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Questions and Answers
The pitch trim stabilizer moves at a rate of 0.4 degrees per second in the direction commanded.
True
In the Cruise sub-mode, the FCS will be in Cruise sub-mode when the On-ground sub-mode logic is satisfied.
False
Pitch response is designed to be conventional without any additional damping.
False
Elevator movement is augmented with sensor feedback to provide a more inconsistent response to column input.
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The aircraft provides protection against exceeding the maximum mach number.
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Wheel deflection commands aileron and roll-spoiler deflection in Roll Control.
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The aircraft can only enter Maintenance mode if the aircraft is moving on the ground with the landing gear up.
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Pitch trim at nose down limit is a cautionary advisory in the operating manual.
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In the event of pitch control miscompare, the pilot and copilot control column positions are different.
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Approaching maximum displacement of pitch axis flight control surfaces is a cause for caution according to the operating manual.
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There are limitations established for the elevator control system according to the provided data.
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Both MLG WOW must be false for the FCC to enter Maintenance mode.
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During normal maneuvering, the entry threshold for AOA limiting sub-mode is approximately 0.88-0.93 normalized AOA regardless of airspeed deceleration rate.
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An abrupt nose up control input can trigger the entry into the AOA limiting sub-mode at any normalized angle of attack.
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If the aircraft touches down while in AOA limiting mode, it will transition to takeoff sub-mode.
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Full aft column input results in the aircraft reaching a maximum allowed angle of attack of approximately 0.96 normalized AOA.
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Reducing the angle of attack will keep the aircraft in the AOA limiting mode.
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The FCC AOA Limiting advisory CAS message will be displayed along with Stall Protection Active caution CAS message when the AOA is near its limit value of 0.96.
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