(Refer to Figure 4.) What Is the Maximum Structural Cruising Speed?

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ane. What force makes an airplane turn?

A. The horizontal component of lift. B. The vertical component of lift. C. Centrifugal force.

3301

2. V_NO is defined as the

A. normal operating range. B. never-exceed speed. C. maximum structural cruising speed.

3009

3. (Refer to Figure 72.) The positive limit load factor is represented past the

A. vertical solid line from D to G. B. horizontal dashed line from C to point E. C. vertical dashed line from Eastward to F.

Figure 72

4167

4. (Refer to Figure 4.) Which colour identifies the normal flap operating range?

A. The lower limit of the white arc to the upper limit of the light-green arc. B. The green arc. C. The white arc.

Figure four

3271

5. (Refer to Figure iv.) Which color identifies the ability-off stalling speed with fly flaps and landing gear in the landing configuration?

A. Upper limit of the greenish arc. B. Upper limit of the white arc. C. Lower limit of the white arc.

Figure 4

3272

6. (Refer to Figure 2.) If an aeroplane weighs four,500 pounds, what approximate weight would the airplane structure exist required to support during a 45° banked turn while maintaining altitude?

A. 4,500 pounds. B. half dozen,300 pounds. C. vii,200 pounds.

Figure two

3216

7. The angle of assault at which an airplane wing stalls will

A. increase if the CG is moved frontward. B. change with an increase in gross weight. C. remain the aforementioned regardless of gross weight.

3311

eight. (Refer to Figure 1.) The acute bending A is the angle of

A. incidence. B. set on. C. dihedral.

Figure 1

3203

9. The amount of excess load that can exist imposed on the wing of an airplane depends upon the

A. position of the CG. B. speed of the airplane. C. abruptness at which the load is applied.

3217

x. What is the purpose of the rudder on an aeroplane?

A. To control yaw. B. To command overbanking tendency. C. To control roll.

3213

11. The left turning tendency of an plane caused by P-factor is the result of the

A. clockwise rotation of the engine and the propeller turning the airplane counter-clockwise. B. propeller blade descending on the right producing more thrust than the ascending blade on the left. C. gyroscopic forces applied to the rotating propeller blades interim 90° in advance of the point the force was applied.

3208

12. What is the relationship of lift, elevate, thrust, and weight when the airplane is in straight-and-level flight?

A. Elevator equals weight and thrust equals elevate. B. Elevator, drag, and weight equal thrust. C. Lift and weight equal thrust and drag.

3205

13. V_{And so} is divers as the

A. stalling speed or minimum steady flight speed in the landing configuration. B. stalling speed or minimum steady flying speed in a specified configuration. C. stalling speed or minimum takeoff safety speed.

3010

14. Wingtip vortices created past large aircraft tend to

A. sink below the aircraft generating turbulence. B. rise into the traffic pattern. C. ascension into the takeoff or landing path of a crossing runway.

3826

xv. The term "angle of attack" is defined as the angle between the

A. chord line of the wing and the relative wind. B. airplanes longitudinal axis and that of the air hit the airfoil. C. airplane's centerline and the relative wind.

3204

16. How will frost on the wings of an plane bear upon takeoff operation?

A. Frost will disrupt the smoothen menstruum of air over the wing, adversely affecting its lifting capability. B. Frost will change the camber of the fly, increasing its lifting capability. C. Frost will cause the aeroplane to get airborne with a higher angle of assail, decreasing the stall speed.

3206

17. Which basic flight maneuver increases the load gene on an plane as compared to straight-and-level flight?

A. Climbs. B. Turns. C. Stalls.

3218

xviii. Loading an plane to the most aft CG will cause the aeroplane to exist

A. less stable at all speeds. B. less stable at tedious speeds, merely more than stable at loftier speeds. C. less stable at loftier speeds, but more than stable at low speeds.

3288

19. What is ground outcome?

A. The result of the interference of the surface of the Earth with the airflow patterns about an airplane. B. The outcome of an alteration in airflow patterns increasing induced elevate about the wings of an airplane. C. The result of the disruption of the airflow patterns about the wings of an plane to the signal where the wings volition no longer support the plane in flight.

