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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 |
---|---|---|---|---|
SPE4A716T1212 | Spar, Aircraft | 5 | EA | 10/26/2015 |
SPE4A717T2529 | Spar, Aircraft | 3 | EA | 11/14/2016 |
SPE4A719T9824 | Spar, Aircraft | 6 | EA | 03/18/2019 |
SPE4A719Q1975 | Spar, Aircraft | 6 | EA | 11/04/2019 |
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