obviously great . . . but every project usually requires some purchases . . . of materials and the occasional tool. Any borrow/buy advice offered by any of us will be polluted with personal perceptions of need/usefulness. I'd suggest that it comes down to expendable cash. Suppose you DID run off and spend $100 on a nice VHF SWR instrument. Suppose further that 10 years from now you find that you've used the device perhaps a few times at the outset but not once in the last 8 years? How would you judge your return on investment then? Can an SWR meter help w/ the setup of VOR receivers as well. Can it help me w/ the installation of the Bob Archer antenna for VOR? (I thought that SWR was used primarily for measurements w/ transmitters). It is true that ALL such instruments need to excite the antenna or feed line at the frequency of interest. But that excitation can come from a variety of sources depending on the sensitivity of the instrument. SWR meters like the Red Dot device we've discussed recently need a watt or so. Antenna analyzers like the MJF-259 (and close cousins) have internal signal generators to supply the necessary excitation. In the case of your VOR antenna, I'd suggest using a hand held and some device like the Red Dot SWR meter. You can tune for optimum performance at the lowest COMM frequency which is at the upper end of the VOR band. This would be great verification of gross performance and more than adequate for VOR reception. Is there a =93Big Dummies Guide to Antenna Theory=94 book available? I=92d like to squelch some of my ignorance in this area. Hmmmm . . . the short answer is YES. But the constellation of antenna styles and design goals is . . . shall we say . . . HUGE? I have antenna books on the shelves wherein 98% of the pages offered nothing useful to my professional activities . . . but the 2% of useful stuff was very helpful. I'm reluctant to suggest specific titles. Do some 'net searches on VHF antennas and SWR. Look over the construction articles, techniques for adjusting, etc. You will probably learn more that is useful to your aviation interests by playing with antennas in the shop that are also destined to go on your airplane. Remember this picture? I don't even recall what we were discussing on the List but I did this little 1/4-Comm antenna setup on a sheet of copper clad right here in the shop. But I'm confident that we learned or demonstrated something interesting or useful. Emacs! Then there is the constellation of grey-matter here on the list that is accessible to you. I've been gathering the stuff together to do a back-yard-antenna-range evaluation of performance for BALUN versus NOBALUN. During this exercise I'll explore the notion that a Pawsy stub does behave like transmission line with some small dielectric effects for velocity factor and should be mechanically shortened to center it up at the frequency of interest. I'll document that experiment and post it to AeroElectric.com (so many questions, so little time=85) You got that right. Education is expensive. It goes far beyond the cost of tuition, tools and materials. The big expense is $time$. Hence the notion that participation in activities like the AeroElectric-List can and should offer significant reduction in the expenditure of $time$. This applies to both academic science and practical arts of our shared interests. Buy an SWR meter? You bet! But with the caveats I've cited above tucked into your hip pocket. Bob . . . ________________________________________________________________________________
Date: Mar 29, 2012
From: paul wilson <pwmac(at)sisna.com>
Subject: Re: Re SWR Meter?
MFJ-862 Reviews http://www.eham.net/reviews/detail/4367 Cannot remember what I paid back when. Withouit a long search looks like $65-70 is the going price I bought it to cover my mobiles 144/220/440 MGHz and of course that includes the aviation band. Ok for the 5 watt as well as my 50 watt units. PaulW ========= At 08:12 AM 3/29/2012, you wrote: >At 08:07 AM 3/29/2012, you wrote: >>Some input >> >>I use my meter to check from time to time to verify all is well. >>This link has info on the meters >><http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579>http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 >> >> >>The one I use is an MFJ-862 It has 2 needles for Forward and >>Reflected and will read watts for both. This is a low price unit, >>definately not a high, but had OK reviews. I have no idea if one >>can still buy it? >>PaulW > > I found one offered here: > >http://tinyurl.com/6m8zrru > > Given it's rather complex set of features > (rear panel calibration pots) and low > price ($16) I'm wondering if they don't > have an inventory that they'd REALLY like > to get rid of. > > MFJ is usually pretty good stuff and this > item does claim to cover VHF but I'm not > convinced that this is a good buy. I'm > tempted to order one at this price just to > take it apart for a looksee . . . > > If you'd like to compare your personal item > with a set of BIRD measurements, I'd be pleased > to do the work. I'll pay return postage. > > Bob . . . > > ><http://www.matronics.com/Navigator?AeroElectric-List>http://www.matronics.com/Navigator?AeroElectric-List ><http://www.matronics.com/contribution>http://www.matronics.com/contribution > ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: re: HID lighting observations
>When I upgraded from halogen to HID lights >several years ago I had a problem with this. My >own design PIC based wig-wag controller no longer worked at all. Did the PIC wander off into the weeds and lock up? > I found that the HID lights had a huge inrush > current each time they switched on. I tried a > few fixes and got the best results by running > the HID power and ground wires together through > a 1/2 dia X 1 long ferrite core. Using two in series worked even better. Ferrites are sometimes useful for repetitive events like noise but less useful for transient events like inrush currents. I'll try to get some transient/running captures on the two HID units I have here. I could probably get some data on the ones in the car too if I can find my current probes for the 'scope. I'm still un-packing move boxes. > >The first time I tested the ferrites I used a >split half type because it is easier to pop on >and off in different locations. While I was >watching the scope I noticed a new, fairly loud >clicking sound coming from the HID controller >area. It turned out to be the split ferrite >half's snapping together each time power came >on. That is some serious energy transfer! I'm reminded of some strange noises I used to hear periodically up in the ceiling structure of a new building put up by my employer. Out in the shops I used to hear a noise that seemed to come from the conduits. I later came to understand that this was the convulsive thrashing of the ac wiring that went out to large motors at the back of the building. Every time a big motor started up, induced repulsion of the adjacent wires in the conduit made noises. Good data Tom. Bob . . . ________________________________________________________________________________
From: "Miskelly, Francis G" <f.miskelly(at)imperial.ac.uk>
Subject: Re SWR Meter?
Date: Mar 29, 2012
Does the MFG-862 cover the aviation band (108-116 MHz) - Frank ________________________________________ From: owner-aeroelectric-list-server(at)matronics.com [owner-aeroelectric-list-server(at)matronics.com] on behalf of paul wilson [pwmac(at)sisna.com] Sent: 29 March 2012 17:05 Subject: Re: AeroElectric-List: Re SWR Meter? MFJ-862 Reviews http://www.eham.net/reviews/detail/4367 Cannot remember what I paid back when. Withouit a long search looks like $65-70 is the going price I bought it to cover my mobiles 144/220/440 MGHz and of course that includes the aviation band. Ok for the 5 watt as well as my 50 watt units. PaulW ========= At 08:12 AM 3/29/2012, you wrote: At 08:07 AM 3/29/2012, you wrote: Some input I use my meter to check from time to time to verify all is well. This link has info on the meters http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd4579 The one I use is an MFJ-862 It has 2 needles for Forward and Reflected and will read watts for both. This is a low price unit, definately not a high, but had OK reviews. I have no idea if one can still buy it? PaulW I found one offered here: http://tinyurl.com/6m8zrru Given it's rather complex set of features (rear panel calibration pots) and low price ($16) I'm wondering if they don't have an inventory that they'd REALLY like to get rid of. MFJ is usually pretty good stuff and this item does claim to cover VHF but I'm not convinced that this is a good buy. I'm tempted to order one at this price just to take it apart for a looksee . . . If you'd like to compare your personal item with a set of BIRD measurements, I'd be pleased to do the work. I'll pay return postage. Bob . . . AeroElectric-List Email Forum - http://www.matronics.com/Navigator?AeroElectric-List - MATRONICS WEB FORUMS - http://forums.matronics.com - List Contribution Web Site - -Matt Dralle, List Admin. http://www.matronics.com/contribution ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re SWR Meter?
