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Question 151-1 : You are flying at fl 130, and your true altitude is 12000 ft. what is the temperature deviation from that of the standard atmosphere at fl 130 qnh 1013,2 hpa ? [ Learning aircraft ]
Isa 20°c.
.to determine the true altitude/height the following rule of thumb, called the 4% rule , shall be used..the altitude/height changes by 4% for each 10°c temperature deviation from isa...4 x 13 x temperature deviation = 1000 ft.temperature deviation = 1000 ft / 4 x 13 = 19.2°c..true altitude is lower than pressure altitude, so this is minus 20°c.
Question 151-2 : Which one of the following statements applies to the tropopause ?
It separates the troposphere from the stratosphere
.the tropopause is a boundary with no finite thickness. the tropopause is the region of the atmosphere where the environmental lapse rate changes from positive, as it behaves in the troposphere, to the stratospheric negative one. following is the exact definition used by the world meteorological organization the boundary between the troposphere and the stratosphere, where an abrupt change in lapse rate usually occurs. it is defined as the lowest level at which the lapse rate decreases to 2 °c/km or less, provided that the average lapse rate between this level and all higher levels within 2 km does not exceed 2 °c/km.
Question 151-3 : The 0° isotherm is forecast to be at fl 50. at what fl would you expect a temperature of 6°c ?
Fl 80.
.the temperature lapse rates of the troposphere is mean value 0.65°c/100 m or 2°c/1000 ft...6° / 2° per 1000 ft = 3000 ft..fl50 + 3000 ft = fl80.
Question 151-4 : A vertical spacing of 1000 ft is the standard required separation between two fl. under conditions of cold air advection isa 15°c , what would the true vertical separation be ?
Less than 1000 ft.
. 515.in flight level, aircraft are using the same subscale reference 1013.25 hpa..theoretical separation is 1000 ft, actual separation is less when air mass is colder than standard.
Question 151-5 : Over paris at what flight level would you expect to find the tropopause according to the map. 269 ?
Fl 300.
.tropopause is at fl290 north est and at fl340 south west of paris..we would expect to find the tropopause at fl300 over paris.
Question 151-6 : What is the approximate height of the tropopause between munich and helsinki. 271 ?
Fl 340.
. 523.the approximate height of the tropopause between munich and helsinki is fl340..400 on the one hand, 300 on the other hand, even if the height change is not uniform, fl340 remains the only valid answer.
Question 151-7 : At what approximate flight level is the tropopause over frankfurt. 276 ?
Fl 330.
. 526.you have to interpolate between different heights. placing the tropopause at approximately fl 330 over frankfurt.
Question 151-8 : The temperature at fl 330 overhead london will be. 278 ?
45°c.
.the height of the tropopause over london is fl290. above the tropopause the temperature stays constant. close to london, t° is around 45°c at fl390 so between fl290 and fl390, no change.
Question 151-9 : What is the average temperature at fl 160 between oslo and paris . 282 ?
19°c.
.this chart is given for fl180...at fl180 between oslo and paris, average temperature is. 25 + 24 + 23 + 21 + 21 /5 = 114 / 5 = around 23°c...average temperature at fl160 is 4° warmer 2° per 1000ft = 19°c.
Question 151-10 : What is the temperature deviation in degrees celsius, from the icao standard atmosphere overhead frankfurt . 283 ?
Isa 13°c
.at fl180, in a standard atmosphere, temperature is.15° 2° x 18 = 21ºc..on the chart, overhead frankfurt, temperature at fl180 is 34°c..temperature deviation is 34° + 21° = 13°c...we can say that temperature overhead frankfurt, at fl180, is colder than icao standard atmosphere.
Question 151-11 : What oat would you expect at fl 200 over geneva . 289 ?
24°c.
.this chart is given for fl180...at fl180 average temperature is. 20 + 21 + 19 + 21 /4 = 81 / 4 = around 20°c...average temperature at fl200 is 4° colder 2° per 1000ft = 24°c.
