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A control designed for use with automatic pilots and/or remote attitude indicators consisting primarily of a gyroscope which provides signals for controlling an aircraft about its lateral and longitudinal axis and/or signals for providing a visual presentation of attitude to the pilot.
Solicitation | Description | Qty | UOM | Close Date |
---|---|---|---|---|
SPE4A518T867J | Control, Gyroscope, A | 2 | EA | 07/16/2018 |
SPE4A518T02Q2 | Control, Gyroscope, A | 3 | EA | 08/20/2018 |
SPE4A518T18T3 | Control, Gyroscope, A | 3 | EA | 10/01/2018 |
SPE4A518T31F7 | Control, Gyroscope, A | 8 | EA | 10/23/2018 |
SPE4A519T1589 | Control, Gyroscope, A | 17 | EA | 12/14/2018 |
SPE7L319T106W | Control, Gyroscope, A | 11 | EA | 04/15/2019 |
SPE7L119Q0440 | Control, Gyroscope, A | 60 | EA | 07/10/2019 |
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