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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 |
---|---|---|---|---|
SPE4A517TB248 | Spar, Aircraft | 3 | EA | 12/23/2016 |
SPE4A518T4839 | Spar, Aircraft | 3 | EA | 11/13/2017 |
SPE4A519T7422 | Spar, Aircraft | 3 | EA | 12/17/2018 |
SPE4A519T612E | Spar, Aircraft | 1 | EA | 07/15/2019 |
SPE4A520T8544 | Spar, Aircraft | 3 | EA | 02/10/2020 |
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