Cessna 182 Handbook Exam

27 Questions | Total Attempts: 128

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Handbook Exam Quizzes & Trivia

Questions and Answers
  • 1. 
    Maximum take-off mass is
    • A. 

      1750 lbs (794kg)

    • B. 

      2450 lbs (1111kg)

    • C. 

      2800 lbs (1270kg)

    • D. 

      4000 lbs (1814kg)

  • 2. 
    Service ceiling is
    • A. 

      12 500 feet

    • B. 

      15 900 feet

    • C. 

      18 900 feet

    • D. 

      19 500 feet

  • 3. 
    Empty mass (Standard aircraft)
    • A. 

      1691 lbs (767 kg)

    • B. 

      2100 lbs (953 kg)

    • C. 

      1620 lbs (735kg)

    • D. 

      2303 lbs (1045 kg)

  • 4. 
    Maximum baggage mass
    • A. 

      50 lbs

    • B. 

      100 lbs

    • C. 

      120 lbs

    • D. 

      150 lbs

  • 5. 
    Maximum engine brake horse power at 2600 RPM
    • A. 

      180hp

    • B. 

      200hp

    • C. 

      230hp

    • D. 

      250hp

  • 6. 
    Vr
    • A. 

      55 mph

    • B. 

      60 mph

    • C. 

      65 mph

    • D. 

      67 mph

  • 7. 
    To minimize engine wear manifold pressure and RPM should be reduced after take-off to
    • A. 

      25 " and 2500 RPM

    • B. 

      23” and 2450 RPM

    • C. 

      21" and 2450 RPM

    • D. 

      23" and 2500 RPM

  • 8. 
    Approach speed with full flaps
    • A. 

      70 mph

    • B. 

      80 mph

    • C. 

      85 mph

    • D. 

      90 mph

  • 9. 
    Fuel capasity is
    • A. 

      79 gallons usable and 2 gallons unusable

    • B. 

      79 gallons usable and 1.5 gallons unusable

    • C. 

      77 gallons usable and 1.5 gallons unusable

    • D. 

      77 gallons usable and 2.0 gallons unusable

  • 10. 
    Prolonged uncoordinated flight, such as slips or skids can cause engine stoppage
    • A. 

      If fuel pump is not being operated

    • B. 

      If there is less than 1/4 of fuel in the tanks

    • C. 

      If there is less than 1/3 of fuel in the tanks

    • D. 

      If fuel selector should be selected for either left or right tank

  • 11. 
    Which is correct regarding the fuel system
    • A. 

      Fuel from each wing taken is drawn by aid of fuel pump to a selector valve. From there it flows through a fuel strainer and carburetor to the engine manifold.

    • B. 

      Fuel from each wing taken flows by gravity to a fuel strainer. From there it flows through a selector valve and carburetor to the engine induction system.

    • C. 

      Fuel from each wing taken flows by gravity to a selector valve. From there it flows through a fuel strainer and carburetor to the engine manifold.

    • D. 

      Fuel from each wing taken flows by gravity to a selector valve. From there it flows through a fuel strainer and carburetor to the engine induction system.

  • 12. 
    Fuel tank selector must be selected for
    • A. 

      Both tanks

    • B. 

      The left tank

    • C. 

      The right tank

    • D. 

      The fullest tank

  • 13. 
    Electrical system is
    • A. 

      14 volt and storage battery is 12 volt

    • B. 

      24 volt and storage battery is 22 volt

    • C. 

      12 volt and storage battery is 14 volt

    • D. 

      24 volt and storage battery is 20 volt

  • 14. 
    During engine start puffs of black smoke from the exhaust stack indicate
    • A. 

      A too weak mixture

    • B. 

      Water in the fuel

    • C. 

      Worn piston rings

    • D. 

      Over priming or flooding

  • 15. 
    During magneto check on the ground
    • A. 

      RPM must drop but should not be more than 50 RPM

    • B. 

      RPM should not drop more than 50 RPM

    • C. 

      RPM must not increase more than 50 RPM

    • D. 

      RPM must drop by 50 RPM

  • 16. 
    Vx is (IAS in mph)
  • 17. 
    Vy is (IAS in mph)
  • 18. 
    For short field take-off which of the following flap settings should be used
    • A. 

      10°

    • B. 

      20°

    • C. 

      30°

    • D. 

      40°

  • 19. 
    Load factors are
    • A. 

      +4.4 to -1.52

    • B. 

      +4.4 to –1.76

    • C. 

      +3.8 to -1.76

    • D. 

      +3.8 to -1.52

  • 20. 
    Vne is (IAS in mph)
  • 21. 
    Vno is (IAS in mph)
  • 22. 
    Vfe is (IAS in mph)
  • 23. 
    Va is (IAS in mph)
  • 24. 
    Minimum oil quantity in quarts
  • 25. 
    Vs1 is (IAS in mph)
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