Kolb-Archive.digest.vol-ao
April 01, 1998 - April 23, 1998
FOR WHAT IT'S WORTHAC43.13-1A Change 3 specifically recommends AGAINST soldered fittings in an aircraft. Listed reasons in Paragraph 450 are;1. more skilled operator is required (not really a problem in my mind, we'll all take the time to do it right.)2. A corrosive flux may be used causing the joint to deteriorate. (if deterioration is inside coupling, etc, it's very hard to see on inspection and have you ever tried to solder with fluxless solder? See NO. 1)3. Maintenance is extremely difficult. (true)4. the wire strands are stiffened by the solder and become more susceptible to breakage due to vibration.(VERY TRUE)5. the wire insulation may be charred (and made brittle) during the soldering process.PERSONAL THOUGHT: Having soldered connections in the past in a number of applications in cars, trucks, motor cycles, trailers, etc, I would not do so in an aircraft. The biggest problem I've experienced is corrosion with breakage running 2nd. Even if the wire and parts are thoroughly cleaned and soldered with no flux, it seems as if any moisture (even inside where it is not exposed to weather) will cause corrosion over the long run.Also, why make the soldered joint any stronger than the wire itself. It needs only to be AS strong as the wire.Tom King124 King Dome Road
Our name is King, our house is a Dome, and it's OUR road!