SACAA AME Instruments Practice Questions - SACAA Aircraft Maintenance Engineer Instrument General (CAT X & W) Theoretical Knowledge Examination Exam

Where are static pressure ports typically mounted on an aircraft fuselage to minimize aerodynamic position error?

In the engine intake plenum where airflow velocity is highest Flush with the skin on both sides of the fuselage in an area of undisturbed airflow Directly behind the propeller arc on the upper nose cowling Inside the unpressurized wheel well bay

Correct Answer:

Flush with the skin on both sides of the fuselage in an area of undisturbed airflow

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