This is why we opted for a connector. I wanted to maximize my use of my heated and air conditioned garage at my house. When we got to the hangar I really wanted everything to be plug and play. If this was not a requirement, I'd have done home runs with a small service loop and no connectors or splices.Walt, George, Mark: thanks!
I can use these best practices now in the garage, before I move to a hangar for final assembly.
Gotta love VAF!
Rather than put more wire in a small wing root."...Sometimes it's more convenient or a more secure installation to have the service loop well upstream or downstream of where you think you might need it as long as you can "un-loop" and get enough slack where you want it."
Every connector is another potential failure point. While that may not be a big deal for something like a landing light, I didn't want to be cutting up my canbus harness, VOR antenna or pitot plumbing. Since I was going to be pulling that stuff after the wings were on anyway I did the same for all the rest of my wing wiring. I don't have any wing root connectors at all.
Unless you're using waterproof bulkhead mounted cannon plugs, it does seem to me that most of the typical connectors we see in RV style airplanes are probably more prone to failure in a wing root than if they're in a less hostile environment like tucked up under the panel or whatever. Maybe not today, but what about after 30 years of use when my not-yet-existing grandkids are flying and I get the call "papaw, the nav lights quit working."I should add that while I did a wing root connector for all the device wiring, I didn't use one for the VOR antenna. That was a home run that I completed after the wings were mounted. This was not due to a concern for the connector failing, but to try and retain the maximum signal strength from the antenna.
I will say this: the idea that connectors are more prone to failure than a solid wire is objectively true. But I also feel that builders over state this risk which is in fact immaterial. Consider the likely dozens of connectors in your avionics suite today, one more is just not a significant increase in risk. And a quality connector that is well installed, supported properly, and literally never disconnected has a chance of failure that rounds to zero.
This is why we opted for a connector. I wanted to maximize my use of my heated and air conditioned garage at my house. When we got to the hangar I really wanted everything to be plug and play. If this was not a requirement, I'd have done home runs with a small service loop and no connectors or splices.
I have the same goal- want to keep the project at home as long as possible and a quick final assembly at a future hangar some day.
For those that are experienced with this, what is the consensus/standard practice here?
- Wing has the longer wire for the connection to be made in the fuselage? (I assume this would be the cleaner/dryer environment?)
- Do you cut another fuselage hole for the wire bundle or share the hole with the aileron push tubes?
- High draw items like pitot heat, do you split the + to two different pins? (I see sources with varying claims anywhere from 5A-11A per pin capacity for 0.093" MOLEX)
- And if the 0.093" MOLEX is a sub-optimal choice, is there another connector choice that is more commonly used for wing/fuselage electrical?
Comments welcome


For the 7 you drill a hole about couple of inches from the edge of the aileron push tube hole at about the 5 o'clock position. It's on one of the prints. I imagine the 8 is similar. Fair warning; if you do it that way by the time you get it stuffed full of wire it's too small for most connectors to fit through so in that case your connector would have to be in the wing root area. or go with individual ring terminals or something like that so you can feed wire through into the fuselage one at a time.I have the same goal- want to keep the project at home as long as possible and a quick final assembly at a future hangar some day.
For those that are experienced with this, what is the consensus/standard practice here?
- Wing has the longer wire for the connection to be made in the fuselage? (I assume this would be the cleaner/dryer environment?)
- Do you cut another fuselage hole for the wire bundle or share the hole with the aileron push tubes?
- High draw items like pitot heat, do you split the + to two different pins? (I see sources with varying claims anywhere from 5A-11A per pin capacity for 0.093" MOLEX)
- And if the 0.093" MOLEX is a sub-optimal choice, is there another connector choice that is more commonly used for wing/fuselage electrical?
