AeroElectric-List Digest Archive

Tue 01/17/12


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 06:37 AM - Weak and Static on Transmission ()
     2. 07:18 AM - Re: Inexpensive Runway lighting (Robert L. Nuckolls, III)
     3. 07:21 AM - Re: Wire Bundle Wrapping Tape? (Robert L. Nuckolls, III)
     4. 07:29 AM - Re: Wire Bundle Wrapping Tape? (Robert L. Nuckolls, III)
     5. 08:08 AM - Re: Weak and Static on Transmission (Robert L. Nuckolls, III)
     6. 08:40 AM - Account hacked (earl_schroeder@juno.com)
     7. 01:00 PM - Re: Wire Bundle Wrapping Tape? (James Kilford)
     8. 04:46 PM - Re: Wire Bundle Wrapping Tape? (Robert L. Nuckolls, III)
     9. 06:37 PM - Crimping to component leads? (Jon McLin)
    10. 07:23 PM - Re: Crimping to component leads? (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 06:37:04 AM PST US
    From: <bakerocb@cox.net>
    Subject: Weak and Static on Transmission
    1/17/2012 Hello Bill Bradburry, You wrote: 1) "Although I didn't need that much length to reach the antenna, I made the coax the recommended 13 feet or so length." It may not have a direct bearing on your "weak and lots of static but usable" problem, but it sounds like you are a bit confused about the antenna requirements of the GNS 430W. The specific coax length that you referred to in your posting refers to the GPS antenna for the 430W. High quality coax such as RG400 is required. Here is what AAE says about the cable length for one of their VHF comm antennas: "Q. What cable length is recommended for the antenna ? A. Any length can be used. This antenna is impedance matched to 50 ohms to allow you to use any length required." 2) "Any ideas as to where I should begin my investigation on the source of this static?" You could narrow down the source of the problem a bit if you could borrow a GNS 430W from a fellow builder or shop and install it temporarily for testing. If the problem goes away the problem is inside your 430W box and not the aircraft installation. 'OC' Baker Says: "The best investment we can make is the time and effort to gather and understand knowledge." PS: Pull out and reseat your 430W box before going to the bother of borrowing another unit -- the problem may just be a reseating or mis aligned pin condition. ============================================================ Time: 06:10:00 AM PST US From: "Bill Bradburry" <bbradburry@bellsouth.net> Subject: AeroElectric-List: Weak and Static on Transmission I have a GNS430W radio and Advanced Aircraft Electronics high gain antenna model 5T in my Lancair Legacy (fiberglass fuselage). The antenna is mounted vertically behind the rear bulkhead on the right side of the fuselage. Although I didn't need that much length to reach the antenna, I made the coax the recommended 13 feet or so length. (right now I cant remember the exact length recommended). This antenna is designed to be mounted inside plastic airplanes and doesn't require a ground plane. I get a "weak and lots of static but usable" reports from radio checks and on occasion, while airborne, static gets so great that I can not hear approach at all. I have had to make two NORDO landings at a Class C airport that is located under an overhanging Class B airspace due to the receiving static. The controllers are beginning to take exception to this and I need to get this fixed! :>) I have checked the SWR on the antenna and it was around 1.5 which I understand to be fine. Any ideas as to where I should begin my investigation on the source of this static? Bill B


    Message 2


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    Time: 07:18:32 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Inexpensive Runway lighting
    As far as the runway lights, I guess it depends on how much you trust your runway lights. If you're willing to trust your work on your OBAM aircraft, I wouldn't think there would be a problem trusting your OBAM runway lights. Raymond Julian Kettle River, MN Excellent point! I've been wrestling semantics with some lawyers who would like for the public to believe that "experimental" aircraft are labeled such because they are fraught with heretofore unproven and potentially dangerous features of design and fabrication. I offered the notion that "experimental" is synonymous with "exploration" and "discovery". For students in the chemistry lab, the treatment of certain substances is indeed an "experiment". For the teacher, it's a recipe for a successful teaching moment. The outcome of the experiment is known to the teacher . . . just as the outcome of a kit airplane built to instructions and common sense. When the kit is completed and flying, that builder can now be a teacher in that they've "been there, done that". It is the job of a teacher to make sure that deviations from instructions are well thought out, perhaps "explored or discovered", and proven to be useful, non-hazardous changes whereupon the changes are no longer experimental. Experimentation is a process by which a useful design goal is achieved. When one sets out to fabricate DIY runway lights, it's almost a certainty that individuals who choose to experiment in public will sort through the ideas and potential pitfalls in places like this List-Server. Even then, I would expect the developer to use the system many times under ever-increasing levels of degradation due to environmental effects . . . and report back as to the limits he/she personally places on the utility of that system. TC aviation has processes and procedures for advancing the state of the art and reducing risk. TC aviation is famous for what I call the $1000 meeting where useful advances are slow and cumbersome. OBAM aviation has a process too. It's different but no less effective . . . and a whole lot more satisfying. We who sit at our keyboards with a cup of coffee collaborate and advance an idea further and faster to the benefit of hundreds who read now and that many more who read the archives later. This is the process by which WE choose to reduce risk. Keep it up folks! We're doing good work here. Bob . . .