Question 151-12 : An altimeter adjusted to 1013 hpa indicates an altitude of 3600 ft. should this altimeter be adjusted to the local qnh value of 991 hpa, the altitude indicated would be ?
3006 ft.
.your altimeter adjusted to 1013 hpa indicates an altitude of 3600 ft..you have to turn altimeter setting adjustement knob in a counter clockwise direction, to set 991 hpa in the subscale window. the altimeter needle will turn in the same direction counter clockwise.. 541.decreasing altimeter setting by 22 hpa 1013 991.22 hpa x 27 ft/hpa = 594 ft...indicated altitude decreases by 594 ft 3600 594 = 3006 ft.
Question 151-13 : In geneva, the local qnh is 994 hpa. the elevation of geneva is 1411 ft. the qfe adjustment in geneva is ?
942 hpa.
.the qfe indicates, in standard atmosphere, the height of the aircraft above the official airport elevation an altimeter set to qfe will therefore read zero when on the ground..qnh is the setting which will give airfield elevation when parked on the airfield...with a subscale setting of 994 hpa, on the ground at geneva, your altimeter reads 1411 ft..you want to read 0 ft...you must turn anti clockwise the adjustment knob 1 hpa = 27 ft..1411 / 27 = 50 hpa...994 52 = 942 hpa.. 531
Question 151-14 : An aircraft is flying at fl 80. the local qnh is 1000 hpa. after the second altimeter has been adjusted to the local qnh, the reading will be approximately ?
7650 ft.
.your main altimeter remains at 1013 hpa with a reading of 8000 ft, the second is set at 1000 hpa, you have to turn altimeter setting adjustement knob in a counter clockwise direction, the altimeter needle will turn also counter clockwise.. 541.decreasing altimeter setting by 13 hpa.13 hpa x 27 ft/hpa = 351 ft...indicated altitude decreases by 351 ft 8000 351 = 7649 ft.
Question 151-15 : The barometric compensator of an altimeter is locked on reference 1013.2 hpa. the aircraft has to land on a point with an elevation of 290 feet where the qnh is 1023 hpa. the reading on the altimeter on the ground will be ?
20 ft.
.1023 1013 = 10 hpa..10 hpa x 27 ft/hpa = 270 ft...290 ft 270 ft = 20 ft...imagine if you landed on this airfield with the correct subscale setting 1023 hpa , the reading on the altimeter on the ground will be 290 ft. now, if you set 1013 hpa in the subscale, the needles will turn couter clockwise, and the altimeter will read 20 ft.
Question 151-16 : The upper wind and temperature chart of 250 hpa corresponds, in a standard atmosphere, to about ?
34 000 ft.
.there is a few questions in the exam that take information directly from that table below, write these down on a sticky and have them on the wall beside you.1013 hpa = msl.850 hpa = fl50.700 hpa = fl100.500 hpa = fl180.300 hpa = fl300.200 hpa = fl390..any others you can interpolate between these and figure it out..the decrease of 1hpa/27 ft is only applicable at the lower levels of the troposphere, as you go up and air pressure decreases, the change of height per 1 hpa increases at msl 1hpa/27ft, at fl180 it's 50ft/hpa and at fl390 it's 105ft/hpa.
Question 151-17 : Going from the equator to the north pole, the altitude of the tropopause ?
Decreases and its temperature increases.
. 491.height of the tropopause...polar tropopause 8 km 45°c..tropicale tropopause 15 km 75°c..equatorial tropopause 16 km 80°c.
Question 151-18 : Atmospheric soundings give the following temperature profile.3000 ft +15°c.6000 ft +8°c.10000 ft +1°c.14000 ft 6°c.18000 ft 14°c.24000 ft 26°c.at which of the following flight levels is the risk for aircraft icing, in cloud, greatest ?
Fl 150.
