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Questions and Answers
What does the pitot air system primarily measure?
What consequence can result from a blocked pitot head?
What is the function of the static air system?
Where is the alternate static air source located?
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What is the role of the drain valves in the pitot and static systems?
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Study Notes
Pitot Air System
- Comprises a pitot mast located underneath the left wing, along with associated plumbing.
- Impact air pressure enters through the pitot inlet and travels via hose and tubing to the airspeed indicator on the instrument panel.
- Can also connect to the Avidyne Entegra PFD or Garmin Air Data Computer for enhanced displays.
- Partial or complete blockage of the pitot head leads to erratic readings or zero instrument values.
Static Air System
- Features a static port on the underside of the pitot-static mast.
- The static port connects to the airspeed indicator, altimeter, and vertical speed indicator through hose and tubing.
- If installed, also connects to the Avidyne Entegra PFD or Garmin Air Data Computer.
- Equipped with an alternate static air source below the instrument panel; includes a shutoff valve to control usage.
Drainage System
- Pitot and static lines are drained separately using designated drain valves.
- Located on the left lower side of the fuselage interior to facilitate maintenance and safety.
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Description
Test your knowledge on the pitot and static air systems essential for aviation. This quiz covers the components, functions, and implications of blockages in these systems. Perfect for aviation students and enthusiasts learning about aircraft instrumentations.