At 12:10 PM 3/29/2012, you wrote: > > > >Does the MFG-862 cover the aviation band (108-116 MHz) > - Frank Probably not guaranteed to published specifications but still useful. There was some discussion a few weeks back about suitability of the LO Band (3-30 Mhz) devices being used at VHF. Typically devices like this: Emacs! These do perform as advertised in the 3-30 Mhz range but tend to run off into the weeds at 4x the top design frequency. On the other hand, the MFJ862 used at 108-135 (full range aviation) is still at 75% of lower end of 144 ham band. Maybe not quite as accurate with respect to absolute readings but still a good indicator of performance and useful for finding frequency of lowest SWR. For about the same $ you can pick up one of these http://tinyurl.com/6pjbckd which is designed for our particular frequencies of interest. On the other hand, there are some DIY options too. Take a look at this article: http://tinyurl.com/7dmupav This DIY project is tailored to the 2.5 GHz range for WiFi work but the same technique can be easily adapted to lower frequencies. Here's another one. http://tinyurl.com/83e5u2q All it takes is $time$ and patience . . . but it can be fun . . . Bob . . . ________________________________________________________________________________
Subject: Re: Wingtip VOR antenna . . . a clearer picture
From: Mark Harris <harrismarkr(at)hotmail.com>
Date: Mar 29, 2012
Bob Ok now I have a problem ,at the weekend I made the VOR antenna to the dimensions previously discussed/aero electrics book I believe,these are very different to the ones shown on the previous link ,which should I use? Thanks Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 28 Mar 2012, at 21:47, "Robert L. Nuckolls, III" wrote: > > Thanks to List member van Saten, we've got some > better details for a DIY wingtip VOR antenna. See: > > http://tinyurl.com/6v5gvhx > > It seems that the sketch I was working from years ago > was either not up to date or in error. > > The insulator turns out to be either glass or cloth > filled phenolic, 0.062 inches thick. The measured > value of an off-the-shelf gamma-match capacitor is > 34 pf @ 1 KHz. > > I think the data above will get the builder closer to > a workable example of this particular antenna. > > Thanks Don! Your antenna will be back in the mail today. > > > Bob . . . > > > > > ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Wingtip VOR antenna . . . a clearer picture
At 01:56 PM 3/29/2012, you wrote: > >Bob > >Ok now I have a problem ,at the weekend I made the VOR antenna to >the dimensions previously discussed/aero electrics book I >believe,these are very different to the ones shown on the previous >link ,which should I use? The dimensions I published originally were parroted from an article in an Van's Air Force publication . . . probably 10-12 years ago. It was not until I put my hands on a 'real' antenna (thanks to Don S) did I have an opportunity to check/update the VAF drawings. Are you flying or close to flying the earlier 'version'? It would be interesting to do a seat-of-the-pants observation on differences in performance. You could build up a 'new' antenna but keep it in reserve until you've flown the 'old' one. I'm thinking that it would be difficult to tell much difference from the pilot's seat but you might perhaps dispel that notion for me. The question that started this thread involved procurement of 1/32" Bakelite . . . while in fact, 1/16" Phenolic is the 'real' material. It was something of a windfall that other discrepancies were discovered. Sorry 'bout that. Bob . . . ________________________________________________________________________________
From: "Miskelly, Francis G" <f.miskelly(at)imperial.ac.uk>
Subject: Re SWR Meter?
Date: Mar 29, 2012
Many thanks Bob. That's extremely helpful. You're a true gentleman! - Frank ________________________________________ From: owner-aeroelectric-list-server(at)matronics.com [owner-aeroelectric-list -server(at)matronics.com] on behalf of Robert L. Nuckolls, III [nuckolls.bob(at)a eroelectric.com] Sent: 29 March 2012 19:29 Subject: RE: AeroElectric-List: Re SWR Meter? At 12:10 PM 3/29/2012, you wrote: imperial.ac.uk> Does the MFG-862 cover the aviation band (108-116 MHz) - Frank Probably not guaranteed to published specifications but still useful. There was some discussion a few weeks back about suitability of the LO Band (3-30 Mhz) devices being used at VHF. Typically devices like this: [Emacs!] These do perform as advertised in the 3-30 Mhz range but tend to run off into the weeds at 4x the top design frequency. On the other hand, the MFJ862 used at 108-135 (full range aviation) is still at 75% of lower end of 144 ham band. Maybe not quite as accurate with respect to absolute readings but still a good indicator of performance and useful for finding frequency of lowest SWR. For about the same $ you can pick up one of these http://tinyurl.com/6pjbckd which is designed for our particular frequencies of interest. On the other hand, there are some DIY options too. Take a look at this article: http://tinyurl.com/7dmupav This DIY project is tailored to the 2.5 GHz range for WiFi work but the same technique can be easily adapted to lower frequencies. Here's another one. http://tinyurl.com/83e5u2q All it takes is $time$ and patience . . . but it can be fun . . . Bob . . . ________________________________________________________________________________
From: Dave Saylor <dave.saylor.aircrafters(at)gmail.com>
Date: Mar 29, 2012
Subject: Uneven dipole elements
Bob, We managed to chop about 3 inches off the end of a dipole comm antenna. Would that have any appreciable effect on performance? --Dave Saylor ________________________________________________________________________________
Date: Mar 29, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Uneven dipole elements
At 05:30 PM 3/29/2012, you wrote: > > >Bob, > >We managed to chop about 3 inches off the end of a dipole comm >antenna. Would that have any appreciable effect on performance? Sure, but if I were to give you a 'number' . . . it wouldn't have much practical meaning. Is this an internal antenna? Can't you splice it back on? Bob . . . ________________________________________________________________________________
From: "Thomas Johnson" <trj03(at)ca.rr.com>
Subject: Re: re: HID lighting observations
Date: Mar 29, 2012
> Did the PIC wander off into the weeds and lock up? Usually it would make one and a half wig-wags and then lock up, requiring a power cycle to recover. At that time I was not utilizing the PIC Brown-out Reset (BOR) feature. I=99ll bet that would have given me a clean reset. Once I knocked the inrush spike down a little I never saw the problem again. I had never needed to fix an inrush issue before and I assumed that a quick internet search would yield a handful of simple solutions. What I found is that high inrush current is a growing problem for modern electronics, and if it=99s not dealt with in the original design it can be real hard to fix later. The neatest solution I read about (but never got around to trying) is to ramp up voltage to the HID controller slowly. I was already using a P-FET to switch power on/off so it didn=99t sound too difficult to do that. Tom Johnson ________________________________________________________________________________
From: Dave Saylor <dave.saylor.aircrafters(at)gmail.com>
Date: Mar 29, 2012
Subject: Re: Uneven dipole elements
>>Can't you splice it back on?<< Short answer--no. We had to lop the tip off a vertical stab to make room for more rudder horn on a Lancair ES. I didn't stop to think about an internal antenna. I shoulda. On further inspection, the antenna seems to have three elements. Two run up each side of the Vstab trailing edge, aft of the stern post. They're embedded in the fiberglass and are nearly equal in length. The element that was cut off is 8" forward of the Vstab trailing edge. I can't tell exactly how the three segments are connected. The aft-most two elements are visible through the fiberglass when the rudder is removed. I can see a lot of the cut element using a boroscope inside the Vstab. Would I hurt the radio to try transmitting and receiving? If this isn't easy to fix, we have the option of installing a belly-mounted replacement antenna using a spray-on ground plane. --Dave Saylor On Thu, Mar 29, 2012 at 7:45 PM, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > nuckolls.bob(at)aeroelectric.com**> > > > At 05:30 PM 3/29/2012, you wrote: > >> dave.saylor.aircrafters(at)**gmail.com > >> >> Bob, >> >> We managed to chop about 3 inches off the end of a dipole comm >> antenna. Would that have any appreciable effect on performance? >> > > Sure, but if I were to give you a 'number' . . . it wouldn't > have much practical meaning. Is this an internal antenna? > Can't you splice it back on? > > > Bob . . . > > ________________________________________________________________________________
Date: Mar 30, 2012
From: Glen Matejcek <aerobubba(at)earthlink.net>
Subject: expanded horizons
Hi Bob- Just in case you're not familiar, the EAA has a series of shorts available online called Hints for Homebuilders. It is quite a collection of how-to's. I don't know what the implications for intellectual property or aero politics would be if one participated there, but they certainly have the venue aspect nailed. FYI- Glen Matejcek ________________________________________________________________________________
Subject: Antennae materials
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Mar 30, 2012
