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A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.
Solicitation | Description | Qty | UOM | Close Date |
---|---|---|---|---|
SPE4A718T3748 | Spar, Aircraft | 9 | EA | 11/20/2017 |
SPE4A719T480U | Spar, Aircraft | 2 | EA | 08/19/2019 |
SPE4A720T2615 | Spar, Aircraft | 1 | EA | 12/03/2019 |
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