Met Gen 3 Flashcards
Given the same pressure gradient over the land and over the adjacent water, what is the most probable wind angle to the isobars and wind speed over the water if the surface wind over the land is blowing across the isobars at an angle of 30 degrees and at a speed of 30 kts?
A) 40 degrees and 20 Kts
B) 30 degrees and 30 Kts
C) 20 degrees and 20 Kts
D) 20 degrees and 40 Kts
D) 20 degrees and 40 Kts
A flight from Vancouver to Montreal at a constant pressure level experiences winds that gradually veer from the southwest to the northwest. The aircrafts actually height above mean sea level will have: (hint: port drift-A/C true altitude is increasing; starboard drift-A/C true altitude is decreasing)
A) Increases steadily.
B) Increases for a time and then decreases steadily thereafter.
C) Decreases steadily.
D) Decreases for a time and then increases steadily thereafter.
B) Increases for a time and then decreases steadily thereafter.
If the temperatures to the southeast today are warmer than those to the northwest, the winds aloft would be blowing from the: (recall buys-ballots law - with your back to the wind, your left hand will point to the area of lower pressure; for upper level winds, your left hand will point to area of lower temperatures)
A) Northeast.
B) Southeast.
C) Northwest.
D) Southwest.
D) Southwest.
From the statements listed below which relate to density altitude, select the one which is FALSE:
A) The calculation of the density altitude at a given aerodrome consists of correcting the existing pressure altitude with the ISA temperature for that level.
B) The density altitude is that altitude in the standard atmosphere which corresponds to a given density value.
C) An increase in density altitude corresponds to a decrease in density.
D) The density altitude for a given aerodrome is changing continuously in response to changes in pressure and temperature.
A) The calculation of the density altitude at a given aerodrome consists of correcting the existing pressure altitude with the ISA temperature for that level.
An aerodromes density altitude is calculated with a flight computer using the:
A) The aerodromes published elevation matched with the ambient air temperature.
B) The aerodromes pressure altitude matched with the aerodromes outside air temperature corrected in terms of ASL.
C) The aerodromes pressure altitude matched with the aerodromes outside air temperature corrected in terms of AGL.
D) The aerodrome altitude above sea level matched with the average sea level temperature during the previous 12 hours.
B) The aerodromes pressure altitude matched with the aerodromes outside air temperature corrected in terms of ASL.
An aircrafts true altitude would be greater than its indicated altitude in terms of:
A) Warm air and high pressure.
B) Warm air and low pressure.
C) Cold air and high pressure.
D) Cold air and low pressure.
A) Warm air and high pressure.
Which of the following statements is true with respect to the term MSL pressure?
A) It is station pressure reduced to MSL assuming ISA conditions.
B) It is station level pressure extracted from the appropriate synoptic chart.
C) It is station pressure reduced to MSL using the average surface temperature for the last 12 hours.
D) It is the average sea level pressure reading at a given station during the previous 3 hour period.
C) It is station pressure reduced to MSL using the average surface temperature for the last 12 hours.
Altimeter setting is:
A) Measured MSL pressure corrected for non-standard temperature.
B) Station pressure reduced to sea level with a 12 hour average temperature correction applied to it.
C) Measured MSL pressure with ISA deviation correction applied.
D) Station level pressure reduced to MSL assuming ISA conditions.
D) Station level pressure reduced to MSL assuming ISA conditions.
It is essential that a pilot flying in the Standard Pressure Region closely monitor terrain clearance, when:
A) Pressures are high and temperatures are high.
B) Operating in an air mass having a variable pressure gradient.
C) Pressures are low and temperatures are low.
D) The current altimeter setting is greater than 31.00 inches (Hg).
C) Pressures are low and temperatures are low.
An aircraft descends from FL380 for an approach to Kelowna Airport. During the descent, the pilot forgets to reset the altimeter subscale. If the published decision height is 2060 ft ASL, what would be the actual height of the aircraft on reaching the indicated DH. (Refer to the following METAR).
METAR CYLW 281700Z 18010KT 5SM -SHRA OVC015 10/06 A2962 RMK SF8 SLP150=
A) 2060 ft ASL
B) 2360 ft ASL
C) 1760 ft ASL
D) 1460 ft ASL
C) 1760 ft ASL
Compare two aircraft on approach- the first aircraft is flying the approach in standard atmospheric conditions; the second aircraft in colder than standard conditions. Both aircraft arrive over the FAF at the altitude that is shown on the approach plate (no temperature corrections applied). What is the second aircrafts altimeter reading in relation to the first, and what is the result?
A) The second aircrafts altimeter will be over reading, and therefore the aircraft will be lower than the published altitude.
B) The second aircrafts altimeter will be under reading, and therefore the aircraft will be lower than the published altitude.
C) The second aircrafts altimeter will be under reading, and therefore the aircraft will be higher than the published altitude.
D) The second aircrafts altimeter will be over reading, and therefore the aircraft will be higher than the published altitude.
A) The second aircrafts altimeter will be over reading, and therefore the aircraft will be lower than the published altitude.
Compare two aircraft on approach- the first aircraft is flying the approach in standard atmospheric conditions; the second aircraft in colder than standard conditions. Both aircraft are on a RNAV/RNP style approach. What will happen to the slope of the approach flown by the second aircraft.
A) No difference.
B) The second aircraft will fly a steeper approach path and touchdown with zero temperature error on the altimeter.
C) The second aircraft will fly a shallower approach path and touchdown with a temperature error on the altimeter.
D) The second aircraft will fly a shallower approach path and touchdown with zero temperature error on the altimeter.
D) The second aircraft will fly a shallower approach path and touchdown with zero temperature error on the altimeter.
The relationship between the amount of water vapor actually present in the air and the maximum possible amount of water vapor that could be held by the air at that temperature and pressure (without condensation occurring) is expressed by which of the following terms?
A) Dewpoint temperature.
B) Saturation vapor pressure.
C) Relative Humidity.
D) Saturation index.
C) Relative Humidity.
The height of a cloud base is most dependent upon the:
A) Moisture content in the air.
B) The dry adiabatic lapse rate.
C) The amount of cooling that is taking place at the earths surface.
D) The strength of any vertical motion present at the 400hPa level.
A) Moisture content in the air.
Clouds and precipitation are common in areas:
A) Of subsiding air.
B) Located immediately above the isothermal layer.
C) Where katabatic flow is present.
D) Of ascending air.
D) Of ascending air.