DGCA Air Navigation: Air Temperature & AoA Measurement Questions
16 exam-style Air Temperature & AoA Measurement questions for the DGCA Air Navigation paper (CPL · ATPL · PPL). The first 12 are free below with answers and explanations — sign up free to practise all of them with progress tracking.
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Q1
Converted into degrees Celsius - 40°F is:
- A -56.5°C
- B -40°C
- C -20°C
- D -108°C
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Correct answer: B. -40°C
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Q2
In an aircraft thermometer with an electrical resistance sensor to measure the air temperature, the resistance wire element is probably:
- A plutonium
- B platinum
- C potassium
- D beryllium copper
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Correct answer: B. platinum
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Q3
Flying at high speed at high altitude, the difference between ram air temperature and static air temperature is:
- A likely to be less than when flying low and slow.
- B due to adiabatic cooling.
- C due to adiabatic warming.
- D proportional to the square of the absolute temperature.
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Correct answer: C. due to adiabatic warming.
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Q4
Aircraft air temperature thermometers are shielded to protect them from:
- A solar radiation.
- B accidental physical damage on the ground or hailstones in flight.
- C airframe icing.
- D kinetic heating.
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Correct answer: A. solar radiation.
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Q5
At a true airspeed of 500 knots, a ram rise of air temperature can be expected of:
- A 50°C
- B 25°C
- C 5°C
- D 16°C
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Correct answer: B. 25°C
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Q6
An air temperature probe may be aspirated in order to:
- A prevent icing.
- B measure air temperature on the ground.
- C compensate for thermal soaking at the ramp position.
- D reduce the effect of solar radiation.
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Correct answer: B. measure air temperature on the ground.
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Q7
Total Air Temperature is:
- A the maximum temperature attainable by the air when brought to rest, adiabatically.
- B the temperature indicated on the air temperature thermometer plus the ram rise.
- C the static air temperature minus the recovery factor.
- D the recovery factor plus the ram rise.
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Correct answer: A. the maximum temperature attainable by the air when brought to rest, adiabatically.
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Q8
The difference between static air temperature and total air temperature is known as:
- A corrected outside air temperature.
- B the ram rise.
- C the recovery factor.
- D hot ramp radiation.
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Correct answer: B. the ram rise.
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Q9
A direct reading aircraft thermometer usually consists of a bimetallic helix protruding into the airstream. Movement of the pointer over the temperature scale will depend upon:
- A difference in electrical resistance of the two metals.
- B increase in pressure as airspeed increases.
- C increase in adiabatic cooling as airspeed increases.
- D different coefficients of expansion of the two metals.
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Correct answer: D. different coefficients of expansion of the two metals.
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Q10
A remote reading thermometer depends upon ....... to indicate changes in temperature:
- A change of electrical resistance of the two metals.
- B change of electrical resistance with temperature.
- C change of electrical resistance with change in pressure.
- D change of electrical capacitance with change in temperature.
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Correct answer: B. change of electrical resistance with temperature.
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Q11
What formula gives the total temperature (TT) from the static temperature (TS):
- A A
- B B
- C C
- D D
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Correct answer: B. B
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Q12
Total Air Temperature is __________ than static air temperature and the difference varies with __________
- A warmer altitude
- B colder altitude
- C warmer CAS
- D colder CAS
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Correct answer: C. warmer CAS
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