First a word on the performance of electronic materials: We all know that materials have a DC bulk resistivity that is a measure of how they transfer electrons through the material. But for high frequency applications another characteristic is critical: Most dielectric materials are made of molecules with polar configurations that is, their constituent molecules have shapes where their atoms tend to be non-symmetrically attached. Thus these molecules will twist to try to align with electromagnetic fields imposed on them. A microwave oven is a good example. Water is somewhat bipolar, and an imposed electromagnetic wave causes the water molecule to change its orientation every cycle, thus producing mechanical heating--and cooking your food. If you were trying to build a PCB for 2.45 GHz, the common household microwave-oven frequency, water, or anything that absorbed water, or anything that was somewhat molecularly-similar to water would be a poor choice. The materials needed for antennas and PCBs have many structural and environmental constraints (strong enough, reasonably high temperature, no asbestos, waterproof, flame retardant, machinable, etc.) but are critically restrained by the requirement that the molecules making up the material not oscillate much at the frequencies to be used. The molecular shape (to over-simplify), and how well they are locked into the material is the key. This usually limits the commercial material selection to thermosetting materials like phenolic and Bakelite or high-pressure thermosetting resins like epoxies. When faced with building PCB or antenna supports or other high-frequency electronic parts, many people rely on some very old and august information. Much of this was compiled over half-a-century ago, and while one can appreciate its particular no-nonsense clarity, it misses all the recent advances. This has many negative affects: Poor material selections drive production prices up and structural dependability down. Time is wasted pursuing arcane magic materials invented decades ago and now largely unobtainablewhile simple to use, cheap and easily-sourced materials are available. See: Good History! Tables of Dielectric Materials. Wright Laboratories, Feb 1944 http://www.dtic.mil/cgi-bin/GetTRDoc?AD=ADA288986 Here is a good and much more recent description of the choice of materials. http://www.speedingedge.com/PDF-Files/tutorial.pdf The recent discussion of searches for micarta, paper phenolic and Bakelite is a case in point. While these materials had their day, modern designs are almost entirely PCB materials like FR-4, (which almost universally replaced G10 and most other G- and FR- materials). So thats the story: Abandon your search for half-century old materials and use FR-4 glass epoxy. MSC Hardware is a great source for machining stock, but if you have a PCB fabricating house nearby, ask to grab some from their dumpster (thats how I do it). -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369609#369609 ________________________________________________________________________________
Date: Mar 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Antennae materials
> >So thats the story: Abandon your search for >half-century old materials and use FR-4 glass >epoxy. MSC Hardware is a great source for >machining stock, but if you have a PCB >fabricating house nearby, ask to grab some from >their dumpster (thats how I do it). Well stated but with one caveat. The dielectric constant for FR-4 versus the filled phenolic may be different. Probably is . . . but haven't had time to research/test it. This was the driving thought for getting my hands on a production example of the subject antenna. Direct measurement of the gamma-match capacitor fabricated from production parts yielded a value of 34 pF. This becomes the benchmark for substitution of materials. The choices are many but in this instance, they are not an apples-for-apples substitution. I'm considering the use of 1/32" copper clad for fabrication of a similar antenna. The copper lends itself to soldered joints (gas tight for centuries). The double-sided cladding offers an opportunity to craft the gamma-match strut from a single piece of FR-4 with copper bonded to both sides. Just another interesting project for the future . . . perhaps we can get to it before VOR goes the way of A-N Range stations. Bob . . . ________________________________________________________________________________
Date: Mar 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Uneven dipole elements
At 12:39 AM 3/30/2012, you wrote: >>Can't you splice it back on?<< Short answer--no. We had to lop the tip off a vertical stab to make room for more rudder horn on a Lancair ES. I didn't stop to think about an internal antenna. I shoulda. If the structure needed to be shortened . . . and the antenna is embedded in structure, would it have made any difference? On further inspection, the antenna seems to have three elements. Two run up each side of the Vstab trailing edge, aft of the stern post. They're embedded in the fiberglass and are nearly equal in length. Do you have any documentation on how this antenna was installed? I'm having trouble putting my gray-matter around your description. The element that was cut off is 8" forward of the Vstab trailing edge. I can't tell exactly how the three segments are connected. The aft-most two elements are visible through the fiberglass when the rudder is removed. I can see a lot of the cut element using a boroscope inside the Vstab. Would I hurt the radio to try transmitting and receiving? If this isn't easy to fix, we have the option of installing a belly-mounted replacement antenna using a spray-on ground plane. Get an SWR meter and see how bad the crippled antenna really is. Spray-on ground planes are like using Kleenex for wing fabric. Metallic radials on inside of skin is both the best and least we know how to do. Bob . . . ________________________________________________________________________________
From: "Mike Wynn" <wynaire(at)citlink.net>
Subject: Re: Uneven dipole elements
Date: Mar 30, 2012
Bob, This ant design sounds like the one I spoke about. BTW: I found the diagrams and factory instructions, finally. Will scan and send today. Maybe it will help Dave S. with decision. GL! Mike Wynn Moab, UT ********** ----- Original Message ----- From: Dave Saylor To: aeroelectric-list(at)matronics.com Sent: Thursday, March 29, 2012 11:39 PM Subject: Re: AeroElectric-List: Uneven dipole elements >>Can't you splice it back on?<< Short answer--no. We had to lop the tip off a vertical stab to make room for more rudder horn on a Lancair ES.=C2 I didn't stop to think about an internal antenna.=C2 I shoulda. On further inspection, the antenna seems to have three elements.=C2 Two run up each side of the Vstab trailing edge, aft of the stern post.=C2 They're embedded in the fiberglass and are nearly equal in length. The element that was cut off is 8" forward of the Vstab trailing edge.=C2 I can't tell exactly how the three segments are connected.=C2 The aft-most two elements are visible through the fiberglass when the rudder is removed.=C2 I can see a lot of the cut element using a boroscope inside the Vstab. Would I hurt the radio to try transmitting and receiving?=C2 If this isn't easy to fix, we have the option of installing a belly-mounted replacement antenna using a spray-on ground plane. --Dave Saylor On Thu, Mar 29, 2012 at 7:45 PM, Robert L. Nuckolls, III wrote: At 05:30 PM 3/29/2012, you wrote: Bob, We managed to chop about 3 inches off the end of a dipole comm antenna. =C2 Would that have any appreciable effect on performance? =C2 Sure, but if I were to give you a 'number' . . . it wouldn't =C2 have much practical meaning. Is this an internal antenna? =C2 Can't you splice it back on? =C2 Bob . . . - ric-List" target="_blank">http://www.matronics.com/Navigator?AeroElectric-List MS - k">http://forums.matronics.com e - =C2 =C2 =C2 =C2 =C2 -Matt Dralle, List Admin. t="_blank">http://www.matronics.com/contribution ________________________________________________________________________________
From: Dave Saylor <dave.saylor.aircrafters(at)gmail.com>
Date: Mar 30, 2012
Subject: Re: Uneven dipole elements
Thanks! I'd like to know what this antenna looks like. Off topic: It's on an as-yet unfinished Lancair ES with a 15-year old panel. It had a huge FMS-type display (that won't boot up) called a Avro-Tec FMP 300. The antenna in question is switched by a Comant gizmo between two comms. We stumbled back-asswards into an antenna engineer who works for L3 across the street from us. His hobby is helping ham operators build antennas, and he should be here Saturday to do a "sweep"...whatever that is. --Dave Saylor On Fri, Mar 30, 2012 at 10:45 AM, Mike Wynn wrote: > ** > Bob, > This ant design sounds like the one I spoke about. BTW: I found the > diagrams and factory instructions, finally. Will scan and send today. May be > it will help Dave S. with decision. GL! > Mike Wynn > Moab, UT > ********** > > ----- Original Message ----- > *From:* Dave Saylor > *To:* aeroelectric-list(at)matronics.com > *Sent:* Thursday, March 29, 2012 11:39 PM > *Subject:* Re: AeroElectric-List: Uneven dipole elements > > >>Can't you splice it back on?<< > > Short answer--no. > > We had to lop the tip off a vertical stab to make room for more rudder > horn on a Lancair ES.=C3=82 I didn't stop to think about an internal ant enna.=C3=82 > I shoulda. > > On further inspection, the antenna seems to have three elements.=C3=82 T wo run > up each side of the Vstab trailing edge, aft of the stern post.=C3=82 Th ey're > embedded in the fiberglass and are nearly equal in length. > > The element that was cut off is 8" forward of the Vstab trailing edge.=C3 =82 I > can't tell exactly how the three segments are connected.=C3=82 The aft-m ost two > elements are visible through the fiberglass when the rudder is removed. =C3=82 I > can see a lot of the cut element using a boroscope inside the Vstab. > > Would I hurt the radio to try transmitting and receiving?