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3 Cards in this Set
- Front
- Back
- 3rd side (hint)
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The elevator control system(a primary flight control) is |
A hydro electromechanical system that provides longitudinal control of the aircraft |
Elevator control |
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Two elevators on the trailing edge of the fixed horizontal stabilizer, are actuated by a |
Hydraulic elevator actuator |
Elevator control system |
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The flap may be actuated to 4 positions; 0 deg (retracted) 10 deg (on-station loiter) 20 deg down (wing fold) |
30 deg down (takeoff and landing). |
Flap and aileron droop system |
