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".Blueskies." wrote in message
... "abripl" wrote in message oups.com... : : I solder my connections because I do not have the correct crimping tools, : not because it is more secure... : : Did you have correct crimping tools in the past to verify they are : superior? : Yes, in the many (electrical/electronic) companies where I have worked. Excellent point, because there are wear limits and approved methods of testing connections, both for security and to verify that the correct crimper was used. When applied correctly, the result is a "cold weld", similar to that achieved in "wire wrap", rather than a gas tight seal. I haven't checked in a *long* time, and don't have reference material currently in my posession; but it stands to reason that any effective testing of the security of a termination/connection would constitute destructive testing. Therefore, if one is really dedicated to verifying that the "secure", one would need to make a number of sample connections--both before and after the actual production run for the airplane project--and make all of the appropriate measurements on the samples. A partial list of good information sources might include: Amp (for their terminals and related crimpers) Burndy (for their terminals and related crimpers) The Boeing Workmanship Manual The McDonnell-Douglas Workmanship Manual (presumably out of print) The ATA Spec. 100 Manual (There are sure to be government publications as well, but I don't know the titles) Alternatively, soldering has been used successfully for many years, but *requires* that the strain relief extend beyond the farthest point to which solder may be wicked. This nearly always means larger, heavier, and more expensive connectors and/or terminal strips. Therefore, if you are trying to "only add lightness", avoid solder! Peter |
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![]() "Peter Dohm" wrote in message . .. ".Blueskies." wrote in message ... "abripl" wrote in message oups.com... : : I solder my connections because I do not have the correct crimping tools, : not because it is more secure... : : Did you have correct crimping tools in the past to verify they are : superior? : Yes, in the many (electrical/electronic) companies where I have worked. Excellent point, because there are wear limits and approved methods of testing connections, both for security and to verify that the correct crimper was used. When applied correctly, the result is a "cold weld", similar to that achieved in "wire wrap", rather than a gas tight seal. I haven't checked in a *long* time, and don't have reference material currently in my posession; but it stands to reason that any effective testing of the security of a termination/connection would constitute destructive testing. Therefore, if one is really dedicated to verifying that the "secure", one would need to make a number of sample connections--both before and after the actual production run for the airplane project--and make all of the appropriate measurements on the samples. A partial list of good information sources might include: Amp (for their terminals and related crimpers) Burndy (for their terminals and related crimpers) The Boeing Workmanship Manual The McDonnell-Douglas Workmanship Manual (presumably out of print) The ATA Spec. 100 Manual (There are sure to be government publications as well, but I don't know the titles) Alternatively, soldering has been used successfully for many years, but *requires* that the strain relief extend beyond the farthest point to which solder may be wicked. This nearly always means larger, heavier, and more expensive connectors and/or terminal strips. Therefore, if you are trying to "only add lightness", avoid solder! Peter I see, with regret, that I neglected to include my final comment; which is: I have not been working on airplanes lately; but when I do have to make connections, I do solder for the same reason and with the same limitations that .Blueskies already cited. Peter |
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