=C3=82 If this isn't > easy to fix, we have the option of installing a belly-mounted replacement > antenna using a spray-on ground plane. > > --Dave Saylor > > > On Thu, Mar 29, 2012 at 7:45 PM, Robert L. Nuckolls, III < > nuckolls.bob(at)aeroelectric.com> wrote: > >> nuckolls.bob(at)aeroelectric.com**> >> >> >> At 05:30 PM 3/29/2012, you wrote: >> >>> dave.saylor.aircrafters(at)**gmail.com > >>> >>> Bob, >>> >>> We managed to chop about 3 inches off the end of a dipole comm >>> antenna. =C3=82 Would that have any appreciable effect on performance? >>> >> >> =C3=82 Sure, but if I were to give you a 'number' . . . it wouldn't >> =C3=82 have much practical meaning. Is this an internal antenna? >> =C3=82 Can't you splice it back on? >> >> >> =C3=82 Bob . . . >> >> ====**=================== ===========**= >> - >> ric-List" target="_blank">http://www.matronics.com/** >> Navigator?AeroElectric-List >> ====**=================== ===========**= >> MS - >> k">http://forums.matronics.com >> ====**=====**= >> e - >> =C3=82 =C3=82 =C3=82 =C3=82 =C3=82 -Matt Dralle, List Admin. >> t="_blank">http://www.matronics.com/**contribution >> ====**=================== ===========**= >> >> >> >> > * > > href="http://www.matronics.com/Navigator?AeroElectric-List">http://www. matronics.com/Navigator?AeroElectric-List > href="http://forums.matronics.com">http://forums.matronics.com > href="http://www.matronics.com/contribution">http://www.matronics.com/c * > > * > =========== =========== =========== =========== > * > > ________________________________________________________________________________
Date: Mar 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Uneven dipole elements
At 12:45 PM 3/30/2012, you wrote: >Bob, >This ant design sounds like the one I spoke about. BTW: I found the >diagrams and factory instructions, finally. Will scan and send >today. Maybe it will help Dave S. with decision. GL! >Mike Wynn >Moab, UT Thank you! I'll post it to the reference documents folder on the website too. Bob . . . ________________________________________________________________________________
Date: Mar 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Uneven dipole elements
At 01:12 PM 3/30/2012, you wrote: >Thanks!=C2 I'd like to know what this antenna looks like. > >Off topic:=C2 It's on an as-yet unfinished >Lancair ES with a 15-year old panel.=C2 It had a >huge FMS-type display (that won't boot up) called a Avro-Tec FMP 300. > >The antenna in question is switched by a Comant gizmo between two comms. > >We stumbled back-asswards into an antenna >engineer who works for L3 across the street from >us.=C2 His hobby is helping ham operators build >antennas, and he should be here Saturday to do a "sweep"...whatever that is. A 'sweep' is done with a supper-whizzy network analyzer usually fitted the a sweep generator and graphical display for the output of the analyzer. You get pictures like this in seconds Emacs! Us poor guys use an SWR meter and variable frequency energy source to step through the frequencies of interest and record data. That data is then massaged like our algebra teachers taught us. After you've done it a few dozen times, any notions of it being a 'sweep' are replace the realization that it's really a 'plod'. It will be interesting to see what he finds. Take pictures of his test setup and data to share with us if you can. Bob . . . ________________________________________________________________________________
Subject: Re: HID lighting observations
From: "Brantel" <brianchesteen(at)gmail.com>
Date: Mar 30, 2012
The newer HID ballast have circuitry to limit the inrush current. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369637#369637 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re SWR Meter?
Date: Mar 30, 2012
I've used MFJ for years with no problems... HF and VHF. Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Harley Sent: March 29, 2012 11:39 AM Subject: Re: AeroElectric-List: Re SWR Meter? Paul... Yep, still available...(a little more than you probably paid for it): www.mfjenterprises.com/Product.php?productid=MFJ-862 Harley I use my meter to check from time to time to verify all is well. This link has info on the meters http://www.eham.net/reviews/products/40?ehamsid=a9efc7e8e58a376ce24c0118effd 4579 The one I use is an MFJ-862 It has 2 needles for Forward and Reflected and will read watts for both. This is a low price unit, definately not a high, but had OK reviews. I have no idea if one can still buy it? PaulW ________________________________________________________________________________
From: Michael Ashura <ashuramj(at)hotmail.com>
Subject: LED WigWag with B&C SSF-1
Date: Mar 30, 2012
Bob, can I wire two LED landing and taxi lights per Page 3.0 (Ref DE 12/15/11) but using a single switch (already installed and labeled in unflown RV-6) as shown on Page 3.0 from 2003? Thank you ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Uneven dipole elements
Date: Mar 30, 2012
I'm wondering if it is now operating like a modified Windom antenna (not straight at centre and different length elements). I also would like to know if it is vertical or horizontal Noel -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: March 30, 2012 12:16 AM Subject: Re: AeroElectric-List: Uneven dipole elements --> At 05:30 PM 3/29/2012, you wrote: > > >Bob, > >We managed to chop about 3 inches off the end of a dipole comm antenna. >Would that have any appreciable effect on performance? Sure, but if I were to give you a 'number' . . . it wouldn't have much practical meaning. Is this an internal antenna? Can't you splice it back on? Bob . . . ________________________________________________________________________________
From: Michael Ashura <ashuramj(at)hotmail.com>
Subject: Correction
Date: Mar 30, 2012
Previous post should read: (Revision -D- 12/15/11) ________________________________________________________________________________
Date: Mar 30, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Uneven dipole elements
At 06:46 PM 3/30/2012, you wrote: > >I'm wondering if it is now operating like a modified Windom antenna (not >straight at centre and different length elements). I also would like to >know if it is vertical or horizontal This would be a vertically polarized antenna and appears to be 1/2 wavelength. Is there enough 'bulk' at the coax end to house a small toroid transformer? There's another 1/2-wave kid on the block which is actually a center-fed dipole with the feedline running up the middle of the lower half of the dipole. It's marketed as the Air Whip at http://miracleantenna.com/shop-products/aviation/42 Emacs! The black box houses the common-mode choke which de-couples the feed line from the high-voltage end of the dipole thusly. http://tinyurl.com/78ph8nz http://tinyurl.com/6ul4o6f Waaayyy back when, there was a brief brush with tiny toroids to match coax feedlines to center fed dipoles the cores they used were very low power handling . . . hence good for receive only. The Antenna Dynamics product has the look and 'smell' of a similar product. By the way, the reason it's not 44" (half wave in free space) long is because the lower 1/4 wave is in coax which is shortened to about 14" by the coax velocity factor. Miracle Antenna is a newer kid on the block and gets very good reviews from their whole customer base which includes amateur radio and SWL applications. Dave, is there any chance you can get the remnants of the old antenna out? Putting one of these in it's place would be a prudent move. If that's not practical/possible, then splicing an extension on the upper end to replace the cut off length would be helpful . . . even if it lays off at right angles to the antenna. This would serve as an extension moving back toward 1/4 wave for the upper element and/or 'capacity' hat to load the shortened antenna thus making it look electrically like a quarter wave. Your antenna guy will know all about this and will be able to help you with the patch. Bob . . . ________________________________________________________________________________
From: Dave Saylor <dave.saylor.aircrafters(at)gmail.com>
Date: Mar 30, 2012
Subject: Re: Uneven dipole elements
We found a diagram of what we think the antenna looks like. I'll post of a picture of it next week at the latest. It's a slanted-N shape similar to an Archer. Earlier I described equal-length parallel elements. Turns out they're carbon reinforcements that aren't part of the antenna. I'll show them in the picture when I post it. I mistook them as part of the antenna because I was using a "wire sniffer" to find the elements. I had the transmitter attached to the end we'd cut off, and it was making the carbon strips, which aren't connected to the antenna in any way I can see, display to the receiver wand as conductors. Thanks to everyone for all the input. We'll get this figured out. I think if I have to I can add a few perpendicular inches to the shortened end. --Dave Saylor On Fri, Mar 30, 2012 at 9:36 PM, Robert L. Nuckolls, III < nuckolls.bob(at)aeroelectric.com> wrote: > At 06:46 PM 3/30/2012, you wrote: > > noelloveys(at)yahoo.ca> > > I'm wondering if it is now operating like a modified Windom antenna (not > straight at centre and different length elements). I also would like to > know if it is vertical or horizontal > > > This would be a vertically polarized antenna and > appears to be 1/2 wavelength. Is there enough > 'bulk' at the coax end to house a small toroid > transformer? > > There's another 1/2-wave kid on the block which > is actually a center-fed dipole with the feedline > running up the middle of the lower half of the > dipole. It's marketed as the Air Whip at > > http://miracleantenna.com/shop-products/aviation/42 > > [image: Emacs!] > > The black box houses the common-mode choke which > de-couples the feed line from the high-voltage > end of the dipole thusly. > > http://tinyurl.com/78ph8nz > > http://tinyurl.com/6ul4o6f > > Waaayyy back when, there was a brief brush with > tiny toroids to match coax feedlines to center fed > dipoles the cores they used were very low > power handling . . . hence good for receive only. > > The Antenna Dynamics product has the look and 'smell' > of a similar product. By the way, the reason it's > not 44" (half wave in free space) long is because > the lower 1/4 wave is in coax which is shortened > to about 14" by the coax velocity factor. > > Miracle Antenna is a newer kid on the block > and gets very good reviews from their whole > customer base which includes amateur radio and > SWL applications. > > Dave, is there any chance you can get the remnants > of the old antenna out? Putting one of these > in it's place would be a prudent move. > > If that's not practical/possible, then splicing an > extension on the upper end to replace the cut off > length would be helpful . . . even if it lays off at > right angles to the antenna. This would serve as > an extension moving back toward 1/4 wave for the > upper element and/or 'capacity' hat to load the > shortened antenna thus making it look electrically > like a quarter wave. > > Your antenna guy will know all about this and > will be able to help you with the patch. > > ** > > ** Bob . . . > ________________________________________________________________________________
Subject: St Patrick's Day
From: "RV7ASask" <rv7alamb(at)sasktel.net>
Date: Mar 31, 2012
I would like to thank Bob for sharing his knowledge, for his patience, guidance and the Aeroelectric course I took in North Carolina about four years ago. Also, thanks to all the other forum contributors from whom I have gleaned so much. On St Patricks Day, 17 March 2012, in Tisdale, Saskatchewan, with sunny skies, light wind and 8 degrees C, RV7A, C-FLAM flew for the first time. It was nine years in construction and worth every moment. The aircraft flew exactly as I hoped it would. It has an Aero Sport IO-360 with dual Light Speeds and dual alternators. The electrical architecture is Bobs Z12 and I am very happy with the final results. On the panel there is a Dynon Skyview and four Garmins, a GDU370, SL30, GTX327 and GMA340. An iPad 2 is mounted with a Ram mount and has checklists, charts, POH and more. My grandson says he will be able to play Angry Birds on the long hauls. Thanks again to everyone. Warmest regards David Lamb Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369684#369684 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Uneven dipole elements
Date: Mar 31, 2012
Bob: Thanks for explaining the shortened shield on the coax. Sa soon as I saw your diagram I immediately wondered why only 14". Noel From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: March 31, 2012 2:06 AM Subject: RE: AeroElectric-List: Uneven dipole elements At 06:46 PM 3/30/2012, you wrote: I'm wondering if it is now operating like a modified Windom antenna (not straight at centre and different length elements). I also would like to know if it is vertical or horizontal This would be a vertically polarized antenna and appears to be 1/2 wavelength. Is there enough 'bulk' at the coax end to house a small toroid transformer? There's another 1/2-wave kid on the block which is actually a center-fed dipole with the feedline running up the middle of the lower half of the dipole. It's marketed as the Air Whip at http://miracleantenna.com/shop-products/aviation/42 <http://miracleantenna.com/shop-products/aviation/42> Emacs! The black box houses the common-mode choke which de-couples the feed line from the high-voltage end of the dipole thusly. http://tinyurl.com/78ph8nz http://tinyurl.com/6ul4o6f Waaayyy back when, there was a brief brush with tiny toroids to match coax feedlines to center fed dipoles the cores they used were very low power handling . . . hence good for receive only. The Antenna Dynamics product has the look and 'smell' of a similar product. By the way, the reason it's not 44" (half wave in free space) long is because the lower 1/4 wave is in coax which is shortened to about 14" by the coax velocity factor. Miracle Antenna is a newer kid on the block and gets very good reviews from their whole customer base which includes amateur radio and SWL applications. Dave, is there any chance you can get the remnants of the old antenna out? Putting one of these in it's place would be a prudent move. If that's not practical/possible, then splicing an extension on the upper end to replace the cut off length would be helpful . . . even if it lays off at right angles to the antenna. This would serve as an extension moving back toward 1/4 wave for the upper element and/or 'capacity' hat to load the shortened antenna thus making it look electrically like a quarter wave. Your antenna guy will know all about this and will be able to help you with the patch. Bob . . . ________________________________________________________________________________
Subject: motorcycle coolant sensor question
From: Sheldon Olesen <saolesen(at)sirentel.net>
Date: Mar 31, 2012
Can a single coolant temperature sensor be used to send temp data to two different units, an engine control unit and display unit? My son is building a self designed racing bike and I have been placed in charge the electrical system. Sheldon Olesen N475PV RV-10 Sent from my iPad ________________________________________________________________________________
Date: Mar 31, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: motorcycle coolant sensor question
At 01:25 PM 3/31/2012, you wrote: > > >Can a single coolant temperature sensor be used to send temp data to >two different units, an engine control unit and display unit? My >son is building a self designed racing bike and I have been placed >in charge the electrical system. It depends. To find the answer you need to know what the characteristics are for the sensor -AND- the circuitry that watches it. Legacy temperature sensors are thermistors . . . a resistor that changes value in a predictable and repeatable way depending on surrounding temperature. A newer device is an integrated circuit which generally offers more user friendly, linear signals. How are these two temperature inputs to be used? Is the 'sensor' already part of the suite of components for one of the data users . . . and you have a second user that wants to eavesdrop on the data? Sensing temperature in a meaningful way is really easy. It might be better that each system have its own sensor tailored to its technology. Have you crafted a power/data distribution diagram? Suggest you start with emulating one of the z-figures and do a pen-to-paper actualization of your design goals. Then do a similar drawing that speaks to control and signal lines while identifying the systems and parts KNOWN to be compatible with their function. At Beech this was called a system interface document. It was a drawing of wire bundles PLUS a table of inputs and outputs from each device along with gains, offsets, and scale factors for signals expected and offered. If you had such a set of documents to share, I and others here on the List can be more specific in our advice. Bur right now, there's not enough data in your question to give a reliable answer. Bob . . . ________________________________________________________________________________
Date: Mar 31, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: St Patrick's Day
At 09:09 AM 3/31/2012, you wrote: > >I would like to thank Bob for sharing his >knowledge, for his patience, guidance and the >Aeroelectric course I took in North Carolina >about four years ago. Also, thanks to all the >other forum contributors from whom I have gleaned so much. > >On St Patricks Day, 17 March 2012, in >Tisdale, Saskatchewan, with sunny skies, light >wind and 8 degrees C, RV7A, C-FLAM flew for the >first time. It was nine years in construction >and worth every moment. The aircraft flew >exactly as I hoped it would. It has an Aero >Sport IO-360 with dual Light Speeds and dual >alternators. The electrical architecture is >Bobs Z12 and I am very happy with the final results. > > On the panel there is a Dynon Skyview and four > Garmins, a GDU370, SL30, GTX327 and GMA340. An > iPad 2 is mounted with a Ram mount and has > checklists, charts, POH and more. My grandson > says he will be able to play Angry Birds on the long hauls. That seminar was in Winterville, NC in the spring of 2007. You've come a long way my friend. How about a picture of your airplane . . . preferably with yourself included? For that matter, it would be interesting to add a page to aeroelectric.com for pictures of List Member's airplanes. Email to me directly along with basic particulars including date of first flight. Congratulations! Bob . . . ________________________________________________________________________________
Date: Mar 31, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Uneven dipole elements
At 01:33 AM 3/31/2012, you wrote: >We found a diagram of what we think the antenna >looks like. I'll post of a picture of it next >week at the latest. It's a slanted-N shape similar to an Archer. > >Earlier I described equal-length parallel >elements. Turns out they're carbon >reinforcements that aren't part of the >antenna. I'll show them in the picture when I post it. How much of the structure/skin around this antenna is carbon? Buried antennas in carbon aircraft typically don't do real well. Fiberglas/epoxy is okay but the carbon is both conductive as well as dissipative . . . in other words it turns a portion of your signal into heat. Bob . . . ________________________________________________________________________________
