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DGCA Technical General · 34 questions

Temperature Indicators: DGCA Technical General Questions and Answers

34 practice questions on Temperature Indicators with answers and explanations, plus the key concepts and formulas, from the TrueHeading question bank.

About this topic

Use this page to revise Temperature Indicators for the DGCA Technical General paper. Below are the key ideas first, then 12 practice questions with answers and explanations, picked from the 34 questions in the TrueHeading bank for this topic.

In short: Thermocouples (two dissimilar metals) produce a voltage.

Open the full set in the student zone to answer every question, track your accuracy and take timed mock tests.

Key concepts: Temperature Indicators

2 ideas to know cold.

How is temperature measured in an engine?

Thermocouples (two dissimilar metals) produce a voltage.

TATSAT=1+0.2 K M2(temperatures in K)\frac{TAT}{SAT}=1+0.2\,K\,M^2\quad(\text{temperatures in K})
  • EGT: chromel–alumel · CHT: iron–constantan
  • Resistance thermometers for oil and air temperature
  • Total air temperature includes ram rise

What are SAT, TAT and RAT?

SAT: static (outside) air temperature. TAT: total air temperature including ram rise. RAT: the ram air temperature rise.

TAT=SAT(1+0.2M2)TAT=SAT\left(1+0.2M^2\right)
  • TAT = SAT (1 + 0.2 M²), in kelvin
  • At M 0.8, ram rise ≈ 28 °C
  • Thermocouples measure EGT

Practice questions: Temperature Indicators

Tap “Show answer” after you have tried each one.

Q1SAT is −56 °C and the aircraft flies at Mach 0.80 with a probe recovery factor of 1. The TAT is approximately:

  1. −19 °C
  2. 0 °C
  3. −28 °C
  4. −34 °C
Show answer

Answer: C. −28 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q2SAT is −50 °C and the aircraft flies at Mach 0.78 with a probe recovery factor of 1. The TAT is approximately:

  1. −14 °C
  2. −23 °C
  3. 4 °C
  4. −29 °C
Show answer

Answer: B. −23 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q3SAT is −40 °C and the aircraft flies at Mach 0.74 with a probe recovery factor of 1. The TAT is approximately:

  1. −20 °C
  2. −5 °C
  3. −14 °C
  4. 11 °C
Show answer

Answer: C. −14 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q4SAT is −60 °C and the aircraft flies at Mach 0.84 with a probe recovery factor of 1. The TAT is approximately:

  1. −30 °C
  2. −36 °C
  3. −21 °C
  4. 0 °C
Show answer

Answer: A. −30 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q5SAT is −20 °C and the aircraft flies at Mach 0.76 with a probe recovery factor of 1. The TAT is approximately:

  1. 18 °C
  2. 38 °C
  3. 3 °C
  4. 9 °C
Show answer

Answer: D. 9 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q6SAT is −56 °C and the aircraft flies at Mach 0.85 with a probe recovery factor of 1. The TAT is approximately:

  1. −16 °C
  2. 7 °C
  3. −25 °C
  4. −31 °C
Show answer

Answer: C. −25 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q7SAT is −35 °C and the aircraft flies at Mach 0.80 with a probe recovery factor of 1. The TAT is approximately:

  1. −11 °C
  2. −5 °C
  3. 4 °C
  4. 26 °C
Show answer

Answer: B. −5 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q8SAT is −30 °C and the aircraft flies at Mach 0.82 with a probe recovery factor of 1. The TAT is approximately:

  1. 35 °C
  2. 3 °C
  3. 12 °C
  4. −3 °C
Show answer

Answer: B. 3 °C

TAT = SAT × (1 + 0.2 M²) with temperatures in kelvin.

Q9−40 °C is equal to:

  1. −40 °F
  2. −30 °F
  3. −8 °F
  4. 10 °F
Show answer

Answer: A. −40 °F

°F = °C × 9/5 + 32.

Q1030 °C is equal to:

  1. 49 °F
  2. 96 °F
  3. 86 °F
  4. 62 °F
Show answer

Answer: C. 86 °F

°F = °C × 9/5 + 32.

Q11100 °C is equal to:

  1. 132 °F
  2. 222 °F
  3. 88 °F
  4. 212 °F
Show answer

Answer: D. 212 °F

°F = °C × 9/5 + 32.

Q1237 °C is equal to:

  1. 53 °F
  2. 69 °F
  3. 99 °F
  4. 109 °F
Show answer

Answer: C. 99 °F

°F = °C × 9/5 + 32.

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