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Aviation Seminars1 #3248. Which instrument will become inoperative if the pitot tube becomes clogged? A- Altimeter. B- Vertical speed. C- Airspeed.

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Presentation on theme: "Aviation Seminars1 #3248. Which instrument will become inoperative if the pitot tube becomes clogged? A- Altimeter. B- Vertical speed. C- Airspeed."— Presentation transcript:

1 Aviation Seminars1 #3248. Which instrument will become inoperative if the pitot tube becomes clogged? A- Altimeter. B- Vertical speed. C- Airspeed.

2 Aviation Seminars2 Sorry that is Incorrect. Go Back and Try Again.

3 Aviation Seminars3 That’s Right!!! Next Question

4 Aviation Seminars4 # 3273. What is the maximum structural cruising speed ? A- 100 MPH. B- 165 MPH. C- 208 MPH.

5 Aviation Seminars5 Sorry that is Incorrect. Go Back and Try Again.

6 Aviation Seminars6 That’s Right!!! Next Question

7 Aviation Seminars7 #5157. While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will A- decrease the rate of turn resulting in a decreased load factor. B- decrease the rate of turn resulting in no change in load factor. C- increase the rate of turn resulting in no change in load factor. Comm.

8 Aviation Seminars8 Sorry that is Incorrect. Go Back and Try Again.

9 Aviation Seminars9 That’s Right!!! Next Question

10 Aviation Seminars10 #5604. Why should flight speeds above ‘Vne’ be avoided? A- Excessive induced drag will result in structural failure. B- Design limit load factors may be exceeded, if gusts are encountered. C- Control effectiveness is so impaired that the aircraft becomes uncontrollable. Comm.

11 Aviation Seminars11 Sorry that is Incorrect. Go Back and Try Again.

12 Aviation Seminars12 That’s Right!!! Next Question

13 Aviation Seminars13 #3012. After takeoff, which airspeed would permit the pilot to gain the most altitude in a given period of time? A- Vy. B- Vx. C- Va.

14 Aviation Seminars14 Sorry that is Incorrect. Go Back and Try Again.

15 Aviation Seminars15 That’s Right!!! Next Question

16 Aviation Seminars16 #3267. The maximum speed at which the airplane can be operated in smooth air is A- 100 MPH. B- 165 MPH. C- 208 MPH.

17 Aviation Seminars17 Sorry that is Incorrect. Go Back and Try Again.

18 Aviation Seminars18 That’s Right!!! Next Question

19 Aviation Seminars19 #3256. What is true altitude? A- The vertical distance of the aircraft above sea level. B- The vertical distance of the aircraft above the surface. C- The height above the standard datum plane.

20 Aviation Seminars20 Sorry that is Incorrect. Go Back and Try Again.

21 Aviation Seminars21 That’s Right!!! Next Question

22 Aviation Seminars22 #3252. Altimeter 3 indicates A- 9,500 feet. B- 10,950 feet. C- 15, 940 feet.

23 Aviation Seminars23 Sorry that is Incorrect. Go Back and Try Again.

24 Aviation Seminars24 That’s Right!!! Next Question

25 Aviation Seminars25 # 5210. If airspeed is increased during a level turn, what action would be necessary to maintain altitude? A- The angle of attack and angle of bank must be decreased. B- The angle of attack must be increased or angle of bank decreased. C- The angle of attack must be decreased or angle of bank increased. Comm.

26 Aviation Seminars26 Sorry that is Incorrect. Go Back and Try Again.

27 Aviation Seminars27 That’s Right!!! Next Question

28 Aviation Seminars28 #3990. If a flight is made from an area of low pressure into an area of high pressure without the altimeter setting being adjusted and a constant indicated altitude is maintained, the altimeter would indicate A- the actual altitude above sea level. B- higher than the actual altitude above sea level. C- lower than the actual altitude above sea level.

29 Aviation Seminars29 Sorry that is Incorrect. Go Back and Try Again.

30 Aviation Seminars30 That’s Right!!! Next Question

31 Aviation Seminars31 #3255. How do variations in temperature affect the altimeter? A- Pressure levels are raised on warm days and the indicated altitude is lower than true altitude. indicated altitude is lower than true altitude. B- High temperatures expand the pressure levels and the indicated altitude is higher than true altitude. C- Lower temperatures lower the pressure levels and the indicated altitude is lower than true altitude.

32 Aviation Seminars32 Sorry that is Incorrect. Go Back and Try Again.

33 Aviation Seminars33 That’s Right!!! Next Question

34 Aviation Seminars34 #3279. Deviation in a magnetic compass is caused by A- presence of flaws in the permanent magnets of the compass. B- the difference in the location between true north and magnetic north. C- magnetic fields within the aircraft distorting the lines of magnetic force.

35 Aviation Seminars35 Sorry that is Incorrect. Go Back and Try Again.

36 Aviation Seminars36 That’s Right!!! Next Question

37 Aviation Seminars37 #3280. In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward the west if A- a left turn is entered from a north heading. B- a right turn is entered from a north heading. C- an aircraft is accelerated while on a north heading.

38 Aviation Seminars38 Sorry that is Incorrect. Go Back and Try Again.

39 Aviation Seminars39 That’s Right!!! Next Question

40 Aviation Seminars40 #3283. In the Northern Hemisphere, the magnetic compass will normally indicate a turn toward the south when A- a left turn is entered from an east heading. B- a right turn is entered from a west heading. C- the aircraft is decelerated while on a west heading.

41 Aviation Seminars41 Sorry that is Incorrect. Go Back and Try Again.

42 Aviation Seminars42 That’s Right!!! Next Question

43 Aviation Seminars43 #3278. How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated? A- The direction of deflection of the banking scale (A). B- The direction of deflection of the horizon bar (B). C- The relationship of the miniature airplane (C) to the deflected horizon bar (B).

44 Aviation Seminars44 Sorry that is Incorrect. Go Back and Try Again.

45 Aviation Seminars45 That’s Right!!! Next Question

46 Aviation Seminars46 #5268. What is an operational difference between the turn coordinator and the turn-and-slip indicator? A- The turn coordinator is always electric; the turn- and-slip indicator is always vacuum-driven. B- The turn coordinator indicates bank angle only; the turn-and-slip indicator indicates rate of turn and coordination. C- The turn coordinator indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination. Comm.

47 Aviation Seminars47 Sorry that is Incorrect. Go Back and Try Again.

48 Aviation Seminars48 That’s Right!!! Move on to the Next Section!!!


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