    Message 3


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    Time: 07:21:03 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Wire Bundle Wrapping Tape?
    At 08:48 AM 1/16/2012, you wrote: >This sounds a lot like rib-lacing cord. Is that an acceptable substitute? Not sure which direction the substitution is taking place. Are you asking if you can use the recommended rib lacing cord to tie wire bundles? The answer would be certainly. Use the flat-lace described to tie fabric to ribs? Don't know. I'd be inclined to stick with the legacy, 'been there, done that' materials. Bob . . .


    Message 4


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    Time: 07:29:07 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Wire Bundle Wrapping Tape?
    At 06:38 PM 1/16/2012, you wrote: Thanks Bob; I knew you would have the right link to a certified product. Let's not be too quick to call it 'certified' . . . it's certainly a material built to known quality and performance standards and suited to the task on certified airplanes. But no part or accessory gets holy-watered by the FAA with any sort of certification, only complete airframes get type certificates. Once ANY part or material shows up on the bill of materials for a TC aircraft, it is 'qualified' for such service irrespective of its pedigree. There are many products built to rigorous specifications that may or may no be suited to task aboard an airplane. So just because it's 'mil-spec' doesn't make it holy. In this case, the flat lace cited has a long and successful history in TC aircraft and elsewhere. Bob . . .


    Message 5


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    Time: 08:08:02 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Weak and Static on Transmission
    At 08:07 AM 1/16/2012, you wrote: . . . I get a "weak and lots of static but usable" reports from radio checks and on occasion, while airborne, static gets so great that I can not hear approach at all. I have had to make two NORDO landings at a Class C airport that is located under an overhanging Class B airspace due to the receiving static. The controllers are beginning to take exception to this and I need to get this fixed! :>) Bob's points are well taken. I can expand by suggesting that you are committed to the classic "divide and conquer" ploy . . . you need to separate the potential for an antenna system problems from the radio's potential problems. It's difficult to sift the sands of potential problems without hearing the nature of the "static". If you were getting a signal report from a grey-bearded ham radio operator he would qualify the report with "weak to the point of inducing pop-corn noise", or succumbing to atmospheric noises like lightning crashes, or scratching noise reminiscent of a loose connection. Further, such noises heard by experienced ears could probably tell if it was in the RF or audio chain of your transmission system. But alas, I've never heard a cogent signal report from a tower operator and seldom from other pilots in their own airplanes. I'd recommend a series of experiments. Plug a hand held into the antenna system and get signal reports from other pilots. You can start on the ground but they should probably be airborne so that they can fly outbound and get some sense of signal strength along with judgement of audio quality. If it doesn't repeat on the ground, then you go flying too. If the other guy reports noises, do YOU hear any noises? Open the radio's squelch control and tune in stations some distance away. Does the complaining controller repeat the complaint while the hand-held is being used? If the antenna system seems okay, this leaves the radio. "Weak and static" suggests one or more issues combining to reduce power output and introduction of noises reminiscent of loose connections. Probably nothing you can do about it personally except to confirm poor performance by getting a measurement of output power during an SWR check. This takes a unique kind of instrument not often found in the OBAM aviation toolbox. Emacs! Also, check with someone else in another airplane or even on the ground who overhears both sides of your conversation with the controllers. Does that third party agree with the controller's assessment? Can they refine the description of "static"? I assisted in a similar exercise many years ago where the builder left a tape recorder running with the mic in front of the Unicom receiver in his hangar. One could hear both sides of the conversation. In this case, both sides of the conversation were clear. We then did a frequency check on the airplane radio and found that it was at the high end of the spec . . . enough off center to be at the edge of the government's receiver bandwidth but still inside the bandwidth of the lower cost receiver in the hangar. Replacing one of the transmitter's crystals fixed the problem. In your modern, frequency synthesized radio, this is an exceedingly remote possibility. The point is that you need GOOD data that tests a host of possibilities. "Weak and static" from one observer is insufficient data. Bob . . .


    Message 6


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    Time: 08:40:57 AM PST US
    From: "earl_schroeder@juno.com" <earl_schroeder@juno.com>
    Subject: Account hacked
    Please ignore any emails from my yahoo account.. I am NOT in England or anywhere else and do NOT send money anywhere!! We are working hard to correct this. Thanks!