3312

20. When parting backside a heavy aircraft, the pilot should avert wake turbulence by maneuvering the shipping

A. beneath and downwind from the heavy aircraft. B. in a higher place and upwind from the heavy shipping. C. below and upwind from the heavy aircraft.

3830

21. Which Five-speed represents maximum landing gear extended speed?

A. V_LE. B. V_LO. C. V_{Atomic number 26}.

3008

22. How does the wake turbulence vortex circulate around each wingtip?

A. Inward, upward, and around each tip. B. Inward, upward, and counterclockwise. C. Outward, upward, and around each tip.

3989

23. Which Five-speed represents maximum flap extended speed?

A. V_{Atomic number 26}. B. Five_LOF. C. V_FC.

3007

24. When landing behind a big shipping, which process should be followed for vortex avoidance?

A. Stay above its final approach flightpath all the way to touchdown. B. Stay below and to one side of its final approach flightpath. C. Stay well below its final arroyo flightpath and land at least 2,000 feet backside.

3986

25. When does P-gene cause the airplane to yaw to the left?

A. When at low angles of assail. B. When at loftier angles of attack. C. When at loftier airspeeds.

3209

26. Which would provide the greatest gain in distance in the shortest distance during climb later on takeoff?

A. V_Y. B. 5_A. C. V_X.

3011

27. The four forces acting on an aeroplane in flight are

A. lift, weight, thrust, and drag. B. lift, weight, gravity, and thrust. C. elevator, gravity, ability, and friction.

3201

28. When are the iv forces that act on an airplane in equilibrium?

A. During unaccelerated flight. B. When the aircraft is accelerating. C. When the aircraft is at rest on the ground.

3202

29. The greatest vortex strength occurs when the generating aircraft is

A. light, dirty, and fast. B. heavy, dirty, and fast. C. heavy, clean, and slow.

3825

30. How does frost affect the lifting surfaces of an aeroplane on takeoff?

A. Frost may prevent the airplane from becoming airborne at normal takeoff speed. B. Frost will change the camber of the wing, increasing lift during takeoff. C. Frost may cause the aeroplane to become airborne with a lower angle of attack at a lower indicated airspeed.

3432

31. When landing behind a large shipping, the pilot should avoid wake turbulence by staying

A. in a higher place the large aircraft'southward final approach path and landing beyond the large aircraft's touchdown indicate. B. below the big aircraft's final approach path and landing before the large aircraft's touchdown point. C. higher up the large shipping's terminal approach path and landing earlier the big aircraft's touchdown point.

3829

32. During an arroyo to a stall, an increased load gene will cause the airplane to

A. stall at a higher airspeed. B. have a tendency to spin. C. be more difficult to control.

3316

33. What does the red line on an airspeed indicator represent?

A. Maneuvering speed. B. Turbulent or rough-air speed. C. Never-exceed speed.

3264

34. As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will

A. decrease every bit the true airspeed decreases. B. decrease as the truthful airspeed increases. C. remain the same regardless of altitude.

3263

35. What is an important airspeed limitation that is not colour coded on airspeed indicators?

A. Never-exceed speed. B. Maximum structural cruising speed. C. Maneuvering speed.

3274

36. Why is frost considered hazardous to flight?

A. Frost changes the bones aerodynamic shape of the airfoils, thereby increasing lift. B. Frost slows the airflow over the airfoils, thereby increasing control effectiveness. C. Frost spoils the shine flow of air over the wings, thereby decreasing lifting capability.

3431

37. Upon encountering severe turbulence, which flight status should the pilot endeavor to maintain?

A. Constant altitude and airspeed. B. Constant bending of attack. C. Level flight mental attitude.

3442

38. What must a pilot exist enlightened of as a event of ground result?

A. Wingtip vortices increase creating wake turbulence problems for arriving and parting shipping. B. Induced drag decreases; therefore, any excess speed at the bespeak of flare may crusade considerable floating. C. A total stall landing will require less upwardly elevator deflection than would a full stall when washed costless of ground effect.

