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Question 1: Why is "System Redundancy" critical in avionics systems, particularly for safety-critical components?

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Question 2: During the testing of a transponder system, what is the correct procedure to verify that it is functioning correctly?

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Question 3: When diagnosing and repairing a malfunction in an aircraft's primary flight display, what is the most common issue?

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Question 4: Which of the following is required for avionics system safety compliance during repair work?

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Question 5: When installing a new aircraft transponder, what should be tested to ensure proper operation?

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Question 6: When diagnosing a failure in the aircraft's communication system, what should be the first thing to check?

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