    Message 7


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    Time: 01:00:24 PM PST US
    Subject: Re: Wire Bundle Wrapping Tape?
    From: James Kilford <james@etravel.org>
    I was wondering if there was anything special about the electrical type that would preclude me from using the spare flat waxed rib cord I have -- it came on a reel with about 2 miles of cord, so there's quite a bit left over from when I did the covering! Thanks for the advice. James On 17 January 2012 15:18, Robert L. Nuckolls, III < nuckolls.bob@aeroelectric.com> wrote: > nuckolls.bob@aeroelectric.com**> > > At 08:48 AM 1/16/2012, you wrote: > >> This sounds a lot like rib-lacing cord. =C3=82 Is that an acceptable >> substitute?=C3=82 >> > > Not sure which direction the substitution is taking > place. Are you asking if you can use the recommended > rib lacing cord to tie wire bundles? The answer would > be certainly. Use the flat-lace described to tie > fabric to ribs? Don't know. I'd be inclined to > stick with the legacy, 'been there, done that' materials. > > > Bob . . . > > =====**=================== ===========**= /www.matronics.com/Navigator?AeroElectric-List> =====**=================== ===========**= =====**=================== ===========**= com/contribution> =====**=================== ===========**= > >


    Message 8


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    Time: 04:46:38 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Wire Bundle Wrapping Tape?
    At 02:54 PM 1/17/2012, you wrote: I was wondering if there was anything special about the electrical type that would preclude me from using the spare flat waxed rib cord I have -- it came on a reel with about 2 miles of cord, so there's quite a bit left over from when I did the covering! Thanks for the advice. I think that's a safe substitution. In fact, does your spool of flat lace have any numbers on it . . . like Mil-T-$#@%? It may well be that the stuff we tie wires with is exactly the same as that used to stitch ribs. In any case, wire ties are not highly stress nor subject to the effects of exposure to the environment. Using it to tie wires is not a high-risk decision. Bob . . .


    Message 9


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    Time: 06:37:18 PM PST US
    From: Jon McLin <jon.mclin@cox.net>
    Subject: Crimping to component leads?
    I recently ran across "crimp sleeves" or some such at a web site, associated with a leaded electrical component. Although it wasn't explicit, I gathered that this is simply a small metal tube which can be used to crimp a wire to the lead of the component. This approach would be convenient in a couple of cases: using resistors in lieu of fuses or circuit breakers for low-amperage circuit (for example, with LED lighting or indicators, one could put the current limiting resistor at the bus rather than the device, and no additional circuit protection would be necessary); or diode functions could be implemented in the wiring harness. I've found no other reference or source to anything like this. Is my interpretation correct? If so, where might one find "crimp sleeves", beyond that one site? I assume this would be limited to lead-to-wire vs. lead-to-lead (as might be used in cascading components) - is this the case? What components are suitable for this approach? The sample was actually an axially-leaded thermostat, but I'd hope/expect it would work with leaded resistors and beefy-bodied plastic-encapsulated diodes. And that leaded reed switches would be a really poor choice. Thoughts? Thx, Jon


    Message 10


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    Time: 07:23:05 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Crimping to component leads?
    At 08:32 PM 1/17/2012, you wrote: I recently ran across "crimp sleeves" or some such at a web site, associated with a leaded electrical component. Although it wasn't explicit, I gathered that this is simply a small metal tube which can be used to crimp a wire to the lead of the component. This approach would be convenient in a couple of cases: using resistors in lieu of fuses or circuit breakers for low-amperage circuit (for example, with LED lighting or indicators, one could put the current limiting resistor at the bus rather than the device, and no additional circuit protection would be necessary); or diode functions could be implemented in the wiring harness. There are a number of such products that I saw in common usage at Beech. Installing in-line components was not allowed but they WERE used to splice wires and COULD be used to install components. Here's my own favorite technique for 'homeless' components. http://www.aeroelectric.com/articles/Homeless/Homeless_Components.htm The goal is (1) good electrical connection and (2) support of vibration prone solid wires including the solid-by-solder strands of the wires. I've found no other reference or source to anything like this. Is my interpretation correct? If so, where might one find "crimp sleeves", beyond that one site? I assume this would be limited to lead-to-wire vs. lead-to-lead (as might be used in cascading components) - is this the case? What components are suitable for this approach? The sample was actually an axially-leaded thermostat, but I'd hope/expect it would work with leaded resistors and beefy-bodied plastic-encapsulated diodes. Yup. And that leaded reed switches would be a really poor choice. You got that right! Bob . . .




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