3314

39. (Refer to Effigy 4.) What is the total flap operating range for the airplane?

A. 55 to 100 KTS. B. 60 to 208 KTS. C. 65 to 165 KTS.

Figure 4

3265

forty. What is one purpose of fly flaps?

A. To enable the pilot to make steeper approaches to a landing without increasing the airspeed. B. To salvage the pilot of maintaining continuous pressure level on the controls. C. To decrease wing area to vary the lift.

3220

41. One of the chief functions of flaps during arroyo and landing is to

A. decrease the bending of descent without increasing the airspeed. B. permit a touchdown at a higher indicated airspeed. C. increase the angle of descent without increasing the airspeed.

3219

42. The angle between the chord line of an airfoil and the relative wind is known as the angle of

A. elevator. B. attack. C. incidence.

3990

43. (Refer to Figure 4.) What is the caution range of the airplane?

A. 0 to 60 KTS. B. 100 to 165 KTS. C. 165 to 208 KTS.

Effigy iv

3266

44. (Refer to Figure 4.) Which marking identifies the never-exceed speed?

A. Upper limit of the green arc. B. Upper limit of the white arc. C. The red radial line.

Figure 4

3268

45. The condition that requires maximum caution when fugitive wake turbulence on landing is a

A. low-cal, quartering headwind. B. calorie-free, quartering tailwind. C. strong headwind.

3828

46. Changes in the heart of pressure of a wing affect the aircraft'due south

A. lift/elevate ratio. B. lifting capacity. C. aerodynamic rest and controllability.

3991

47. (Refer to Figure 4.) The maximum speed at which the airplane can be operated in smooth air is

A. 100 KTS. B. 165 KTS. C. 208 KTS.

Figure 4

3267

48. After takeoff, which airspeed would the airplane pilot employ to gain the most altitude in a given period of time?

A. V_Y. B. V_X. C. V_A.

3012

49. An airplane said to be inherently stable will

A. be difficult to stall. B. require less attempt to control. C. non spin.

3210

50. The speed at which a single flight control can be moved, one time, to its full revolt without run a risk of damage to the aircraft is

A. maneuvering speed. B. structural cruise speed. C. never exceed speed.

4144

51. (Refer to Figure 4.) What is the maximum structural cruising speed?

A. 100 KTS. B. 165 KTS. C. 208 KTS.

Effigy 4

3273

52. The angle of attack for a propeller is defined as

A. the angle betwixt the propeller chord line and the relative wind. B. the bending between the propeller chord line and the thrust vector. C. the pitch angle of the bract to the propeller hub.

4102

53. What determines the longitudinal stability of an plane?

A. The location of the CG with respect to the middle of lift. B. The effectiveness of the horizontal stabilizer, rudder, and rudder trim tab. C. The relationship of thrust and elevator to weight and drag.

3211

54. (Refer to Figure 4.) What is the maximum flaps-extended speed?

A. 65 KTS. B. 100 KTS. C. 165 KTS.

Figure four

3270

55. In what flight condition is torque outcome the greatest in a single-engine airplane?

A. Depression airspeed, high ability, loftier bending of attack. B. Depression airspeed, low ability, low bending of attack. C. Loftier airspeed, high ability, high angle of assault.

3207

56. Which argument relates to Bernoulli's principle?

A. For every action at that place is an equal and opposite reaction. B. An additional upward strength is generated every bit the lower surface of the wing deflects air down. C. Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the elevation surface.

3988

57. In what flight condition must an aircraft be placed in lodge to spin?

A. Partially stalled with i wing low. B. In a steep diving spiral. C. Stalled.

3309

58. (Refer to Figure 2.) If an plane weighs three,300 pounds, what approximate weight would the aeroplane structure be required to support during a 30° banked turn while maintaining altitude?

A. 1,200 pounds. B. 3,100 pounds. C. 3,960 pounds.

Figure 2

3215

59. Wingtip vortices are created but when an aircraft is

A. operating at high airspeeds. B. heavily loaded. C. developing lift.

3824

60. Which V-speed represents maneuvering speed?

A. V_A. B. V_LO. C. V_NE.

3006

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