Which of the following erroneous readings is an attitude indicator that may indicate while deaccelarating?
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Pitch up attitude
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Pitch down attitude
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Turn towards right
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All of the above
B
Correct answer
Explanation
When an aircraft decelerates rapidly, the attitude indicator's gyro exhibits precession error, temporarily showing a false pitch-down indication. This occurs because the gyro mechanism responds to acceleration forces. The pilot must recognize this as an instrument error and cross-check with other instruments like the VSI and altimeter to maintain proper attitude.