Question: Boeing introduced the B - 7 8 7 using primary structural components made of advanced composites, which hadn't been done before. ( Primary structure up
Boeing introduced the B using primary structural components made of advanced composites, which hadn't been done before. Primary structure up to the B was made of metal. What kind of proof of the reliability of the B structure do you believe the FAA most likely required?
Lifetime reliability projections showing compliance
Convincing engineering analysis
Computerbased structural analysis
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