Comments welcome
Thanks! After I posted I did find a reference OP-11(this is for the '8 which I imagine is similar to '7), which I think is the one you are referring to? Could not find a plan reference for the pitot line into fuselage though... Also I see on some online build log pictures alternative locations were also used... Sometimes I don't know what I don't know... If anyone is cringing, feel free to speak up - always better to know before I drill the holesFor the 7 you drill a hole about couple of inches from the edge of the aileron push tube hole at about the 5 o'clock position. It's on one of the prints. I imagine the 8 is similar. Fair warning; if you do it that way by the time you get it stuffed full of wire it's too small for most connectors to fit through so in that case your connector would have to be in the wing root area. or go with individual ring terminals or something like that so you can feed wire through into the fuselage one at a time.
oops, I was remembering this wrong. I just looked and print 28 for the 7 has you enlarge a tooling hole to feed pitot & aoa lines through. I called tech support and they didn't see why I couldn't add a second hole as I described above(which is basically where you show it on the RV8 print) so that's what I did for everything else. As always, it's probably best to pick up the phone and ask for yourself because as you say, it's a lot easier than un-drilling a hole.Thanks! After I posted I did find a reference OP-11(this is for the '8 which I imagine is similar to '7), which I think is the one you are referring to? Could not find a plan reference for the pitot line into fuselage though... Also I see on some online build log pictures alternative locations were also used... Sometimes I don't know what I don't know... If anyone is cringing, let me know- always better before to know before I drill the holes
It did later occur to me that I can have a larger connector on either side of the fuselage wall, I just would have to de-pin/re-pin. After seeing @georgemohr 's bracket, I like that idea and will try do something similar...
Good luck working on that connection after the wings are installed!Our excess wire is in the fuselage.
We used the stock exit hole for the wiring harness, but supported it with an Adel clamp at that point
We did a butt splice for the high draw pitot heat wires, because they are out of spec for DSub connectors
DSub for us, but I really like Deutsche connectors from what I've seen.
View attachment 76237
Exactly. The area aft of the wing spar is impossible to access. You have about 1" between the fuse and wing skin and the aileron pushrod hole.Good luck working on that connection after the wings are installed!
My sincere hope is to never have to work on this connection againGood luck working on that connection after the wings are installed!
Hmmm, pretty sure hope is not a very good plan....My sincere hope is to never have to work on this connection again![]()
Another thing I would add is that if you spend any time in IMC or rain, that will get wet.Good luck working on that connection after the wings are installed!
Just for my own learning purposes, what happened? Was it a crimp failure or contamination/corrosion within the connection itself?“NO MOLEX CONNECTORS EVER!!
That 14 build had two separate molex connectors in the two separate wings with failures in the Molex connectors.
That's why my actual plan was to build proper support for this connector and install it well. But hey if it ever fails I'll be sure to DM you about how right you were.Hmmm, pretty sure hope is not a very good plan....
I recently did a panel job with brackets and connectors in the wing root, a lot of bad words removing that mess.That's why my actual plan was to build proper support for this connector and install it well. But hey if it ever fails I'll be sure to DM you about how right you were.
Sounds like someone did a poor job installing it. Ours took a total of 2 minutes to connect after putting the wings on, and that was only because we opted for through-studs instead of the usual dsub jackscrews.I recently did a panel job with brackets and connectors in the wing root, a lot of bad words removing that mess.
Can you remove both connectors and re-pin if you need to?Sounds like someone did a poor job installing it. Ours took a total of 2 minutes to connect after putting the wings on, and that was only because we opted for through-studs instead of the usual dsub jackscrews.
Yep, easily. There's a service loop inside the fuse, and one inside the wing.Can you remove both connectors and re-pin if you need to?
Thanks, indeed it isMaybe different on your bird, but on my 7A, the fuel sender (capacitive) is on the forward side of the wing spar.
Well, I really don’t know what caused it. In both instances I did continuity checks from the instruments to the connector. Then from the connector to the magnetometer and the roll servo. Continuity was good in all directions from the connector(s) with it unplugged. When I plugged the connector(s) back in, no continuity. At that point I pulled out my wire cutters in both instances and cut all the wires to the connector(s) and replaced the magnetometer wiring with the round d-sub connector that has a positive screw on connector. On the wiring for the roll servo, the bad connection was for the wire for the termination of the can bus. For that group of wires I used butt splices to connect all the wires running out from the fuselage to the roll servo.Just for my own learning purposes, what happened? Was it a crimp failure or contamination/corrosion within the connection itself?