.greatest icing occurs at temperature between 0°c and 10°c...temperature at fl80 is largely positive at around +4°c there will be no risk of icing...at fl150, temperature is around 8°c, severe icing has greatest possibility to occur...temperature above fl160 will be lower than 10°c, risk for aircraft icing is possible but with a less intensity than temperature between 0°c and 10°c.
Question 151-19 : Half the mass of the atmosphere is found in the first ?
5 km.
Question 151-20 : The thickness of the troposphere varies with ?
Latitude.
.tropopause is the boundary layer between troposphere and stratosphere.. 491.16 km is approximately the average thickness of the troposphere over the equator 0° n/s of latitude..at 45° of latitude, the thickness is around 12 km..at poles 90° n/s of latitude, the thickness is around 8 km...the thickness of the troposphere varies with latitude.
Question 151-21 : In the lower part of the stratosphere the temperature ?
Is almost constant.
. 633.in the real world, in the lower part of the stratosphere, the temperature is rising a little with altitude, but in isa no.
Question 151-22 : Which of the following conditions would cause the altimeter to indicate a lower altitude than that actually flown ?
Air temperature higher than standard.
.if the temperature or pressure is higher than isa your true altitude will be higher than indicated, you are safe. if the temperature or pressure is lower than isa your true altitude will be lower than indicated or closer to the ground which is dangerous...if it is cold, imagine the air 'shrinking' down so the pressure level will be closer to the ground, while if it is hot the air will 'expand' so the pressure level will be higher above the ground...remember the altimeter is reading a pressure level, but it does not know how high the pressure level is above the ground. if you are flying at 10000 ft indicated you are following the 700 hpa line, and although you are keeping the altimeter at 10000 ft you will not always be at 10000 ft above the ground.
Question 151-23 : 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.
.qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the 'cold' qnh will be less than qff and the 'warm' qnh will be more than qff...this table will help for the exam. 539
Question 151-24 : 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.
.qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the cold qnh will be less than qff and the warm qnh will be more than qff...this table will help for the exam. 539
Question 151-25 : 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.
.qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the 'cold' qnh will be less than qff and the 'warm' qnh will be more than qff...this table will help for the exam. 539.we need to know the temperature
Question 151-26 : 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.
.qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the 'cold' qnh will be less than qff and the 'warm' qnh will be more than qff...this table will help for the exam. 539.when temperature is unknown you are unable to calculate qff, expect at mean sea level..at sea level qfe = qnh = qff regardless of temperature, because you are not correcting up or down to find msl... pantalejandro.fast and furious analogy..qff = fast furious..from the starting point all 3 race cars 'qfe, qnh and qff' are at same position m.s.l. , same pressure value , as the race goes on qff =>fast furious' will lead if it is cold colder than isa= more thrust => 'qnh is less', or will lag behind if it is warm warmer than isa = less thrust => 'qnh is more'. while the other two cars will go hand by hand...note below m.s.l the story is reverted. > qff less if colder...i made this out, hope it works for you guys
Question 151-27 : 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.
Qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the 'cold' qnh will be less than qff and the 'warm' qnh will be more than qff...this table will help for the exam. 539
Question 151-28 : 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
.qff is atmospheric pressure at sea level..qnh is the setting which will give airfield elevation when parked on the airfield..in cold conditions a column of air will shrink so the 'cold' qnh will be less than qff and the 'warm' qnh will be more than qff...this table will help for the exam. 539
Question 151-29 : If the qfe at locarno 200 metres above sea level is 980 hpa, what is the approximate qnh ?
1005 hpa.
.the qfe indicates, in standard atmosphere, the height of the aircraft above the official airport elevation an altimeter set to qfe will therefore read zero when on the ground. and you want the qnh to read an altitude... qfe 980 hpa..|..| 200m / 8m per hpa = 25 hpa..|..| qnh 1005 hpa.
Question 151-30 : If the qfe at locarno 200 metres above sea level is 1000 hpa, what is the approximate qnh ?
1025 hpa.
