Return-Path: Received: from pop.centurytel.net ([209.142.136.253]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 23 Oct 1999 12:26:49 -0400 Received: from pavilion (ppp076.pa.centurytel.net [209.142.129.218]) by pop.centurytel.net (8.9.3/8.9.3) with SMTP id LAA15733 for ; Sat, 23 Oct 1999 11:30:58 -0500 (CDT) Message-ID: <000e01bf1d74$1e67e380$da818ed1@pavilion> From: "J. N. Cameron" To: "Lancair List" Subject: Wire types for experimentals; LNCE & others Date: Sat, 23 Oct 1999 11:27:17 -0500 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Seems like there was some misinterpretation of my earlier post regarding the merits of tefzel-insulated, milspec wire vs. more ordinary types like PVC- and teflon-insulated wire. I was not advocating using PVC wire, rather thinking aloud about whether there might be an easier, more decipherable way to wire our beasts. Whenever I see an inch-thick bundle of all white wires, the electronic repairman in me cringes at the thought of trying to track anything down without color-coding or wire labelling. That said, I do appreciate the responses, and they've made me realize there was a lot I didn't know about aircraft wiring. I therefore have tried to do a bit of research, which I'll pass along in case anyone's interested. Tefzel: This is a DuPont trademark, first registered about 1969, for ethylenetetrafluoroethylene, or ETFE. It's a chemical cousin of Teflon (also a DuPont mark), but mechanically tougher and less subject to cold flow. It's supplied by DuPont in pellets or powder for various sorts of molding and extrusion processes. Depending on how it's used in fabrication and whether or not it's crosslinked, its mechanical properties can vary somewhat in the finished product. MIL-W-22759/xxx The actual text of the milspecs can be accessed at www.dscc.dla.mil/Downloads/MilSpec/Docs, and it turns out there are quite a number of variants, revisions, etc., to this one. The latest seem to be /32C and /46A, but some leftover wire I have from my ES is marked /16, which is similar, but a superseded revision, I think. Anyway, this is the applicable milspec for most of the unshielded hookup wire we use. Aircraft Spruce carry it only white, whereas my normal electronics suppy houses (Allied, Newark, Digi-Key) don't list it as either a Belden or Alpha Wire product (these are the two largest wire mfr's in the U.S., I think). Newark has a listing for Dearborn Wire & Cable, but only in black and white. Thanks to Brent Reagan for posting the EDMO number -- I'll be calling them. I also found a website for Milspec Wire & Cable Co. (www.milspecwire.com); I've e-mailed them to see if I can get a catalog, whether they sell direct, and what their minimum orders are. Coaxial & Triaxial Cable: This seems to be more problematical. The book titled "Avionics" by John Ferrara refers to RG58 as the most common type used in aircraft. Correct me if I've missed something, but all the RG58 I've found has PVC insulation. Jim McMillan suggests RG142, then further on in his post and in one or two of the others, the point is made that teflon, due to its cold-flow property, is not acceptable for use in aircraft. Well, Belden's RG-142B/U, which meets milspec MIL-C-17D, has teflon insulation (and costs about $4 per foot). Aircraft Spruce list RG-400 but gives no spec's; Newark's catalog lists Dearborn #6400 as RG-400, also with teflon (TFE) insulation ($4.18/ft). In searching for triaxial cable (to try to get really low RF loss on COM antenna wires) I've had even less luck. There is a part of MIL-C-17 that deals with triax, but the only commercially available stuff I've found is Belden's yellow-jacketed, PVC-insulated stuff. Conduit: The Lancair construction manuals say little about providing conduit, except for the wing leading edge PVC pipe. Does anyone have a good suggestion for alternate materials? Inside the fuselage, standard aluminum electrical conduit could be used, but it would add some weight. If no conduit is used, then extra precautions have to be taken to avoid chafing at each place where wire bundles go through bulkheads. Further rooting in the leftovers box came up with these items: Wire left over from Whelen strobe installation, supplied by Whelen, is marked MW13860. Anyone know what that means? Cabling supplied by S-Tec for the autopilot installation is unmarked, and in my informal flame test it appeared to be PVC insulated. A further note, or question, really: I looked at FAR 23.1365, which is under the airworthiness standards for certificated aircraft, electric cables and equipment. All its says is: "Each cable ... that would overheat in the event of circuit overload or fault must be at least flame resistant and may not emit dangerous quantities of toxic fumes." Not very informative, but probably eliminates PVC, even the "Flamarrest" treated stuff. Part 21 has to do with certification of parts, etc., but is not on-line. Does anyone know if there is more detailed info in there? Finally, I heartily agree with the comments made by several of you that the cost of wiring is not really a consideration, given the potential risk of using the wrong stuff. It is not always an easy task, however, to find out exactly what to use in a given situation, and having found out, it's not easy to locate a source. Jim Cameron, LNCE (once and future) >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html