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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 |
---|---|---|---|---|
SPE4A719T140S | Spar, Aircraft | 9 | EA | 04/22/2019 |
SPE4A719T337L | Spar, Aircraft | 17 | EA | 06/20/2019 |
SPE4A720T0878 | Spar, Aircraft | 2 | EA | 10/31/2019 |
SPE4A620T214A | Spar, Aircraft | 5 | EA | 01/24/2020 |
SPE4A720T9622 | Spar, Aircraft | 5 | EA | 03/16/2020 |
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