AP Flight Final Exam Trimester 1

79 Questions | Total Attempts: 39

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Engineering Quizzes & Trivia

All questions pertain to the Private Pilot Textbook and the Private Pilot Maneuvers Binded Book. Total Questions: 80 Allotted Time: 1:30


Questions and Answers
  • 1. 
    • A. 

      Approved Airplane Flight Manual (AFM)

    • B. 

      Pilot's Operating Handbook (POH)

    • C. 

      An appropriate checklist for your airplane

    • D. 

      Private Pilot Maneuvers (PPM)

  • 2. 
    • A. 

      Water is more dense, therefore it sinks to the bottom of the test tube

    • B. 

      Water is less dense, therefore it rises to the top of the test tube

    • C. 

      Water is neither more nor less dense than fuel, therefore it will mix with the fuel

    • D. 

      You must ask the mechanic specialist

  • 3. 
    • A. 

      Avco Lycoming, O-352-L2C

    • B. 

      Avco Lycoming, O-253-L2C

    • C. 

      Avco Lycoming, O-325-L2C

    • D. 

      Avco Lycoming, O-235-L2C

  • 4. 
    • A. 

      100 rated BHP at 1550 RPM

    • B. 

      110 rated BHP at 2550 RPM

    • C. 

      110 rated BHP at 1550 RPM

    • D. 

      100 rated BHP at 2550 RPM

  • 5. 
    • A. 

      67 in. & 65.5 in.

    • B. 

      68 in. & 66.5 in.

    • C. 

      69 in. & 67.5 in.

    • D. 

      70 in. & 68.5 in.

  • 6. 
    • A. 

      Constant Speed

    • B. 

      Fixed Pitch

    • C. 

      Metal Propellers

    • D. 

      Controllable Pitch

  • 7. 
    • A. 

      25 psi & 110 psi

    • B. 

      25 psi & 105 psi

    • C. 

      20 psi & 90 psi

    • D. 

      25 psi & 100 psi

  • 8. 
    • A. 

      1670 lbs.

    • B. 

      1675 lbs.

    • C. 

      1680 lbs.

    • D. 

      1685 lbs.

  • 9. 
    • A. 

      23

    • B. 

      24

    • C. 

      25

    • D. 

      26

  • 10. 
    • A. 

      100LL & 80/87

    • B. 

      100LL & 100/130

    • C. 

      100LL & Jet

    • D. 

      100LL Only

  • 11. 
    • A. 

      +4.4g, -1.76g

    • B. 

      +4.4g, -1.75g

    • C. 

      +3.5g, -1.76g

    • D. 

      +3.5g, -1.75g

  • 12. 
    • A. 

      0.5

    • B. 

      1

    • C. 

      1.5

    • D. 

      2

  • 13. 
    KCAS
  • 14. 
    KIAS
  • 15. 
    KTAS
  • 16. 
    VA
  • 17. 
    VNO
  • 18. 
    Vx
  • 19. 
    Vy
  • 20. 
    OAT
  • 21. 
    BHP
  • 22. 
    RPM
  • 23. 
    CG
  • 24. 
    During the preflight inspection inside the cabin, what is the first thing you should do?
    • A. 

      Turn the Master Switch ON

    • B. 

      Turn the Ignition Switch ON

    • C. 

      Remove the Control Wheel Lock

    • D. 

      Turn the Fuel Shutoff Valve ON

  • 25. 
    If you are taxiing with winds coming from your 315˚, how would you position the flight controls?
    • A. 

      Use up aileron on the left hand wing and neutral elevator

    • B. 

      Use up aileron on the right hand wing and neutral elevator

    • C. 

      Use down aileron on the left hand wing and down elevator

    • D. 

      Use down aileron on the right hand wing and down elevator

  • 26. 
    You may not operate this aircraft with an oil level of less than how many quarts?
    • A. 

      6 quarts

    • B. 

      5 quarts

    • C. 

      4 quarts

    • D. 

      3 quarts

  • 27. 
    The C-152 is approved for intentional spins
    • A. 

      True

    • B. 

      False

  • 28. 
    • A. 

      Apply brakes to slow down

    • B. 

      Use differential braking

    • C. 

      Retard the throttle to slow down

    • D. 

      There is no possible way

  • 29. 
    If the altimeter setting is not available during the before takeoff check, you can adjust the altimeter to agree with field elevation.
    • A. 

      True

    • B. 

      False

  • 30. 
    Unless you are assigned a discrete transponder code, you should use 1220 for VFR flight
    • A. 

      True

    • B. 

      False

  • 31. 
    You should install the control lock before engine shutdown.
    • A. 

      True

    • B. 

      False

  • 32. 
    To maintain straight-and-level flight, you normally need to make a continuous series of small adjustments in pitch and bank.
    • A. 

      True

    • B. 

      False

  • 33. 
    As the pitch attitude is increased and the airspeed decreases, left-turning tendencies become less pronounced.
    • A. 

      True

    • B. 

      False

  • 34. 
    You can control your rate of descent with pitch attitude.
    • A. 

