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CPL Test Series
Question Bank
Questions for ALTIMETRY1
Answer the following questions
Test Mode
Training Mode
1. You have landed on an airport elevation 1240 ft and QNH 1008 hPa. Your altimeter subscale is erroneously ser to 1013 hPa. The indication on the altimeter will be?
1375 ft
1200 ft
1105 ft
1280 ft
2. You are flying at FL 100 in an air mass that is 15°C colder than ISA. Local QNH is 983 hPa. What would the true altitude be?
10210 ft
10000 ft
8590 ft
11410 ft
3. When flying at FL180 in the Southern Hemisphere you experience a left crosswind. What is happening to your true altitude if indicated altitude is constant?
Remains the same
Increasing
Impossible to tell
Decreasing
4. Up to FL 180 ISA Deviation is ISA -10°C.What is the actual depth of the layer between FL 60 and FL 120?
5760 ft
6240 ft
5700 ft
6000 ft
5. Up to FL 180 ISA Deviation is ISA +10°C. What is the actual depth of the layer between FL 60 and FL 120?
5760 ft
6240 ft
5700 ft
6000 ft
6. You are flying from Madrid (QNH 1012) to Paris (QNH 1015) at FL 80. If your true altitude and indicated altitude remain the same then
The air at Madrid is warmer than Paris
Your indicated altitude must be changing
The altimeters are incorrect
The air at Paris is warmer than Madrid
7. Flying at FL 135 above the sea, the Radio Altimeter indicates a true altitude of 13500 ft. The local QNH is 1019 hPa. Hence the crossed air mass is, on average,
Warmer than ISA
Colder than ISA
There is insufficient information to determine the average temperature deviation
At ISA standard temperature
8. How is QNH determined from QFE?
Using the temperature of the airfield and the elevation of the airfield
Using the elevation
Using the temperature at MSL and the elevation of the airfield
Using the temperature
9. You fly from east to west at the 500 hPa level in the Northern Hemisphere;
if the wind is from the south there is again in altitude
if you encounter northerly drift, there is a gain in altitude
you fly towards an area of lower pressure, and therefore, experience a loss in altitude
if the wind is from the north there will be a gain in altitude
10. You are flying in the Alps at the same level as the summits on a hot day. What does the altimeter read?
Lower altitude as the summit
Higher altitude as the summit
Impossible to tell
Same altitude as the summit
11. When is pressure altitude equal to true altitude?
When the indicated altitude is equal to the pressure altitude
When surface pressure is 1013.25mb
In standard conditions
When the temperature is standard
12. QFE is 1000 hPa with an airfield elevation of 200 m AMSL. What is QNH? (use 8 m per hPa)
992 HPa
1008 HPa
1025 HPa
975 HPa
13. Flying from Marseilles to Palma you discover your true altitude is increasing, but oddly the QNH is identical at both places. What could be the reason?
Re-check the QNH
Palma is lower than Marseilles
The air at Palma is warmer
Re-check the radio altimeter
14. Altimeter set to 1023 at aerodrome. On climb to altitude the SPS is set at transition altitude. What will indication on altimeter do on resetting to QNH?
Dependent on temperature
Decrease
Same
Increase
15. Which of these would cause your true altitude to decrease with a constant indicated altitude?
Cold air/High pressure
Cold air/Low pressure
Hot air/Low pressure
Hot air/High pressure
16. Which of the following is true? QNH is
Can never be above or below 1013 hPa
Always less than 1013.25 hPa
Never 1013.25 hPa
Always more than 1013.25 hPa
17. An aircraft flying in the Alps on a very cold day, RPS 1013 set in the altimeter, flies level with the summit of the mountains. Altitude from aneroid altimeter reads
Higher than mountain elevation
Impossible to determine
Same as mountain elevation
Lower than mountain elevation
18. MSA given as 12,000 ft, flying over mountains in temperatures +9°C, QNH set as 1023 (obtained from a nearby airfield. What will the true altitude be when 12,000 ft is reached?
11,148
11,940
12,864
12,210
19. Which statement is true?
QNH is always lower than QFE
QFE is always lower than QNH
QNH can be equal to QFE
QFE can be equal to QFF only
20. If you are flying on a QNH 1009 on very cold day and you circle the top of a peak in the Alps, your altimeter will read
Not enough information to tell
The same as the elevation of the peak
Lower than the elevation of the peak
Higher than the elevation of the peak
21. You are flying in an atmosphere which is warmer than ISA, what might you expect?
True altitude to be lower than Indicated altitude
True altitude to be the same as Indicated altitude
True altitude to be the decreasing
True altitude to be higher than Indicated altitude
22. If an Aerodrome is 1500ft AMSL on QNH 1038, what will the actual height AGL to get to FL75?
5325 ft
8175 ft
6675 ft
8325 ft
23. You fly over the sea at FL 90, your true altitude is 9100 ft and QNH is unknown. What can be said about the atmosphere temperature?
QNH is lower than standard
It is colder than ISA
It is warmer than ISA
Nothing, insufficient information.
24. You are flying from Marseilles (QNH 1012 hPa) to Palma de Mallorca (QNH 1012 hPa) at FL100. You notice that the effective height above MSL (Radio Altitude) increases constantly. Hence...
You have to adjust for a crosswind from the right.
You have the altimeters checked, as their indications are obviously wrong.
One of the QNH values must be wrong.
The air mass above Palma is warmer than that above Marseilles
25. You are flying at FL160 with an OAT of -27°C. QNH is 1003 hPa. What is your true altitude?
15,730 ft
16,330 ft
15,540 ft
15,090 ft
26. What is the relationship between QFE and QNH at an airport 50ft below MSL?
QFE > QNH
QFE = QNH
QFE < QNH
There is no clear relationship
27. Flying from Marseilles (QNH 1012) to Palma (QNH 1015) at FL100. You do not reset the altimeter, why would true altitude be the same throughout the flight?
Blocked static vent
Air at Palma is warmer than air at Marseilles
Air at Marseilles is warmer than air at Palma
Not possible to tell
28. QNH is 1003. At FL100 true altitude is 10,000ft. Is it
Colder than ISA
Same as ISA
Cannot tell
Warmer than ISA
29. How do you calculate the lowest useable flight level?
Highest QNH and highest temperature above ISA
Highest QNH and lowest temperature
Lowest QNH and highest negative temperature below ISA
Lowest QNH and lowest negative temperature below ISA
30. You are cruising at FL 200, OAT is -40°C, sea level pressure is 1033 hPa. Calculate the true altitude?
18260 ft
21740 ft
19340 ft
20660 ft
31. What temperature and pressure conditions would be safest to ensure that your flight level clears all the obstacles by the greatest margin?
Temp less than or equal to ISA and a QNH less than 1013
Temp more than or equal to ISA and a QNH greater than 1013
Warm temp/high pressure
Cold temp/low pressure
32. QNH is 1030. Aerodrome is 200m AMSL. What is QFF?
Higher than 1030
Lower than 1030
Same
Not enough info
33. What condition would cause your indicated altitude to be lower than that being actually flown?
temperature higher than standard
Pressure lower than standard
temperature lower than standard
Pressure is standard
34. The QNH is 1030 hPa and at the Transition Level you set the SPS. What happens to your indicated altitude (assume 27 ft per 1 hPa)?
Rises
Rises by 459 ft
No change
Drops by 459 ft
35. An airfield has an elevation of 540ft with a QNH of 993mb. An aircraft descends and lands at the airfield with 1013mb set. What will its altimeter read on landing?
540ft
380ft
0ft
1080ft
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