| http://www.w3.org/ns/prov#value | - These implementations are merely exemplary, and other implementations may also be used. [0107] In one implementation, the components of forward cabin area spar forming tooling 437, aft cabin area spar forming tooling 439, and middle insert section 441 are constructed of aluminum, nickel alloys, or Invar, or they may be constructed of non-metallic materials.
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