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CPL Test Series
Question Bank
Questions for Kw inst CRP5
Answer the following questions
Test Mode
Training Mode
1. The velocity of the speed of sound at sea level in the standard atmosphere is?
1059 kts.
661 kts
644 kts.
332 kts.
2. An increase of 0.15 mach results in an increase of 93 Kts TAS. The local speed of sound is?
620 Kts
685 Kts.
580 Kts.
560 Kts.
3. If outside air temperature at 35000 ft is -40°C, the local speed of sound is?
596 kts.
307 kts.
686 kts.
247 kts.
4. What is the TAS when pressure altitude = 20000 ft, OAT = -20°C, CAS = 200 Kts?
296 Kts
273 Kts
239 Kts.
194 Kts.
5. An aircraft is flying at FL 390, temperature is -56.5°C at mach 0.85. The TAS is?
476 Kts.
472 Kts.
561 Kts.
485 Kts.
6. An aircraft flying at FL 310 is cruising at a CAS of 280 Kts. If the correct outside air temperature is -48°C, this will give a mach number of?
0.76
0.78
0.71
0.82
7. An aircraft is flying at an indicated altitude of 16000 ft. The outside air temperature is -30°C. What is the true altitude?
16200 ft
15200 ft.
13500 ft.
18600 ft.
8. The temperature at the airport is 23°C, what is the local speed of sound?
615 Kts.
644 Kts.
671 Kts.
694 Kts.
9. What is the TAS when pressure altitude = 15000 ft, OAT = -15°C, CAS = 145 Kts?
148 Kts.
183 Kts.
133 Kts.
198 Kts.
10. An aircraft is flying at FL290 at 500 Kts TAS, 0.86M, the temperature deviation is?
+7.
+25.
-8.
-15.
11. Cruising at FL 390, M0.84, is found to give a TAS of 499 Kts. The ISA deviation at this level is?
+17.
-17.
+19
-19
12. An increase of 0.15 in mach number results in an increase of 93 Kts TAS. If temperature deviation from ISA is +9°C, the FL is?
FL90
FL220
FL170
FL200
13. An increase of 0.15 mach results in an increase of 93 Kts TAS. If temperature deviation from ISA is +5°C, the approximate flight level is?
FL250.
FL 200.
FL150.
FL220.
14. An aircraft is flying at 310 kts TAS at FL290, Temperature deviation is -6°C. The local speed of sound is?
583 Kts.
596 Kts.
563 Kts.
570 Kts.
15. An aircraft is flying at 1100 Kts TAS at FL650. A change of 0.1M gives a change of 57 Kts TAS. The temperature deviation at FL650 assuming an ISA atmosphere is?
+5
+2.5.
-2.5.
-5
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