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09-20-2007, 01:02 PM
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Join Date: Apr 2007
Location: San Jose, Ca
Posts: 60
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Grounding to Airframe & corrosion
When using the airframe for ground wire return (Like the stuff on the wing tip), Does that cause more corrosion?
Grounding causes current to flow via airframe. Flow of current can encourage corrosion.
I always see a lot of corrosion around battery cables in my car. That is why I was concerned.
Ben
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09-20-2007, 01:38 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 3,954
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Use correct materials...
Not a problem if you use the correct materials for the ground connection.
Check the Electrical section in AC 43.13
However, for aluminum structures the use of cadmium plated steel hardware (standard AN hardware) is the correct procedure.
gil A
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
RV-6A VSB (Very Slow Build)
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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09-20-2007, 01:43 PM
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Join Date: Jan 2005
Posts: 3,606
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Do one better
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George McQueen
Raleigh, NC area.
RV-4, RV-7, ATP, CFII, MEI, 737/757/767
Last edited by gmcjetpilot : 09-20-2007 at 01:49 PM.
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09-21-2007, 10:08 AM
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Join Date: Feb 2007
Location: MN
Posts: 148
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George,
I really like reading your posts. If I see something you posted I always read it. Sometimes I even understand them! Thanks!
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09-22-2007, 10:52 AM
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Join Date: Mar 2007
Location: Beaverton, OR
Posts: 36
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Good question
This had never occured to me, but once you mention it I realize how obvious this is. I immediately thought of a Mythbusters episode where they used the powersupply from a small radio and some salsa to corrode away a 1 inch diameter steel bar. I believe that corrosion would be accelerated anywhere the current passes that anodic and cathodic potentials exist. The use of cadmium plated hardware for the ground hookup prevents corrosion at the attachment of the ground, however, there could/would be corrosion occuring elsewhere. I think we get away with this because the airplane, and its electronics, operate for relatively short periods of time and the corrosion that results is minimal. The real corrosion acts slowly over thousands of hours while the plane sits at its tiedown with the current for the corrosion cells generated by difference in electrochemical potental between metals. (rust never sleeps)
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RV-8A: Finished wings, working on fuselage.
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09-22-2007, 01:14 PM
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Join Date: Feb 2006
Location: East Texas
Posts: 84
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ground return
What about a ground return line to a common ground bus?
I understand this adds weight but no grounding problems
to worry about. Just an idea.
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09-22-2007, 04:39 PM
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Join Date: Sep 2006
Posts: 725
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Do Both!
Quote:
Originally Posted by marchudson
What about a ground return line to a common ground bus?
I understand this adds weight but no grounding problems
to worry about. Just an idea.
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If I were to build another plane, I would do both, ground to the airframe and a ground wire. Redundancy, and this is what Honda does on their cars, so it must be good. Most electrical problems I have seen are ground faults.
Nucleus 
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09-22-2007, 08:47 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 3,954
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Modern cars
Quote:
Originally Posted by nucleus
If I were to build another plane, I would do both, ground to the airframe and a ground wire. Redundancy, and this is what Honda does on their cars, so it must be good. Most electrical problems I have seen are ground faults.
Nucleus 
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May not be a good extrapolation. Modern cars seem to isolate body parts with rubber/sealer/shock mounts to keep things quite and stop squeaks. This might be the reason for the separate ground returns.
Most aircraft electrical problems I have seen have been broken wires and poorly made connectors...
gil A
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
RV-6A VSB (Very Slow Build)
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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09-23-2007, 02:32 AM
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Join Date: Jan 2006
Location: Belgium
Posts: 536
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Do you prime/paint?
Hello Ben,
Don’t forget that your battery is out in the wet part of the car and the acid of the battery (fumes) helps the corrosion a lot! Also the currents through the battery terminals are a lot higher than through the average ground connector of your equipment.
I am actually at the stage where I am wiring stuff in the fuselage. All my parts are primed, inside and out, before final assembly. This will obviously cause bad ground if I was using the airframe as a ground conductor. So I am running a ground wire to the center wing spar and to some other strategic places, where ground wires from various equipment (strobe power supply, AP-servo, flap motor, etc.) connect to. For all the wings-stuff, I use the wing spar for local ground, because it is anodized and is a good conductor, being bolted to the center section. So far I have not bothered with any special materials for the connections, just plated screws, nuts and washers, with standard ring terminals. As long as everything stays dry (which all these connections normally should), I guess there will be no problems for many years.
Just in case, I will put the ground connections on my “annual” check list, anyway.
Regards, PilotTonny.
__________________
"Pilottonny"
Tonny Tromp
Lanaken, Belgium (EU)
RV9A, Registration: PH-VAN
ECI-Titan IOX-320 with dual EI.
Waiting on paperwork before first flight.......
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09-23-2007, 07:27 AM
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Join Date: Oct 2005
Location: Wetumpka, AL
Posts: 2,008
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<<because it is anodized and is a good conductor>>
No....anodizing is an insulator.
__________________
Dan Horton
RV-8 QB - Alabama
Barrett IO-390
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