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The Pitot-Static System: A Quick Review

Total questions: 12

Worksheet time: 7mins

Name
Class
Date
1.

Which of the following instruments interprets data from the pitot tube?

a)

Pressure Altimeter

b)

Airspeed Indicator

c)

Vertical Speed Indicator

d)

Directional Gyro (Heading Indicator)

2.

Which of the following instruments interprets data from the static pressure port?

a)

Artificial Horizon (Attitude Indicator)

b)

Airspeed Indicator

c)

Pressure Altimeter

d)

Turn Coordinator (or Turn & Slip Indicator)

e)

Vertical Speed Indicator

3.

As altitude increases, static atmospheric pressure will __________?

a)

Increase

b)

Remain the Same

c)

Decrease

d)

Increase up to 20,000 Feet, then Decrease

4.

This instrument uses a calibrated leak to measure climb/sink rate.

a)

Vertical Speed Indicator

b)

Engine Tachometer (RPM Gauge)

c)

Airspeed Indicator

d)

Pressure Altimeter

5.

Which instrument uses aneroid wafers (set to an internal pressure of 29.92 inches of mercury) to measure altitude?

a)

Airspeed Indicator

b)

Heading Bug

c)

Vertical Speed Indicator

d)

Pressure Altimeter

6.

An obstructed pitot tube will most profoundly affect which instrument?

(a)  

7.

Which instruments belong to the Pitot-Static System?

a)

Engine Tachometer (RPM Gauge)

b)

Vertical Speed Indicator

c)

Airspeed Indicator

d)

Heading Indicator (Directional Gyroscope)

e)

Pressure Altimeter

8.

If a pilot flies from an area of high pressure into an area of lower pressure without adjusting their altimeter, what will it indicate?

a)

The altimeter will indicate higher than reality.

b)

The altimeter is unaffected by changes in pressure and will indicate true.

c)

The altimeter will malfunction and indicate a fault.

d)

The altimeter will malfunction and default to a 20,000 feet indication.

e)

The altimeter will indicate lower than reality.

9.

Which of the following instruments do not belong to the Pitot-Static System?

a)

Magnetic Compass

b)

Pressure Altimeter

c)

Vertical Speed Indicator

d)

Airspeed Indicator

e)

Artificial Horizon (Attitude Indicator)

10.

True or False (?): The pressure altimeter in the Cessna 172 Skyhawk indicates the aircraft's current height above ground.

a)

TRUE

b)

FALSE

11.

Which of the following is a possible symptom of an obstructed Pitot Tube and unobstructed drain hole?

a)

The Airspeed Indicator may erroneously indicate a higher-than-normal airspeed in climbs.

b)

The Altimeter may fail and erroneously indicate zero feet.

c)

The Altimeter may fail and default to a 20,000 feet indication.

d)

The Airspeed Indicator may erroneously indicate zero knots.

12.

Which of the following is a possible symptom of an obstructed Pitot Tube and obstructed drain hole?

a)

In level flight, the Airspeed Indicator may fail to register changes in airspeed and erroneously indicate the last true airspeed.

b)

In climbs, the Airspeed Indicator may erroneously indicate an airspeed slower than normal.

c)

In climbs, the Airspeed Indicator may erroneously indicate zero knots.

d)

In descents, the Airspeed Indicator may erroneously indicate an airspeed faster than normal.

e)

In descents, the Airspeed Indicator will fail and indicate a fault.