AeroElectric-List Digest Archive

Thu 06/03/10


Total Messages Posted: 16



Today's Message Index:
----------------------
 
     1. 05:40 AM - Ammeter, voltmeter and other diagnostics (James Kilford)
     2. 05:40 AM - Europa electrics (mike gamble)
     3. 05:55 AM - Re: Ammeter, voltmeter and other diagnostics (Robert L. Nuckolls, III)
     4. 06:41 AM - Flying on the edge of wetness (Larry McFarland)
     5. 08:51 AM - wireing a ICOM A 210 with a Flightcom 403MC (gordon)
     6. 11:09 AM - Re: Ammeter, voltmeter and other diagnostics (earl_schroeder@juno.com)
     7. 01:10 PM - Europa electrics (mike gamble)
     8. 02:23 PM - Re: Long and short hot feeders (rckol)
     9. 04:52 PM - Re: Europa electrics (rampil)
    10. 04:52 PM - Re: Europa electrics (rampil)
    11. 05:40 PM - Wires going to CB question (rparigoris)
    12. 06:33 PM - Re: Flying on the edge of wetness (Robert L. Nuckolls, III)
    13. 06:50 PM - Re: Re: Long and short hot feeders (Robert L. Nuckolls, III)
    14. 06:57 PM - labeling panel (bob noffs)
    15. 08:24 PM - Re: Wires going to CB question (Robert L. Nuckolls, III)
    16. 08:58 PM - Re: The state of the industry (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 05:40:45 AM PST US
    Subject: Ammeter, voltmeter and other diagnostics
    From: James Kilford <james@etravel.org>
    Gents, In reading the AC, it's clear that an ammeter is a useful diagnostic tool onboard the aeroplane, and yet at the same time, Bob's often espousing the virtues of not trying to diagnose faults in flight. So far, I've taken his latter view on board -- make a nice simple electric scheme, and then if things go awry, switch to e-bus. I then know I have n hours of time to run a few essential items -- more than enough to get on the ground, and most probably get to my home airfield. The scheme, incidentally, is Z11. Consequently, I haven't installed an ammeter or voltmeter. After all, the LV warning's going to flash away pretty soon, should the alternator pack up. Is this approach a good one? It makes sense to me, a daytime-VFR-for-the-foreseeable-future pilot, not to be trying to fathom electrical problems in-flight. Am I missing something though? Any thoughts you might have on the subject would be greatly appreciated. Thanks in anticipation, James


    Message 2


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    Time: 05:40:45 AM PST US
    From: "mike gamble" <mp.gamble@talktalk.net>
    Subject: Europa electrics
    Europa xs +912s. (Preparing for first engine start) Wired up and powered by 12v external source I select master on and note 12 volts on the meter. I then select alternator on and nothing happens. Should I not get an alt warning light in this situation with regulator providing an earth return to the warning light? I do have 12v at the C terminal and at the +ve side of the capacitor. Comments please. Mike G-CFMP


    Message 3


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    Time: 05:55:51 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Ammeter, voltmeter and other diagnostics
    In reading the AC, it's clear that an ammeter is a useful diagnostic tool on board the aeroplane, and yet at the same time, Bob's often espousing the virtues of not trying to diagnose faults in flight. So far, I've taken his latter view on board -- make a nice simple electric scheme, and then if things go awry, switch to e-bus. I then know I have n hours of time to run a few essential items -- more than enough to get on the ground, and most probably get to my home airfield. The scheme, incidentally, is Z11. Consequently, I haven't installed an ammeter or voltmeter. After all, the LV warning's going to flash away pretty soon, should the alternator pack up. Is this approach a good one? It makes sense to me, a daytime-VFR-for-the-foreseeable-future pilot, not to be trying to fathom electrical problems in-flight. Am I missing something though? Any thoughts you might have on the subject would be greatly appreciated. Sure. But only because you've taken the time to study, understand, and craft a process by which you're going to build, operate and maintain your airplane. Instruments are for telling you things you do not know or have not planned for. Limiting your in-flight accessibility to real-time amps and volts is a perfectly rational design goal when the system is failure tolerant and backed up with a battery of known endurance. Confidence is a great mitigator of uncertainty. Bob . . .