Date: Mar 31, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: LED WigWag with B&C SSF-1
At 06:19 PM 3/30/2012, you wrote: > >Bob, can I wire two LED landing and taxi lights per Page 3.0 (Ref DE >12/15/11) but using a single switch (already installed and labeled >in unflown RV-6) as shown on Page 3.0 from 2003? Thank you Give me a few days on this. It occurs to me that I've been twisting what WAS a good system for incandescent lamps into a pretzel in search of the elegant solution for LED lamps. I'm going to do a clean-piece-of-paper study of some alternatives to the automotive flasher. Given the very low current draw and insignificant inrush for the LED lamps, some sort of all solid state approach is called for. I think some others here on the List have mentioned their own adventures in this arena. Perhaps they'll share. In any case, there's a cleaner way to go about it and so the answer is "Yes, we can use the single switch configuration you've already installed." Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: LED WigWag with B&C SSF-1
Date: Mar 31, 2012
I used a ETHFSS-SP with my HID landing lights as other on VAF have suggested. I can have them both on or flashing mode. Should work with LED's I would think see... http://www.bestwarninglights.com/m7/ETHFSS-SP--sound-off-signal-select-a-pat tern-headlight-flasher-positive-switching.html $48 so not cheap but solid state and good for up to 55W per side. Bevan -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Saturday, March 31, 2012 6:33 PM Subject: Re: AeroElectric-List: LED WigWag with B&C SSF-1 --> At 06:19 PM 3/30/2012, you wrote: >--> > >Bob, can I wire two LED landing and taxi lights per Page 3.0 (Ref DE >12/15/11) but using a single switch (already installed and labeled in >unflown RV-6) as shown on Page 3.0 from 2003? Thank you Give me a few days on this. It occurs to me that I've been twisting what WAS a good system for incandescent lamps into a pretzel in search of the elegant solution for LED lamps. I'm going to do a clean-piece-of-paper study of some alternatives to the automotive flasher. Given the very low current draw and insignificant inrush for the LED lamps, some sort of all solid state approach is called for. I think some others here on the List have mentioned their own adventures in this arena. Perhaps they'll share. In any case, there's a cleaner way to go about it and so the answer is "Yes, we can use the single switch configuration you've already installed." Bob . . . ________________________________________________________________________________
Date: Apr 01, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: motorcycle coolant sensor question
At 10:11 PM 3/31/2012, you wrote: > >A little mix up perhaps. I was just asking for an example of an >interface document for my own information. Sometimes organizing the >info. is half the battle. I like to see how others have solved a >problem. I guess I was expecting something with:"a table of inputs >and outputs from each device along with gains, offsets, >and scale factors for signals expected and offered." No mixup. I understood what you were requesting. Problem is that the few dozens of documents I've had any contact with or input to are Hawker-Beechcraft documents and not part of my library for sharing. I understand what you're experiencing when trying to visualize the expected work-product as described verbally. It's especially bad when the document description is part of a "policies and procedures manual" crafted by English majors and publications 'experts'. At HBD we had rows of P&P Manuals with requirements written so badly as to defy understanding. The first time I was confronted with the ISO9000 approved policy and procedure for writing a report, I was pretty much adrift for direction. I'd been writing technical documents to Mil-Std-490 for decades. They seemed to have satisfied the needs of thousands of readers of technical documents since WWII. I could outline and draft one in my sleep. Now comes the 'better' way with a description that might just as well be written in Swahili. Grammatically correct, perfectly formatted, picturesque fonts . . . but for the most part vacuous. The problem with such instructions is two-fold. The understanding by which a writer produces produces a document probably differs from understanding possessed by the readers, not the least of which is some individual who has to 'approve' the document . . . not understand it but approve it. I abandoned the rows of books on the shelf. When tasked with production of some document described therein, I asked, "please provide me with a published document of this type that meets with your approval." Only then did I have half a chance of delivering to the customer's desires. It's a certainty that the P&P manual bordered on useless. Let's start with your proposed wiring diagrams. You're right . . . the planning is the hard part. When I did my first brain-child to TC aviation in '75 I found that making it work was 20% of the effort. Packaging it for environmental concerns was 40%, documenting for design review, qualification and production was 40%. Nowadays, making it work is 10%, packaging is 30% and generating the required piles of paper is 70% . . . with the risk that no two people agree on what the piles should look like. This guarantees cost overruns when the paper effort going into paper piles busts the statement of work. Let's keep your paperwork at no more than 40%. Further, doing it right will make the rest fun instead of vexing. Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Converting to externally reg alternator
Date: Apr 01, 2012
Bob, I have seen it but can't find it right now. Can you point me to an instruction for converting an internally regulated alternator to external? Thanks Bevan ________________________________________________________________________________
Date: Apr 02, 2012
From: David <dlposey-atlanta(at)att.net>
Subject: Fwd: Fwd: The Fence
________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Converting to externally reg alternator
Date: Apr 02, 2012
I have seen it but can't find it right now. Can you point me to an instruction for converting an internally regulated alternator to external? Thanks Bevan Here is one at the EAA site which might help you. http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp Roger ________________________________________________________________________________
Subject: Re: Converting to externally reg alternator
From: "Eric M. Jones" <emjones(at)charter.net>
Date: Apr 02, 2012
Eric is easily amused... try: http://lmgtfy.com/?q=Converting+to+externally+regulated+alternator But here is where I will annoy Bob N.: Consider the fact that if automobile regulators had a lower failure rate if they were externally regulated, auto makers would use them. The fact is that BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a nearly-zero failure rate. Then make your decision. I have had several builders send me their external regulators for examination. This cemented my opinion permanently. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369828#369828 ________________________________________________________________________________
Subject: Re: Converting to externally reg alternator
From: Jared Yates <email(at)jaredyates.com>
Date: Apr 02, 2012
I think Bob will say that the failure rate is less important than the failure mode. At least that is what I would say. On Apr 2, 2012, at 9:43, "Eric M. Jones" wrote: > > Eric is easily amused... > > try: > > http://lmgtfy.com/?q=Converting+to+externally+regulated+alternator > > But here is where I will annoy Bob N.: Consider the fact that if automobile regulators had a lower failure rate if they were externally regulated, auto makers would use them. The fact is that BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a nearly-zero failure rate. > > Then make your decision. I have had several builders send me their external regulators for examination. This cemented my opinion permanently. > > -------- > Eric M. Jones > www.PerihelionDesign.com > 113 Brentwood Drive > Southbridge, MA 01550 > (508) 764-2072 > emjones(at)charter.net > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=369828#369828 > > > > > > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
I have been flying over 12 years on a Bosch (rebuilt) alternator with internal regulator - with no problems. The only downside I can see is that once it has bootstrapped itself, removing voltage to the field coil does not stop the output. So if I had a runaway alternator it could theoretically fry my electronics - on the other hand, in all my life of driving automobiles and the one or two alternator failures (failed diodes), I've never had a runaway alternator failure mode. FWIW Ed Edward L. Anderson Anderson Electronic Enterprises LLC 305 Reefton Road Weddington, NC 28104 http://www.andersonee.com http://www.eicommander.com -------------------------------------------------- From: "Eric M. Jones" <emjones(at)charter.net> Sent: Monday, April 02, 2012 9:43 AM Subject: AeroElectric-List: Re: Converting to externally reg alternator > > > Eric is easily amused... > > try: > > http://lmgtfy.com/?q=Converting+to+externally+regulated+alternator > > But here is where I will annoy Bob N.: Consider the fact that if > automobile regulators had a lower failure rate if they were externally > regulated, auto makers would use them. The fact is that BRAND NEW (not > rebuilt) Nippon Denso alternators seem to have a nearly-zero failure rate. > > Then make your decision. I have had several builders send me their > external regulators for examination. This cemented my opinion permanently. > > -------- > Eric M. Jones > www.PerihelionDesign.com > 113 Brentwood Drive > Southbridge, MA 01550 > (508) 764-2072 > emjones(at)charter.net > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=369828#369828 > > > ________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
