Q. What is the position accuracy that can be achieved by satellite guidance systems?

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Q. What is the beam error in localizer for aircraft CG displacement of 5 m at a range of 1,500m?

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Q. The guidance sensitivity decreases as the range decreases.

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Q. When does an ILS localizer coupling loop become unstable?

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Q. What is missing in the localizer coupling loop?

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Q. Which one of the following is not a basic parameter used to define visibility category?

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Q. Which of the following is not one of the operational limits and autopilot requirement for a category IIIc visibility condition?

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Q. How is altitude measured when the aircraft is about to land?

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Q. Why is flare maneuver executed during landing phase?

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Q. Why is the kick off drift maneuver executed?

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Q. What is HREF in the control law used for auto flare?

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Q. The final approach path in a satellite landing guidance can be curved

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Q. What controls the efficient functioning of an engine?

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Q. The response of a jet engine thrust to the throttle angle is instantaneous.

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Q. Which one of the following is not a function of the FMS?

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Q. The number of independent FMS in a typical commercial aircraft is?

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Q. Which of the following is not a way cockpit-flight crew interfaces in the FMS?

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Q. What type of cockpit flight crew interface is used to enter or modify the data on the MFD?

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Q. What control does the EFIS Control Panel provide?

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Q. What is the number of Flight Management Computers used in a typical commercial aircraft?

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