    Message 4


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    Time: 06:41:46 AM PST US
    From: Larry McFarland <larry@macsmachine.com>
    Subject: Flying on the edge of wetness
    Hi Guys, I fly mostly good weather, but theres been a few times Ive had to fly thru light showers to get home. The greater concern is getting into too much rain. Id think this was possible, but a few of our Chapter 75 have flown in a car wash type rain that put them on the gages for a few minutes. Does anyone know the limits of the ignition system wires and spark plugs? I fly the Stratus Subaru in my 601 and am just now looking at my plugs and wires and wondering if theres much difference between wet aircraft plugs and mine. Anyone knowledgeable? Larry McFarland 601HDS at www.macsmachine.com


    Message 5


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    Time: 08:51:14 AM PST US
    Subject: wireing a ICOM A 210 with a Flightcom 403MC
    From: "gordon" <gptailwind@msn.com>
    Has any one had success wireing up a new ICOM A 210 with a Flightcom 403 voice activated intercom? After reading some of the problems posted last July and some having problems with the intercom function of the radio I have decided I would like to use my Flightcom that worked fine with my Val 760. The Val gave me so much trouble over about 6 years that I removed it for the ICOM. Sure would apprecite any suggestions on wireing them together. Thanks Gordon -------- tailwind10 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=299869#299869


    Message 6


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    Time: 11:09:00 AM PST US
    From: "earl_schroeder@juno.com" <earl_schroeder@juno.com>
    Subject: Re: Ammeter, voltmeter and other diagnostics
    >---------- Original Message ---------- >From: James Kilford <james@etravel.org> >In reading the AC, it's clear that an ammeter is a useful diagnostic >tool onboard the aeroplane, and yet at the same time, Bob's often >espousing the virtues of not trying to diagnose faults in flight. >Consequently, I haven't installed an ammeter or voltmeter. >Is this approach a good one? I do have ammeters and use them for cross checking my tired memory. For instance, if I neglect to turn off the boost pump, landing light etc when my cross check scan gets to the ammeter, I notice a higher than normal current consumption which (from experience) shifts my attention to the forgotten item. I can usually tell by the indicated draw which item needs attention. A small relay in parallel with the starter solenoid switch opens the meter circuit when starting. BTW, my ammeter is a sensitive analog voltmeter (50 millivolt FS) connected across the heavy wire from the alternator to the bus. (fuse protected and sizing resistor - with the idea borrowed a Jim Weir's forum at Oshkosh) I have another across the heavy wire from the battery which should be zero (actually below) during flight and an operating alternator.. neither of these are calibrated and used only for reference. A black mark on the scale near 'normal' is easily used for a verifying glance as the mark 'hides' the red meter pointer. I use the same meters for CHT, EGT, fuel press etc with the black marks allowing control-by-deviation. This phrase borrowed from Fisher controls I used at GE Plastics years ago.. That said, I agree that trouble shooting is best left to ground bound vehicles. do not archive Earl


    Message 7


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    Time: 01:10:08 PM PST US
    From: "mike gamble" <mp.gamble@talktalk.net>
    Subject: Europa electrics
    Europa xs +912s. (Preparing for first engine start) Wired up and powered by 12v external source I select master on and note 12 volts on the meter. I then select alternator on and nothing happens. Should I not get an alt warning light in this situation with regulator providing an earth return? I do have 12v at the C terminal and at the +ve side of the capacitor. Comments please. Mike G-CFMP


    Message 8


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    Time: 02:23:42 PM PST US
    Subject: Re: Long and short hot feeders
    From: "rckol" <rckol@kaehlers.com>
    John, It looks like you are going to change course here based on Bob's advice, so this information may not be needed but, I noticed yesterday that SteinAir is selling bus bar/terminal strips with 10 terminals each on them that could probably be used to feed your fuse holders, if they were located in close proximity to your fuse holders. http://www.steinair.com/strips.htm -------- rck Read this topic online here: http://forums.matronics.com/viewtopic.php?p=299921#299921


    Message 9


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    Time: 04:52:06 PM PST US
    Subject: Re: Europa electrics
    From: "rampil" <ira.rampil@gmail.com>
    Mike, You have not described how your Europa is wired, and especially where and how you have an "Alt Warning Lamp" set up. Is your aircraft wired per Kirbymoorside, or per an Aeroelectric scheme? Have you wired a lamp to the regulator terminal for just such a lamp or is the warning to be driven from elsewhere? Did you use an LED or an incandescent lamp? Ira A224 flying 6 years -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=299943#299943


    Message 10


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    Time: 04:52:07 PM PST US
    Subject: Re: Europa electrics
    From: "rampil" <ira.rampil@gmail.com>
    Mike, You have not described how your Europa is wired, and especially where and how you have an "Alt Warning Lamp" set up. Is your aircraft wired per Kirbymoorside, or per an Aeroelectric scheme? Have you wired a lamp to the regulator terminal for just such a lamp or is the warning to be driven from elsewhere? Did you use an LED or an incandescent lamp? Ira A224 flying 6 years -------- Ira N224XS Read this topic online here: http://forums.matronics.com/viewtopic.php?p=299944#299944


