WorksheetsUnderstanding the Pitot Static System
Total questions: 14
Worksheet time: 7mins
What is the primary function of the pitot-static system in an aircraft?
To measure fuel levels
To provide information to basic flight instruments
To control the aircraft's engine
To manage the aircraft's navigation system
Which of the following instruments relies on air pressure for its readings?
Attitude Indicator
Heading Indicator
Altimeter
Turn Coordinator
What are the three types of air pressure involved in the pitot-static system?
Static, Dynamic, and Total Pressure
Atmospheric, Hydraulic, and Pneumatic Pressure
Static, Kinetic, and Potential Pressure
Dynamic, Hydraulic, and Total Pressure
What is static pressure also known as?
Dynamic Pressure
Atmospheric Pressure
Total Pressure
Kinetic Pressure
How does static pressure change with altitude?
It increases with altitude
It remains constant
It decreases with altitude
It fluctuates randomly
What does dynamic pressure depend on?
Altitude and temperature
Speed and air density
Humidity and wind direction
Aircraft weight and balance
What is total pressure also known as?
Static Pressure
Dynamic Pressure
Pitot Pressure
Atmospheric Pressure
Which instrument is fed by both the pitot tube and the static port?
Altimeter
Vertical Speed Indicator
Airspeed Indicator
Attitude Indicator
Where is the pitot tube typically located on small aircraft?
Under the wings
On the tail
Inside the cockpit
On the landing gear
What is the purpose of the heating system in a pitot tube?
To increase airspeed
To prevent icing
To reduce drag
To improve fuel efficiency
What is the function of the drain hole in a pitot tube?
To measure airspeed
To remove water from the system
To increase static pressure
To decrease dynamic pressure
What happens to static pressure as you climb a mountain?
It increases
It remains the same
It decreases
It fluctuates
What is the relationship between static pressure and altitude increase?
Static pressure increases by 1 inch of mercury for every 1000 feet
Static pressure decreases by 1 inch of mercury for every 1000 feet
Static pressure remains constant regardless of altitude
Static pressure fluctuates randomly with altitude
Which component of the pitot-static system is primarily responsible for measuring airspeed?
Static port
Altimeter
Pitot tube
Vertical Speed Indicator
