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On Sep 19, 5:31 am, Bob Noel
wrote: In article .com, Le Chaud Lapin wrote: Hi All, [snip]] and cost difference should be huge . [Yes, I know, reliability, FAA certification...yada...] You say you know about reliability, etc. But do you really know what it takes to do the safety analysis? Nope. I just know that it will be a fixed cost. My guess is that it would be under $100,000,000. If so, then those costs would be recuperated. What are the failure modes of these components? Same as for most pieces of software and hardware. ![]() How will failures and errors be detected and handled? Self-checking, pre-flight, and during flight, redundancy, etc. How will component changes be handled? With more professionalism than the free pop-up blockers, for example. The first time a plane crashes due to a company's gross oversight (read, bad engineering), they would get license revoked by FAA. Also, the components would still have to be checked. How much will it cost to repeat the appropriate analyses when various vendors roll part numbers? Dunno...I think this is the crux of the issue. The existing older components are well understood and familiar. 5,000 lines of C code is not as familiar. How will you determine that the part hasn't changed when the vendor didn't change the part number? Abstraction barrier. The component would have to comform to specification. After that, they can changes as they wish. (Don't laugh, I've seen an LRU no longer work in a particular aircraft when a chipset vendor changed a production process which ever so slightly changed functionality but the vendor didn't change the part number). And do you have any concept of what it would take to put a commodity OS like windows into a safety-critical application? From a technical point of view, I guess, yes. From a "How much must I pay the FAA and fight political fall-out" point of view, no. -Le Chaud Lapin- |
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Thread | Thread Starter | Forum | Replies | Last Post |
Cockpit instruments | T L Jones | Restoration | 0 | November 19th 03 08:40 PM |