Question Bank

1. When climbing through an inversion at constant mach number?

2. If indicated TAT is - 10°C, pressured altitude is 30000 ft. amsl, and mach number is 0.84, what is the temperature deviation?

3. CAS is IAS corrected for

4. When descending through an isothermal level the TAS will _____, the CAS and the LSS will ________ :

5. An Air Data Computer (ADC)

6. TAT = -25°. SAT = -35°. Find TAS.

7. The Airspeed Indicator measures

8. If pressure altitude is 30000 ft., indicated TAT is -10°C, mach number is 0.82, what is the density altitude?

9. An is aircraft flying at a TAS of 1100 knots at FL650. A change in 0.1M causes a change i TAS of 57 knots. The temperature deviation at FL 650 assuming an ISA atmosphere is

10. As pressure altitude increases

11. EAS is

12. A/C is flying at TAS = 400 Kts. SAT = -23°. Find Dynamic rise in temperature

13. Calibrated air speed is

14. Cruising at FL 390, M.84 is found to give a TAS of 499kt. The ISA deviation at this level will be

15. When descending through an inversion at constant CAS?

16. The difference between static air temperature and total air temperature is known as

17. When climbing through an inversion at constant TAS.

18. When descending through an isothermal layer at a constant Calibrated Airspeed (CAS), the True Airspeed (TAS) will

19. An aircraft is flying at FL390, temperature -56.5° C at Mach0.85. The TAS of the aircraft is

20. Total Air Temp is always... than Static Air Temp and the difference varies with....

21. In An Air Data Computer (ADC), aero plane altitude is calculated from

22. When descending through an isothermal layer at a constant Calibrated Airspeed (CAS), the True Airspeed (TAS) will?

23. As pressure altitude increases when climbing at constant mach number?

24. An aircraft is flying at mach 0.86 and the true ambient air temperature is - 42°C. Determine

25. If pressure altitude is 30000 ft amsl and mach number is 0.84 what is the ISA TAT?

26. At any given height or altitude, an aircraft will always lift-off at the same?

27. As pressure altitude increases when climbing at constant IAS?

28. If a Decrease of 0.12 in the Mach number results in a decrease of 80 Knots in the TAS, what is the local speed of sound?

29. When climbing through an inversion at constant CAS?

30. At a constant Mach number, the calibrated airspeed (CAS)

31. An increase of 0.15 Mach results in an increase of 93 kt TAS of an aircraft. The local speed of sound is

32. M 0.80, OAT - 50°C, FL 330, GS 490 kt, VAR 20°W, Magnetic heading 140°, drift is 11° right. Calculate the true W/V?

33. FL250,OAT -15°C, TAS 250 kt, Calculate the Mach No.?

34. TAS 487kt, FL 330, Temperature ISA + 15. Calculate the MACH number?

35. For a constant Calibrated Airspeed (CAS) and a level flight, a fall in ambient temperature will result in a

36. TAS = 485 kt, OAT = ISA + 10°C, FL 410. Calculate the Mach number?

37. When descending through an inversion at constant TAS?

38. When descending through an inversion at constant CAS?

39. When climbing at a constant Mach number below the tropopause, in ISA conditions =, the Calibrated Airspeed (CAS) will

40. When climbing through an inversion at constant CAS?

41. A/C is flying at TAS = 520 Kts. SAT is - 20°C. Find TAT.

42. The velocity of sound at the sea level in a standard atmosphere is

43. What corrections must be applied to indicated airspeed to produce true airspeed?

44. Total air temp is _____ than _____ by an amount which is proportional to _____.

45. When climbing through an isothermal layer at constant TAS?

46. A temperature sensor having a recovery factor of 0.75 indicates 30°C. Static Air Temperature (SAT) is 25°C. How high is the Ram-rise?

47. EAS is?

48. Mach number is the ratio of?

49. When descending through an isothermal layer at constant TAS?

50. FL120, OAT is ISA standard, CAS is 200 kt, Track is 222°(M), Heading is 215°(M), Variation is 15°W. time to fly 105 NM is 21 MIN. what is the W/V?