Consider the fact that if automobile regulators had a lower failure rate if they were externally regulated, auto makers would use them. The fact is that BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a nearly-zero failure rate. Then make your decision. I have had several builders send me their external regulators for examination. This cemented my opinion permanently. Eric, I believe that perhaps Bob does agree with you, in that the internally regulated alternator has "nearly-zero" but NOT ZERO failure. Apparently there have been some cases of catastrophic over voltage with no way to shut it down, when in the air. Have you found this to be the case with the externally regulated alternators? With the external regulator, when you shut off power to the regulator it positively shuts down the alternator. I personally feel that the risk is very low with the internal regulation, but also wonder why TC aircraft have continued to use external regulation. Roger ________________________________________________________________________________
Date: Apr 02, 2012
Subject: Re: Converting to externally reg alternator
From: Bob Verwey <bob.verwey(at)gmail.com>
Does the crowbar module not offer enough protection? With a VFR day only, electronic ignition setup, minimal elctrogizmos, does not the reserve battery power give a safe reserve? Bob Verwey On 02/04/2012, ROGER & JEAN CURTIS wrote: > Consider the fact that if automobile regulators had a lower failure rate if > they were externally regulated, auto makers would use them. The fact is that > BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a nearly-zero > failure rate. > > Then make your decision. I have had several builders send me their external > regulators for examination. This cemented my opinion permanently. > > > Eric, > > I believe that perhaps Bob does agree with you, in that the > internally regulated alternator has "nearly-zero" but NOT ZERO failure. > Apparently there have been some cases of catastrophic over voltage with no > way to shut it down, when in the air. Have you found this to be the case > with the externally regulated alternators? With the external regulator, > when you shut off power to the regulator it positively shuts down the > alternator. > > I personally feel that the risk is very low with the > internal regulation, but also wonder why TC aircraft have continued to use > external regulation. > > Roger > > ________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
Does the crowbar module not offer enough protection? With a VFR day only, electronic ignition setup, minimal elctrogizmos, does not the reserve battery power give a safe reserve? Bob Verwey The Conventional crowbar module is used with the external regulator. The internal regulator does not work with the external crowbar circuit. Roger ________________________________________________________________________________
Subject: Re: Converting to externally reg alternator
From: Jared Yates <email(at)jaredyates.com>
Date: Apr 02, 2012
My internally regulated plane power alt has crowbar ov protection. On Apr 2, 2012, at 12:12, "ROGER & JEAN CURTIS" wrote: > > Does the crowbar module not offer enough protection? With a VFR day > only, electronic ignition setup, minimal elctrogizmos, does not the > reserve battery power give a safe reserve? > > Bob Verwey > > > The Conventional crowbar module is used with the external > regulator. The internal regulator does not work with the external crowbar > circuit. > > Roger > ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
Wow, I didn't think my question would hit such a sensitive nerve. In the same league as a primer war. My question was about the "how" but many of you are interested in discussing the "why". Here's where I'm coming from. For better or worse, the decision was made a long time ago to configure my electrical system for external regulation ala Bob M. Now I'm getting close to needing an alternator and looking at the options. I will have an SD-8 backup alternator and therefore don't consider the main alternator as being required to be of the absolute best quality. It just needs to have a failure mode that does not affect other more expensive electronics. As far as I know, there are no "100% guaranteed to work for ever" alternators anyway. So my theory is to have a spare in the hangar ready to go or to be brought to me when/if a failure occurs. I'm thinking I would rather have two $100 alternators that I have converted to external regulation and tested than one $595 alternator and no spare. When, converting two to external regulation I will learn something and decide whether I can do this when away from my regular tool box. I may be too far from my spare and have to buy an internally regulated one and convert it out in the field. I seem to recall that it's not too difficult of a process. More like a removal of unnecessary parts. Something I am usually pretty good at. I plan on keeping some maintenance papers in the plane's tool bag anyway, one of which could be the alternator process. My thoughts only. You may have another opinion and that's fine with me. Bevan "I like to build and fix things" > _____________________________________________ > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of ROGER > & JEAN CURTIS > Sent: Monday, April 02, 2012 9:12 AM > To: aeroelectric-list(at)matronics.com > Subject: RE: AeroElectric-List: Re: Converting to externally reg > alternator > > > Does the crowbar module not offer enough protection? With a VFR day > only, electronic ignition setup, minimal elctrogizmos, does not the > reserve battery power give a safe reserve? > > Bob Verwey > > > The Conventional crowbar module is used with the external regulator. > The internal regulator does not work with the external crowbar circuit. > > Roger ________________________________________________________________________________
Subject: Re: Wingtip VOR antenna . . . a clearer picture
From: Mark Harris <harrismarkr(at)hotmail.com>
Date: Apr 02, 2012
Hi Bob Thanks for the reply ref the differing dimensions of the VOR antenna.i am some way off flying but will run with the one already made and see how it performs.depending on the out come I can always try the other dimension antenna. Thanks for all your help Mark Rent our beautiful 3 bedroom luxury villa in Orlando, Florida. View our virtual tour but book direct with us. See the link below:- http://www.florida1strentals.com/property.php?id=21 Contact Emma and Mark Harris 01582 529820 harrisfloridavilla(at)hotmail.com On 28 Mar 2012, at 21:47, "Robert L. Nuckolls, III" wrote: > > Thanks to List member van Saten, we've got some > better details for a DIY wingtip VOR antenna. See: > > http://tinyurl.com/6v5gvhx > > It seems that the sketch I was working from years ago > was either not up to date or in error. > > The insulator turns out to be either glass or cloth > filled phenolic, 0.062 inches thick. The measured > value of an off-the-shelf gamma-match capacitor is > 34 pf @ 1 KHz. > > I think the data above will get the builder closer to > a workable example of this particular antenna. > > Thanks Don! Your antenna will be back in the mail today. > > > Bob . . . > > > > > ________________________________________________________________________________
From: <longg(at)pjm.com>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
Beven, According to Mr. Google, this should take about 30 minutes. http://www.wallaceracing.com/alt-conversion.html It looks like it's more popular to covert externals to internals (at least in the automotive world where the externals always failed). Funny, I don't see too many folks lying under their cars on the turnpike pulling out their internally regulated jobs. I've run many a car well past 100k and never had the alternator go. That's why I've got an IR in my bird. I took have an SD-8. Wouldn't leave home without it. Occasionally I talk to pilots who piss and moan about how they had to fly their so and so to the alternator shop so they could have Mr. Alternator specialist provide a special part for their regulator. No Thanks Cut those wires and go fly. It's summer time. Glenn, N57 -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of B Tomm Sent: Monday, April 02, 2012 1:39 PM Subject: RE: AeroElectric-List: Re: Converting to externally reg alternator Wow, I didn't think my question would hit such a sensitive nerve. In the same league as a primer war. My question was about the "how" but many of you are interested in discussing the "why". Here's where I'm coming from. For better or worse, the decision was made a long time ago to configure my electrical system for external regulation ala Bob M. Now I'm getting close to needing an alternator and looking at the options. I will have an SD-8 backup alternator and therefore don't consider the main alternator as being required to be of the absolute best quality. It just needs to have a failure mode that does not affect other more expensive electronics. As far as I know, there are no "100% guaranteed to work for ever" alternators anyway. So my theory is to have a spare in the hangar ready to go or to be brought to me when/if a failure occurs. I'm thinking I would rather have two $100 alternators that I have converted to external regulation and tested than one $595 alternator and no spare. When, converting two to external regulation I will learn something and decide whether I can do this when away from my regular tool box. I may be too far from my spare and have to buy an internally regulated one and convert it out in the field. I seem to recall that it's not too difficult of a process. More like a removal of unnecessary parts. Something I am usually pretty good at. I plan on keeping some maintenance papers in the plane's tool bag anyway, one of which could be the alternator process. My thoughts only. You may have another opinion and that's fine with me. Bevan "I like to build and fix things" > _____________________________________________ > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of > ROGER & JEAN CURTIS > Sent: Monday, April 02, 2012 9:12 AM > To: aeroelectric-list(at)matronics.com > Subject: RE: AeroElectric-List: Re: Converting to externally reg > alternator > > > Does the crowbar module not offer enough protection? With a VFR day > only, electronic ignition setup, minimal elctrogizmos, does not the > reserve battery power give a safe reserve? > > Bob Verwey > > > The Conventional crowbar module is used with the external regulator. > The internal regulator does not work with the external crowbar circuit. > > Roger ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Re: Converting to externally reg alternator
