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CPL Acft Tech - Pressure instruments

Total questions: 20

Worksheet time: 10mins

Name
Class
Date
1.

Static air pressure is...

a)

the amount of pressure exerted by a fluid that is not flowing

b)

only the weight of air pushing upwards

c)

only the weight of air pushing downwards

d)

only the weight of air pushing sideways

2.

Dynamic pressure is...

a)

pressure due to movement of air

b)

pressure due to movement of electrons independent of an electrical field

c)

pressure exerted on an object by air when in a perfect vacuum

d)

pressure that is constantly changing

3.

The pressure measured or collected by a pitot probe consists of..

a)

static and dynamic pressure

b)

dynamic pressure

c)

static pressure

d)

ambient pressure

4.

The airspeed indicator requires...

a)

GPS to work

b)

dynamic and static pressure to work

c)

dynamic pressure only to work

d)

static pressure only to work

e)

dynamic and static pressure, and GPS to work

5.

The vertical speed indicator requires...

a)

GPS to work

b)

dynamic and static pressure to work

c)

dynamic pressure only to work

d)

static pressure only to work

e)

dynamic and static pressure, and GPS to work

6.

The altimeter requires...

a)

GPS to work

b)

dynamic and static pressure to work

c)

dynamic pressure only to work

d)

static pressure only to work

e)

dynamic and static pressure, and GPS to work

7.

Pitot heat is used to...

a)

remove any water from the air entering the pitot tube

b)

remove any water from the air entering the static vent

c)

prevent or remove any ice from the pitot head

d)

remove any ice from the static air pressure system

8.

Looking at the Christchurch ATIS in the picture, what is the density altitude?

a)

1733 feet

b)

1610 feet

c)

803 feet

d)

1033 feet

9.

Compressibility error causes...

a)

the airspeed indicator to over read

b)

the airspeed indicator to under read

c)

the altimeter to under read

d)

the altimeter to over read

10.

As you increase altitude in an aircraft...

a)

TAS increases relative to IAS due to air density

b)

IAS increases relative to TAS due to air density

c)

TAS increases relative to IAS due to air instrument error

d)

IAS increases relative to TAS due to air instrument error

11.

You are flying an aircraft with suction driven instruments. During flight, the static vent becomes blocked.


Select all instruments which will be affected?

a)

Altimeter

b)

Airspeed Indicator

c)

Direction Indicator

d)

Balance ball

e)

Turn coordinator

12.

You are flying from Dunedin to Christchurch. At Dunedin the QNH is 1015 and temperature +11 degrees Celsius. At Christchurch it is 1020 and +12 degrees Celsius.


Which statement is true?

a)

If you fly from Dunedin to Christchurch without changing your QNH, your altimeter will under read

b)

If you fly from Dunedin to Christchurch without changing your QNH, your altimeter will over read

c)

The QNH change will balance out the temperature change

d)

The temperature change will balance out the QNH change

13.

Position error is a well known error regarding the...

a)

Vertical Speed Indicator, Altimeter and Airpeed Indicator

b)

Vertical Speed Indicator only

c)

Altimeter only

d)

Airspeed Indicator only

14.

You are flying south from point A (in the north) to point B (in the south). At point A, the temperature is 15 degrees Celsius and QNH is 1010 hPa. At point B, the temperature is 21 degrees Celsius and QNH is 1010 hPa. Which statement is correct?

a)

Air density at the destination is lower than at the origin

b)

Air density at the origin is lower than at the destination

c)

Density altitude is the same at both A and B

d)

Pressure altitude is the same at both A and B

15.

Climbing through 6000 feet, you pitot tube becomes blocked due to icing but your static vent remains clear.


Select all instruments which will be affected.

a)

Altimeter

b)

Airspeed Indicator

c)

Vertical Speed Indicator

d)

Direction Indicator

e)

Manifold Air Pressure gauge

16.

Select the correct tolerances for an altimeter.


Select both a positive and a negative value

a)

+30 feet

b)

- 45 feet

c)

+ 60 feet

d)

+ 45 feet

e)

- 30 feet

17.

A Vertical Speed Indicator uses what device as part of the internal mechanism?

a)

Metering unit

b)

Bourdon tube

c)

Pitot tube

d)

Gyroscope

18.

A Vertical Speed Indicator is considered serviceable if, within a temperature range of -20o to +50o Celsius, it is accurate to within...

a)

+ or - 200 feet per minute

b)

+ or - 100 feet per minute

c)

+ or - 300 feet per minute

d)

+ or - 50 feet per minute

19.

On an airspeed indicator what does the bottom of the green band indicate?

a)

Stalling speed with landing gear and flaps up, and power off

b)

Stalling speed with landing gear and flaps down, and power off

c)

The maximum speed for flight in smooth air

d)

Maximum flap extension speed

20.

On the take off role you notice that the Vertical Speed Indicator indicates a slight rate of climb. This is likely to be due to...

a)

airflow past the static vent causing a lower pressure

b)

airflow past the pitot tube causing a lower pressure

c)

airflow past the static vent causing a higher pressure

d)

airflow past the pitot tube causing a higher pressure