.the qfe indicates, in standard atmosphere, the height of the aircraft above the official airport elevation an altimeter set to qfe will therefore read zero when on the ground. and you want the qnh to read an altitude... qfe 1000 hpa..|..| 200m / 8m per hpa = 25 hpa..|..| qnh 1025 hpa.
Question 151-31 : If the qnh at locarno 200 metres above sea level is 1015 hpa, what is the approximate qfe ?
990 hpa.
.the qfe indicates, in standard atmosphere, the height of the aircraft above the official airport elevation an altimeter set to qfe will therefore read zero when on the ground..qnh is the setting which will give airfield elevation when parked on the airfield.... qfe 990hpa..|..| 200m / 8m per hpa = 25hpa..|..| qnh 1015hpa...use this craftiness.your altimeter is reading 675 ft 200 m when parked on the airfield with a subscale setting of 1015 hpa. you want to read 0 ft the qfe. you must decrease the subscale setting until the needle shows 0 ft. the adjustment knob turns counter clockwise as the needle. 541
Question 151-32 : If the qnh at locarno 200 metres above sea level is 1025 hpa, what is the approximate qfe ?
1000 hpa.
.the qfe indicates, in standard atmosphere, the height of the aircraft above the official airport elevation an altimeter set to qfe will therefore read zero when on the ground..qnh is the setting which will give airfield elevation when parked on the airfield.... qfe 1000hpa..|..| 200m / 8m per hpa = 25hpa..|..| qnh 1025hpa...use this craftiness.your altimeter is reading 675 ft 200 m when parked on the airfield with a subscale setting of 1025 hpa. you want to read 0 ft the qfe. you must decrease the subscale setting until the needle shows 0 ft. the adjustment knob turns counter clockwise as the needle. 541
Question 151-33 : 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 ?
30°c.
.in standard atmosphere, the decrease in temperature per 1000 feet is 2°c..in standard atmosphere, temperature is 15°c at 0 ft...at fl300, temperature is 15°c 30 x 2°c = 45°c...air mass is 15°c warmer than standard. 45°c + 15°c = 30°c.
Question 151-34 : 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 ?
+5°c.
.in standard atmosphere, the decrease in temperature per 1000 feet is 2°c..in standard atmosphere, temperature is 15°c at 0 ft...at fl100, temperature is 15°c 10 x 2°c = 5°c...air mass is 10°c warmer than standard. 5°c + 10°c = +5°c.
Question 151-35 : If you are flying at fl 120 and the outside temperature is 2°c, at what altitude will the 'freezing level' be ?
Fl 110.
.in standard atmosphere, the decrease in temperature per 1000 feet is 2°c..at fl120, temperature is 2°c...1000 ft below, temperature will be 2° warmer..1000 ft above, temperature will be 2° colder...the 'freezing level' 0°c will be at fl 110.
Question 151-36 : 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 ?
The air at palma de mallorca is warmer than that at marseille.
.case n°1. 540.if temperature is the same between both locations, the true altitude will be reduced over palma by 6 hpa around 162 ft...case n°2
Question 151-37 : 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 ?
None, the reason for the change is that the air around palma is warmer than the air around marseille
Question 151-38 : 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.
.if the qnh remains unchanged, and the true altitude is constantly decreasing, the only reason is a reduction of the volume of the 'air mass'. how an 'air mass' can contract.the temperature is decreasing and thus the density is increasing..the air at palma de mallorca is colder than that at marseille in other words air at marseille is warmer than that at palma de mallorca.
Question 151-39 : 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.
.if you are flying at fl135, your subscale altimeter setting is 1013 hpa..if the local qnh is 1019 hpa, and if you set your second altimeter with this value, you will normally read more than 13500 ft..but you read today 13500 ft this is your true altitude... it means that the air mass is colder than isa air mass is contracted.
Question 151-40 : 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.
.you need to know the local qnh, even if we know that the aircraft is flying flight levels 1013 hpa , there is insufficient information to make any assumption..true altitude is 9100 ft do not mean that air mass is warmer than isa, it could be because the local qnh is higher than 1013 hpa.
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