Question 138-1 : Which of the following conditions would cause the altimeter to indicate a lower altitude than that actually flown ? [ Revision flight ]
Air temperature higher than standard

Question 138-2 : The qff at an airfield located 400 metres above sea level is 1016 hpa the air temperature is 10°c lower than a standard atmosphere what is the qnh ?
Less than 1016 hpa
Question 138-3 : The qnh at an airfield located 200 metres above sea level is 1009 hpa the air temperature is 10°c lower than a standard atmosphere what is the qff ?
More than 1009 hpa
Question 138-4 : The qnh at an airfield located 200 metres above sea level is 1022 hpa the air temperature is not available what is the qff ?
It is not possible to give a definitive answer

Question 138-5 : The qnh at an airfield located 0 metres above sea level is 1022 hpa the air temperature is not available what is the qff ?
1022 hpa

Question 138-6 : The qnh at an airfield in california located 69 metres below sea level is 1018 hpa the air temperature is 10°c higher than a standard atmosphere what is the qff ?
More than 1018 hpa
Question 138-7 : The qff at an airfield in california located 69 metres below sea level is 1030 hpa the air temperature is 10°c lower than a standard atmosphere what is the qnh ?
More than 1030 hpa

Question 138-8 : If the qfe at locarno 200 metres above sea level is 980 hpa what is the approximate qnh ?
Question 138-9 : If the qfe at locarno 200 metres above sea level is 1000 hpa what is the approximate qnh ?
Question 138-10 : If the qnh at locarno 200 metres above sea level is 1015 hpa what is the approximate qfe ?
990 hpa

Question 138-11 : If the qnh at locarno 200 metres above sea level is 1025 hpa what is the approximate qfe ?
1000 hpa

Question 138-12 : If you are flying at fl 300 in an air mass that is 15°c warmer than a standard atmosphere what is the outside temperature likely to be ?
Question 138-13 : If you are flying at fl 100 in an air mass that is 10°c warmer than a standard atmosphere what is the outside temperature likely to be ?
Question 138-14 : If you are flying at fl 120 and the outside temperature is 2°c at what altitude will the 'freezing level' be ?
Question 138-15 : An aircraft flying at fl 100 from marseille qnh 1012 hpa to palma de mallorca qnh 1006 hpa experiences no change to true altitude the reason for this is that ?
Question 138-16 : During a flight over the sea at fl 100 from marseille qnh 1012 hpa to palma de mallorca qnh 1012 hpa the true altitude is constantly increasing what action if any should be taken ?
Question 138-17 : During a flight over the sea at fl 100 from marseille qnh 1016 hpa to palma de mallorca qnh 1016 hpa the true altitude is constantly decreasing what is the probable reason for this ?
The air at marseille is warmer than that at palma de mallorca

Question 138-18 : During a flight over the sea at fl 135 the true altitude is 13500 feet local qnh is 1019 hpa what information if any can be gained about the air mass in which the aircraft is flying ?
It is colder than isa

Question 138-19 : An aircraft is flying over the sea at fl 90 the true altitude is 9100 feet local qnh is unknown .what assumption if any can be made about the air mass in which the aircraft is flying ?
There is insufficient information to make any assumption
Question 138-20 : An aircraft is flying over the sea at fl 120 with a true altitude of 12000 feet local qnh is 1013 hpa what assumption if any can be made about the air mass in which the aircraft is flying ?
Question 138-21 : An aircraft is flying over the sea at fl 100 with a true altitude of 10000 feet local qnh is 1003 hpa what assumption if any can be made about the air mass in which the aircraft is flying ?
It is warmer than isa

Question 138-22 : Which layer of the atmosphere contains more than 90 per cent of all water vapour ?
Question 138-23 : The temperature at fl 80 is +6°c what will the temperature be at fl 130 if the icao standard lapse rate is applied ?
4°c

Question 138-24 : The temperature at fl 110 is 5°c what will the temperature be at fl 50 if the icao standard lapse rate is applied ?
Question 138-25 : The temperature at fl 160 is 22°c what will the temperature be at fl 90 if the icao standard lapse rate is applied ?
8°c

Question 138-26 : A temperature of +15°c is recorded at an altitude of 500 metres above sea level if the vertical temperature gradient is that of a standard atmosphere what will the temperature be at the summit of a mountain 2500 metres above sea level ?
Question 138-27 : How would you characterise an air temperature of 15°c at the 700 hpa level over western europe ?
Low

Question 138-28 : An air temperature of 30°c at the 300 hpa level over central europe in summer is ?
Question 138-29 : How would you characterise an air temperature of 55°c at the 200 hpa level over western europe ?
Within +/ 5°c of isa

Question 138-30 : What is the technical term for an increase in temperature with altitude ?
Question 138-31 : The station pressure used in surface weather charts is ?
Qff

Question 138-32 : Which fl corresponds with the 300 hpa pressure level ?
Fl 300

Question 138-33 : Which fl corresponds with the 500 hpa pressure level ?
Fl 180

Question 138-34 : Which fl corresponds with the 700 hpa pressure level ?
Fl 100

Question 138-35 : Which fl corresponds with the 850 hpa pressure level ?
Fl 50

Question 138-36 : The qff at an airfield located 400 metres above sea level is 1016 hpa the air temperature is 10°c higher than a standard atmosphere what is the qnh ?
More than 1016 hpa

Question 138-37 : An aircraft is descending to land under ifr if the local qnh is 1009 hpa what will happen to the altitude reading when the altimeter is reset at the transition level ?
It will decrease

Question 138-38 : During the climb after take off the altimeter setting is adjusted at the transition altitude if the local qnh is 1023 hpa what will happen to the altimeter reading during the resetting procedure ?
It will decrease

Question 138-39 : During the climb after take off the altimeter setting is adjusted at the transition altitude if the local qnh is 966 hpa what will happen to the altimeter reading during the resetting procedure ?
Question 138-40 : An aircraft is flying from point a to point b on the upper level contour chart the altimeter setting is 1013 2 hpa which of these statements is correct . 292 ?
The true altitude will be higher at a than at b

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