Free ATPL Questions & Answers Practice Test

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Question ID: 108001

The wind direction and velocity (° / kts) at 40° N 040° E is

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A

300/75

B

330/75

C

150/75

D

330/85

Explanation

See attached image to locate the area on the map

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Question ID: 107997

5.

Which best describes the maximum intensity of CAT, if any, forecast for FL330 over BENGHAZI (32° N 020° E)?

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A

Severe.

B

Moderate.

C

Nil.

D

Light.

Explanation

CAT area 1 is overhead of Benghazi. Check the FLs that are affected in the box on the left. FL330 is below the affected FLs

Explanation Provided by James Le Cuirot

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Question ID: 107996

5.At position 38° N 15° E what is the worst hazard which could be expected?

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A

Nil.

B

Engine flame-out and windscreen damage.

C

Reduced visibilty.

D

Turbulence.

Explanation

Volcanic Ash from Mount Etna.

Explanation Provided by Callum Jagger

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Question ID: 107992

5.

Which best describes the significant cloud, if any, forecast for the area southwest of BODO (67° N 014° E)?

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A

Nil.

B

5 to 7 oktas CU and CB base FL100, tops FL180.

C

3 to 7 oktas CU and CB base below FL100, tops FL180.

D

5 to 7 oktas CU and CB base below FL100, tops FL180.

Explanation

BKN = 5-7 Oktas. and CU CB clearly stated in the information box overhead Bodø, and "180" means that the clouds tops are at FL180.
The clue for solving this question is understanding what "XXX" means.
XXX means that the clouds base is below the area that the chart is covering - in other words, below FL100. As you can see in the big information box in the top left corner, the chart is valid between FL100 and FL450.

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Question ID: 106152

An aircraft is flying at an indicated altitude of 16 000 ft. The outside air temperature is -30 ° C. What is the true altitude of the aircraft?

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A

13 500 ft

B

15 200 ft

C

18 600 ft

D

16 200 ft

Explanation

Work out ISA deviation - here it is -13°C

Altitude correction = (pressure alt ÷ 1000) × 4 × ISA

This gives 832ft.

As it is colder than ISA, our true altitude is going to be lower and so we minus the correction.

16,000 - 832 = 15,168ft

Round to nearest 100 gives 15,200ft.

Explanation Provided by James Le Cuirot

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Question ID: 106151

The altitude indicated on board an aircraft flying in an atmosphere where all atmosphere layers below the aircraft are warm is

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A

higher than the real altitude.

B

the same as the real altitude.

C

lower than the real altitude.

D

equal to the standard altitude.

Explanation

When it's warm, the isobars will expand. Therefor your aircraft will think it is lower than it actually is.
(see image)
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Question ID: 106129

When flying with an indicated altitude of 3 000 ft into a low pressure area, the actual altitude

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A

will increase.

B

will be as before entering a low-pressure area.

C

will decrease.

D

will be the same as indicated altitude.

Explanation

High to low, watch out below - you will actually be descending

Explanation Provided by James Le Cuirot

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Question ID: 104477

The volcano alert code used in field E of an ASHTAM is

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A

ID number code.

B

a number and the ID of the volcano.

C

a colour code.

D

a colour code & ID.

Explanation

See an example attahced ASHTAM

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Question ID: 104166

In the standard atmosphere FL150 is equivalent to

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A

15 000 m

B

455 m

C

6 100 m

D

4 550 m

Explanation

FL150 in standard atmosphere = 15,000FT

15000/3.28(The diver for meters to feet) = 4572M

Rounded is 4500M
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Question ID: 104156

A pre-flight altimeter check should be carried out

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A

at the holding point.

B

at a known elevation on the aerodrome.

C

on the apron.

D

on the manoeuvring area.

Explanation

For you to check the consistency of your altimeter, it will be a smart idea to carry out a check on a place where you know the elevation. This way, you can check what the altimeter says, and further on figure out the error.

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