    Message 11


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    Time: 05:40:05 PM PST US
    Subject: Wires going to CB question
    From: "rparigoris" <rparigor@suffolk.lib.ny.us>
    Reading "The Aeroelectric Connection" Chapter on Circuit Protection, stated is to not use the Circuit Breaker screws that mounts to bus to also connect inter-bus jumpers or main power feed lines. "These things should get their own 8-32 fasteners." I have 2 question: 1) I have a mini e-bus on passenger headrest that will never see more than 15 amps. It consists of 3 P+B CBs. Can I feed this bus with ring terminal under the head of one of the CB screws that mounts to the bus? 2) I need to take off a wire from this e-bus that will immediately go to a 2 amp in line fuse to power my variometer, can I take power off e-bus through a ring terminal under the head of one of the CB screws that mounts to the bus? This goes against what is stated in AC, but I am thinking perhaps it was stated considering there may be more amps than 10 or 1. Bus bar is silver plated copper. Thx. Ron Parigoris Read this topic online here: http://forums.matronics.com/viewtopic.php?p=299951#299951


    Message 12


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    Time: 06:33:34 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Flying on the edge of wetness
    At 08:18 AM 6/3/2010, you wrote: ><larry@macsmachine.com> > >Hi Guys, > >I fly mostly good weather, but there's been a few times I've had to >fly thru light showers to get home. The greater concern is getting >into too much rain. I'd think this was possible, but a few of our >Chapter 75 have flown in a "car wash" type rain that put them on the >gages for a few minutes. Does anyone know the limits of the ignition >system wires and spark plugs? I fly the Stratus Subaru in my 601 and >am just now looking at my plugs and wires and wondering if there's >much difference between wet aircraft plugs and mine. Anyone knowledgeable? My 'test for condition' for refurbishment of the ignition wiring and distributor cap on by '59 Chevy was to go into the car wash and clean the engine with high pressure soapy water followed by a good rinse . . . and don't spare the wiring. Get down around plugs real good too. When things were as they should be, I could close the hood, hop in and smoothly drive away. That would have been in 1965 or so. My sense is that if your wiring is still "flexible" meaning that the seal between boots and the objects they cover is good, the wiring will be exceedingly resistant to the effects of accelerated rain drops. That doesn't mean that OTHER engine accessories are equally rain resistant . . . but I think your ignition wires are the least of your concerns. Bob . . .


    Message 13


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    Time: 06:50:23 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Long and short hot feeders
    At 04:21 PM 6/3/2010, you wrote: > >John, > >It looks like you are going to change course here based on Bob's >advice, so this information may not be needed but, I noticed >yesterday that SteinAir is selling bus bar/terminal strips with 10 >terminals each on them that could probably be used to feed your fuse >holders, if they were located in close proximity to your fuse holders. > >http://www.steinair.com/strips.htm Hmmmm . . . I cannot imagine where those would be used. Further, they feature non-locking, threaded fasteners. When such devices are called for in TC aircraft (rarely) they look more like this . . . http://aeroelectric.com/Pictures/Wiring_Technique/Terminal_Strip_Captive_Stud.jpg Note the captive treaded studs with LOCKING hardware. I need to go back and look up that installation in the wire books. In the picture above we see a mix of wire guages which makes me wonder if it's a ground bus. Otherwise, one would be hard pressed to provide appropriate fuse/breaker protection for the wires serviced by the bus. In any case, if one truly needs such a bus, then drill and tap a copper bar for at least 8-32 (10-32 better) screws. Thread in from back side and captivate screws to bus bar with JB weld under head of screws and last few threads under head. Torque well. Terminal faces on wires go right against the bar and against each other on the stud side. Cap of with a flat washer and well torqued locking nut. If you need to insulate the assembly from ground, then some work on a saw and drill press will carve out a piece of phenolic, delrin, lexan or perhaps even some cutting board stock. Bob . . .