Date: Apr 02, 2012
Eric, Very funny. But even this google search did not turn up what I was looking for. It seems that your search result was to convert an old car to internally regulated alternators. So I say "very funny". I know how to do a google search. What I was looking for was a step by step documented procedure I had seen on someone's build site. Could it be that automotive manufactures may have gone to internal regulation because is was more reliable via a solid state design with all components contained within one housing therefore easier to install in the vehicles coming down the assembly line? Were the voltage regulators that you took apart and didn't like, mechanical regulators? I seem to recall my 1971 chev truck had a mechanical regulator mounted on the fender. Bevan -----Original Message----- From: owner-aeroelectric-list-server(at)matronics.com [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Eric M. Jones Sent: Monday, April 02, 2012 6:43 AM Subject: AeroElectric-List: Re: Converting to externally reg alternator --> Eric is easily amused... try: http://lmgtfy.com/?q=Converting+to+externally+regulated+alternator But here is where I will annoy Bob N.: Consider the fact that if automobile regulators had a lower failure rate if they were externally regulated, auto makers would use them. The fact is that BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a nearly-zero failure rate. Then make your decision. I have had several builders send me their external regulators for examination. This cemented my opinion permanently. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=369828#369828 ________________________________________________________________________________
From: "ROGER & JEAN CURTIS" <mrspudandcompany(at)verizon.net>
Subject: Converting to externally reg alternator
Date: Apr 02, 2012
Bevan, Was this not the information you were looking for?? I have seen it but can't find it right now. Can you point me to an instruction for converting an internally regulated alternator to external? Thanks Bevan Here is one at the EAA site which might help you. http://www.eaa.org/experimenter/articles/2009-09_howto_alternator.asp Roger ________________________________________________________________________________
Date: Apr 02, 2012
From: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: Re: Converting to externally reg alternator
At 08:43 AM 4/2/2012, you wrote: > >Eric is easily amused... > >try: > >http://lmgtfy.com/?q=Converting+to+externally+regulated+alternator > >But here is where I will annoy Bob N.: Consider the fact that if >automobile regulators had a lower failure rate if they were >externally regulated, auto makers would use them. The fact is that >BRAND NEW (not rebuilt) Nippon Denso alternators seem to have a >nearly-zero failure rate. > >Then make your decision. I have had several builders send me their >external regulators for examination. This cemented my opinion permanently. Eric my man! This has never been a discussion about comparative failure rates. If I've failed to illuminate the logic behind my writings, indulge me please with the following: Without doing a very hi-labor study to discover practical failure rates of any design philosophy, one is presented with the question: "Knowing that the failure rate of neither philosophy is zero, what is the potential return on investment for some active form of over-voltage management?" In retrospect, had we considered and implemented the PlanePower approach for ADDING ov protection to an existing IR alternator design, it's an indisputable fact that B&C could have brought a lower cost alternator/ regulator design to the OBAM aircraft marketplace than the products which ultimately became the LR series regulators and L series alternators. But even with the PP philosophy in our hip pocket, it did not address another feature of the design philosophy for having ACTIVE notification of low voltage as part of the package. So once you have . . . (1) a black box with LV warn and OV management features and . . . (2) we still have to open the alternator to make the necessary interface that provides positive, any time control over the alternator's output (a legacy design goal carried across from TC aviation). (3) it just made more sense to us at the time to offer one black box that offered the features of three functions classically accomplished by three separate devices, hence the LR1, 2 and 3 series regulators were crafted and offered to OBAM aviation. I'm still amazed that folks get so embroiled over the idea of "my alternator is more RELIABLE than your alternator." It's not about relative reliability. It's about delivering to design goals that have served us well in airplanes for nearly 100 years. The simple-idea behind OV protection has ALWAYS been an assumption that ANY regulator can fail in a runaway condition. Unless KNOW that a particular design combined with proper installation and maintenance has a 10 to the minus 9 failure rate, then the FAA doesn't care if one alternator is 1.5 x 10 to the minus 7 and the other is 1.0 x 10 to the minus 8 and perhaps a third can be expected to crap out in less than 2000 hours. The working assumption is that they are not perfect and building an automated response to acknowledged imperfections is not only a good idea, it's mandated: FAR23.2451(c)(5) "Each generator/alternator must have an overvoltage control designed and installed to prevent damage to the electrical system, or to equipment supplied by the electrical system that could result if that generator/alternator were to develop an overvoltage condition." Notice that no relief is offered for the more "reliable" of two systems. I have always said that the modern automotive products are of stellar value and performance. I also elaborated on the potential for equal or better value in remanufactured alternators in the latest revision to chapter 3 in the 'Connnection. http://tinyurl.com/cx6426c So in retrospect, I still believe that the B&C LR/L combo was a good decision. We could probably redesign for ease of manufacturing and reducing costs, I don't see an alternative architecture that still stands up to design and marketing goals we adopted at that time. Even if we left the stock regulator in place, we still have to open the alternator for other reasons. So why not keep the internal mods simple . . . and make the most vulnerable parts easily trouble shot and replaced without pulling a very reliable alternator off the engine? The fact that perhaps thousands of OBAM aircraft are flying successfully with un- modified IR alternators doesn't even merit honorable mention in the discussion. It's not about comparative reliability. It's about perceptions of perfection. I'm aware of no suppliers of perfect alternators . . . nor is the FAA. Even PlanePower subscribes to legacy design goals when they modify commercial- off-the-shelf alternators to provide OV management and any-time, any-conditions, positive control from the cockpit. I have recommended nothing more . . . . or less. If I am annoyed, its because there are those among us that cast me in the role of Ralphie's mother who admonishes, "Don't shoot that B-B gun, you'll put your eye out!" My concerns are not about the very low risk for loosing one's eyesight. They're about understanding and managing risks that are NOT zero. We're not even talking about safety. I'm aware of no fatal accident where an unmitigated ov condition precipitated the event. . . . risk with potential for damage that far exceeds the cost of a mitigating feature. Bob . . . ________________________________________________________________________________
From: "B Tomm" <fvalarm(at)rapidnet.net>
Subject: Converting to externally reg alternator
Date: Apr 02, 2012
Yes but, I seem to recall a modification procedure that did not require machining any part of the case. It also did (as I recall) have you completely remove the internal regulator. So the process of conversion was different as I recall. All accomplished with simple hand tools. Perhaps Bob will chime in with his recommendation. Bevan > _____________________________________________ > From: owner-aeroelectric-list-server(at)matronics.com > [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of ROGER > & JEAN CURTIS > Sent: Monday, April 02, 2012 12:12 PM > To: aeroelectric-list(at)matronics.com > Subject: AeroElectric-List: Converting to externally reg alternator > > Bevan, > > Was this not the information you were looking for?? > > > I have seen it but can't find it right now. Can you point me to an


March 19, 2012 - April 02, 2012

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