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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 |
---|---|---|---|---|
SPE4A717T4044 | Spar, Aircraft | 3 | EA | 12/23/2016 |
SPE4A719T6852 | Spar, Aircraft | 1 | EA | 01/07/2019 |
SPE4A719T6853 | Spar, Aircraft | 2 | EA | 01/07/2019 |
SPE4A719T287T | Spar, Aircraft | 1 | EA | 06/10/2019 |
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