    Message 14


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    Time: 06:57:57 PM PST US
    Subject: labeling panel
    From: bob noffs <icubob@gmail.com>
    hi all, i am ready to label switches etc. on my grey panel. i am using white letters on a clear tape. what works best to keep the tapes ''level''? masking tape or a light pencil mark maybe? how far below the switch as a rule of thumb? and the best way to remove the pencil line if that is the way to go? any info appreciated. bob noffs


    Message 15


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    Time: 08:24:38 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Wires going to CB question
    At 07:38 PM 6/3/2010, you wrote: ><rparigor@suffolk.lib.ny.us> > >Reading "The Aeroelectric Connection" Chapter on Circuit Protection, >stated is to not use the Circuit Breaker screws that mounts to bus >to also connect inter-bus jumpers or main power feed lines. "These >things should get their own 8-32 fasteners." > >I have 2 question: >1) I have a mini e-bus on passenger headrest that will never see >more than 15 amps. It consists of 3 P+B CBs. Can I feed this bus >with ring terminal under the head of one of the CB screws that >mounts to the bus? >2) I need to take off a wire from this e-bus that will immediately >go to a 2 amp in line fuse to power my variometer, can I take power >off e-bus through a ring terminal under the head of one of the CB >screws that mounts to the bus? > >This goes against what is stated in AC, but I am thinking perhaps it >was stated considering there may be more amps than 10 or 1. > >Bus bar is silver plated copper. The idea for a bus bar is to offer contiguous electrical connection from some feeder to an array of tap-offs that feed breakers or fuses using techniques that minimize single points of failure. This design goal suggests that if you can stamp or otherwise fabricate a bus from a single piece of metal, the design goal is met. When the "bus" is two rows, then some means for inter connection the rows must be devised. Certainly, strapping between the rows with a similar piece of metal - each end enjoying a SOLID connection (solder, steel fastener with locking hardware, etc. then the design goal has been faithfully observed. Having said that, we can peek behind the breaker panel on a contemporary A36 Bonanza and see this: http://aeroelectric.com/Pictures/Breakers/Breaker_Panel_Busing_1.jpg http://aeroelectric.com/Pictures/Breakers/Breaker_Panel_Busing_2.jpg . . . here we observe specially fabricated inter-bus jumpers crafted from some rather robust material fitted on each end with equally robust flags that have been hard-soldered. These particular assemblies attach with the non-locking, threaded fasteners SHARED with the upstream side of a breaker. Hmmmm . . . they've been doing this for decades . . . if it's good for an A36 it's probably good for an RV7. But it DOES offer single points of multiple failures due to loosening of non-secured fasteners. So here the design goals I cited above were not observed. At the same time, out of many thousands of aircraft involved, we've probably not heard about a situation (if any) where the loosening of one non-locking screw affected several systems. I don't know the 'chefs' who crafted this recipe for success but the risks for adopting their philosophy is demonstrably low. I cannot offer a powerful argument for observing the former design goal over that used on the A36 except that it's not hard to do and has a logical rationale for implementation based on the same rationale that drove fabrication and assembly of the terminal-strip bus discussed in an earlier posting this evening. It's your kitchen . . . Bob . . .


    Message 16


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    Time: 08:58:51 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: The state of the industry
    > >It is the attitude that counts the most! > >I sure DO NOT have an answer, but I think we aviators need to be the >ones who make the decisions, not a bunch of ivory tower sideliners. This phenomenon is present throughout most if not all technology based services and industries. There's a growing trend in belief that if you can write, administrate and enforce the right policies, then all will be right with the world. Virtually ALL the companies that offered me opportunity to grow in skill and understanding no longer avail themselves of those exact same skill-sets nurtured by an 'obsolete' business model that made my own career possible. I could not hire into Hawker-Beech as an engineer today. New policy. I CAN contract as a technical services specialist . . . at a rate considerably higher than I made there while wearing a badge that called me engineer! I think I like being a TSS better! The phenomenon is endemic to the culture. Folks in positions of power have been given or have assumed control over skill- sets they do not personally possess nor understand. Bureaucratic organized stagnation is replacing entrepreneurial spontaneous order. This is being demonstrated throughout the full spectrum of those who would call themselves leader and/or crafter of a successful business model in our nation. The counter-productive effort of elitist leadership has exerted a strangle-hold on independently self sufficient persons in many societies for hundreds of years. It's our turn in the barrel. The over worked, under trained ATP pilot has many counterparts in every industry. Unfortunately, it may require a game-changing and devastating event before it turns around . . . and only if opportunities for the truly productive are not quashed. If aviation for the ordinary citizen recovers, it will be from the efforts of folks like those on the Lists. Even the EAA, for all it's facility, programs and cash flow will have little if anything to do with a new future of aviation. If we want little airplanes to be around for our grandchildren, YOU and I and our FRIENDS are going to have to do it. > >Flame away at will my friends, but that is the way I see it! Your vision may be a scene from your worst nightmare but it's not a hallucination. The things you've observed are demonstrably common EVERYWHERE. >Happy Skies, > >Old Bob >(soloed 64 years ago this month) Younger Bob . . . (soloed on Memorial Day 29 years ago) DO NOT ARCHIVE




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