When aligning an aircraft for a compass swing, the maximum allowable error is
- 1 degrees.
- 3 degrees.
- 5 degrees.
Explanation
When positioning an aircraft on each cardinal heading for a compass swing, the heading need only be set within a tolerance, the maximum allowable alignment error being about 5 degrees. Greater precision is unnecessary because the swing procedure averages the readings, but the aircraft must still be reasonably close to the intended heading.
Edigno92 asking:
Why?
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