      True

    • B. 

      False

  • 35. 
    You can decrease your descent rate by lowering the flaps.
    • A. 

      True

    • B. 

      False

  • 36. 
    During a level turn, you maintain the same amount of aileron deflection throughout the turn.
    • A. 

      True

    • B. 

      False

  • 37. 
    As your airspeed decreases, you should anticipate the need for increasing right rudder pressure.
    • A. 

      True

    • B. 

      False

  • 38. 
    After recovering from a stall, you should climb at Vx
    • A. 

      True

    • B. 

      False

  • 39. 
    You should execute a power-on stall at a high airspeed using high power.
    • A. 

      True

    • B. 

      False

  • 40. 
    An applicant for a private pilot certificate is required to demonstrate flight proficiency with regard to stalls and spins.
    • A. 

      True

    • B. 

      False

  • 41. 
    Any airplane can be used to perform an accelerated stall.
    • A. 

      True

    • B. 

      False

  • 42. 
    A private pilot applicant must be able to demonstrate flight proficiency in elevator trim stalls.
    • A. 

      True

    • B. 

      False

  • 43. 
    In comparison to the roll-in, you need more rudder and aileron pressure during the roll-out from a steep turn.
    • A. 

      True

    • B. 

      False

  • 44. 
    • A. 

      November 21, 1783

    • B. 

      December 17, 1903

    • C. 

      December 23, 1986

    • D. 

      May 21, 1927

  • 45. 
    • A. 

      November 21, 1783

    • B. 

      December 17, 1903

    • C. 

      December 23, 1986

    • D. 

      May 21, 1927

  • 46. 
    • A. 

      November 21, 1783

    • B. 

      December 17, 1903

    • C. 

      December 23, 1986

    • D. 

      May 21, 1927

  • 47. 
    • A. 

      9 days, 3 minutes

    • B. 

      9 days, 5 minutes

    • C. 

      9 days, 7 minutes

    • D. 

      9 days, 9 minutes

  • 48. 
    Airplanes, Rotorcrafts, Gliders, Lighter-Than-Air, and Powered-Lifts are grouped into to what?
    • A. 

      Type

    • B. 

      Class

    • C. 

      Category

    • D. 

      Rating

  • 49. 
    Single-Engine Land, Multi-Engine Sea, Multi-Engine land, and Single-Engine Sea are all types of...
    • A. 

      Gliders

    • B. 

      Powered-Lifts

    • C. 

      Rotorcraft

    • D. 

      Airplanes

  • 50. 
    • A. 

      Aerial Application, Corporate Flying, The Coast Guard

    • B. 

      Aerial Application, Corporate Flying, Military Aviation

    • C. 

      Flight Instructing, Regional Airlines, Major Airlines

    • D. 

      Flight Instructing, Regional Airlines, The Ninety-Nines Inc.

  • 51. 
    • A. 

      Rotorcraft Ratings, Airplane Class Ratings, Category and Class Ratings

    • B. 

      Additional Pilot Ratings, Airplane Class Ratings, Category and Class Ratings

    • C. 

      Multi-Engine Ratings, Seaplane Ratings, and Rotorcraft Ratings

    • D. 

      Instrument Rating, Seaplane Ratings, and Rotorcraft Ratings

  • 52. 
    Name the parts of the airplane.
  • 53. 
    The rudder is located on the horizontal stabilizer.
    • A. 

      True

    • B. 

      False

  • 54. 
    As an airplane climbs, do you enrichen or lean the mixture to maintain an optimum fuel/air ratio?
    • A. 

      Enrichen

    • B. 

      Lean

  • 55. 
    If the fuel grade specified for your airplane is not available, can you use a lower grade of fuel? A higher grade?
  • 56. 
    The four forces of flight are...
  • 57. 
    Aspect Ratio: Wing Span = 196 ft Average Chord = 28 ft
  • 58. 
    Aspect Ratio: Wing Span = 35 ft Average Chord = 5 ft
  • 59. 
    Aspect Ratio: Wing Span = 37 ft Average Chord = 11 ft
  • 60. 
    Aspect Ratio: Wing Span = 69 ft Average Chord = 12 ft
  • 61. 
    Aspect Ratio: Wing Span = 156 ft Average Chord = 24 ft
  • 62. 
    Name the three axes of flight.
  • 63. 
    Name two types of stalls.
  • 64. 
    Name the three types of spins.
  • 65. 
    Given: Limit Load factor (n): 3.8G's Maximum weight (W1): 2,400 lbs. Stall speed at maximum weight (Vs): 51 KCAS
  • 66. 
    Given: Can you determine the maneuvering speed for a Boeing 727 approaching to land at 122,000 lbs? Va at maximum landing weight: 200 KIAS Maximum landing weight: 137,500 lbs.
  • 67. 
    Class A airspace begins at what altitude?
    • A. 

      18,000 feet MSL

    • B. 

      14,500 feet MSL

    • C. 

      10,000 feet MSL

    • D. 

      5,000 feet MSL