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Recently, we've seen Icon go through layoffs due to production delays related to "Manufacturability". I assume this is due to their wing structure in part, but I'm curious, in general, how a company goes about designing with manufacturability in mind.

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closed as too broad by Simon, Federico, Ralph J, ymb1, SMS von der Tann Sep 10 '16 at 11:17

Please edit the question to limit it to a specific problem with enough detail to identify an adequate answer. Avoid asking multiple distinct questions at once. See the How to Ask page for help clarifying this question. If this question can be reworded to fit the rules in the help center, please edit the question.

  • $\begingroup$ this seems an engineering.se question, rather than an aviation one. $\endgroup$ – Federico Sep 10 '16 at 6:07
  • $\begingroup$ I think it's definitely aviation but rather broad. $\endgroup$ – Notts90 Sep 10 '16 at 9:13
  • $\begingroup$ Apologies guy, not attempting to drift off topic with my questions as I thought this was acceptable in this SE. I am not sure who has privileges to do this, but I personally would like general aviation engineering questions to be either explicitly on or off topic in this SE as I would not really say this is clear at aviation.stackexchange.com/help/on-topic. As home building is an activity that many aviation enthusiast take part it, I'd prefer it be on topic. $\endgroup$ – David Sep 10 '16 at 12:53
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This answer can only scratch the surface - a good answer would take you several days to read.

Manufacturability is the combination of several things which combine to

  • improve the repeatability of the finished products without much individual reworking, and
  • reduce the work hours required to produce a given component or system

under the local conditions (wage level, worker skills, energy prices, logistics etc.). This list of factors is incomplete but should give you an idea what is involved.

This is done by selecting the proper techniques (lots of jigs and molds for repeatability, the fewest amounts of parts and joints for reducing man hours) and by designing the system such that producing the components and combining them into the finished product can be done quickly and with the available workforce.

An example: When Fairchild joined up with Dornier, they planned to relocate the production of the Do-328 from Bavaria to Arizona. The production line in Germany was set up for the local workforce, and since they were highly skilled metal workers, the holes they drilled manually were straight within ±2°. In the USA, however, Fairchild could not find enough adequately trained workers, so the production line would had needed jigs for every single hand-drilled hole - and there were lots of them on the 328. The whole endeavor floundered because the production line was not designed for manufacturability under the new local conditions, and remedying this would had cost too much.

Another example would be the Tu-4. This was a Russian copy of the Boeing B-29, which the Russians had ample time to study after some landed in Eastern Siberia after attacks on Japan. But it was no cheap knock-off: The Tupolev design bureau redid the design, airframe, engines, systems and all, in metric dimensions, so standard Russian gage sizes, fasteners and tools could be used. It was re-designed for manufacturing, in other words.

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