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Questions and Answers
What is the primary means of controlling the stabilator?
How is pitch trim control provided for the stabilator?
Where is the stabilator trim control typically located?
What component moves the pushrod that controls the stabilator trim tab?
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What is the optional installation for trim control mentioned?
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Study Notes
Stabilator Operation
- Operated via movement of the control column-tee bar assembly for pitch control.
- Cable connects the tee bar assembly's bottom to an aft fuselage bellcrank, which in turn controls pitch via a pushrod.
Pitch Trim Control
- Adjustable trim mechanism specifically designed for the stabilator enhances flight stability.
- Trim control can be operated using a wheel and drum system located in the floor tunnel between the front seats.
- Optional S-TEC Manual Electric Trim Control can be installed on the control yoke for trim adjustments.
Mechanism and Routing
- Cables are routed from the trim drum aft towards a screw assembly situated above the stabilator attachment point.
- The screw assembly operates to move the pushrod, which ultimately adjusts the stabilator trim tab for fine-tuning pitch control.
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Description
Test your knowledge on stabilator control mechanisms in aerodynamics. This quiz covers the operation of the control column-tee bar assembly, cable connections, and pitch trim control for the stabilator. Explore how these elements contribute to aircraft performance and stability.
