Piper Seminole Aircraft Systems

25 Questions | Total Attempts: 158

SettingsSettingsSettings
Piper Seminole Aircraft Systems - Quiz

Instructions. Please read. After completing Unit 3 of the Multiengine Addon Training Course, you must take this quiz. The minimum passing grade is 80%. If you fail the quiz, please review Unit 3. Put special attention on the questions you got wrong in the quiz. You may retake the quiz until you get 80% at least. After successfully completing the quiz, you will get a completion certificate that you must download and keep in your records as proof of passing this quiz. This certificate is a requirement to receive credit for the Unit and graduation of the Course. Please type your name in the fields below for your completion certificate after passing the quiz.


Questions and Answers
  • 1. 
    Which type of engines is the seminole equipped with?
    • A. 

      Lycoming TO-320

    • B. 

      Continental TIO-520

    • C. 

      Lycoming (L)TO-360

    • D. 

      Continental O-200

  • 2. 
    What is the rated power of the Piper Turbo Seminole engines?
    • A. 

      200 horsepower at 2700 RPM

    • B. 

      180 horsepower at 2700 RPM

    • C. 

      160 horsepower at 2575 RPM

    • D. 

      180 horsepower at 2575 RPM

  • 3. 
    How is the propeller driven on the Piper Turbo Seminole engines?
    • A. 

      Reduction Gearbox Drive

    • B. 

      Direct Drive

    • C. 

      Non-Direct Drive

  • 4. 
    The Piper Turbo Seminole engines are not susceptible to induction icing:
    • A. 

      True

    • B. 

      False

  • 5. 
    How many blades does the propeller of each engine has?
    • A. 

      1 blade

    • B. 

      2 blades

    • C. 

      3 blades

    • D. 

      4 blades

  • 6. 
    This is the capability of a propeller to change the blade angle:
    • A. 

      Full Feathering

    • B. 

      Constant Speed

    • C. 

      Controllable Pitch

  • 7. 
    This is the capability of the propeller blades to align with the relative wind to decrease drag:
    • A. 

      Full Feathering

    • B. 

      Constant Speed

    • C. 

      Controlable Pitch

  • 8. 
    The propeller governor constantly varies oil pressure into the propeller hub to change the propeller blade pitch. This is known as:
    • A. 

      Full Feathering

    • B. 

      Constant Speed

    • C. 

      Controlable Pitch

  • 9. 
    Regardless of the propeller lever position, what will happen when oil pressure is lost?
    • A. 

      Propeller will not feather.

    • B. 

      Propeller will feather if the RPM are above 950

    • C. 

      Propeller will feather if the RPM are below 950

    • D. 

      Propeller will feather regardless of the RPM

  • 10. 
    The landing gear on the Seminole is:
    • A. 

      Manually operated

    • B. 

      Electrically operated

    • C. 

      Hydraulically actuated, electrically operated

    • D. 

      Electrically actuated, hydraulically operated

  • 11. 
    The landing gear is held up by:
    • A. 

      Mechanical up locks 

    • B. 

      Hydraulic pressure

    • C. 

      Electrical actuators

    • D. 

      Spring system

  • 12. 
    The landing gear horn will sound:
    • A. 

      When power is approximately below 15” with the landing gear up

    • B. 

      Airspeed is below 88 KIAS and the gear is up

    • C. 

      Flaps 25 or 40 are selected and the landing gear is not down

    • D. 

      Landing gear handle is selected up on ground

    • E. 

      RPMs drop below 2300 and the landing gear is up

  • 13. 
    Gear retraction on ground is prevented by:
    • A. 

      Squat switch on the right main landing gear

    • B. 

      Squat switch on the left main landing gear

    • C. 

      Landing gear handle

    • D. 

      Hydraulic pressure trapped by a valve

  • 14. 
    If hydraulic pressure is lost, the landing gear:
    • A. 

      Won’t operate up or down

    • B. 

      Will free fall down

    • C. 

      Will stay up

  • 15. 
    Emergency landing gear extension is limited to:
    • A. 

      88 KIAS

    • B. 

      100 KTAS

    • C. 

      100 KIAS

    • D. 

      140 KIAS

  • 16. 
    The Seminole is equipped with brakes on:
    • A. 

      Main landing gear

    • B. 

      Nose landing gear

    • C. 

      Nose and main landing gear

  • 17. 
    Parking brake is permitted to be used during training flights at TecBlue:
    • A. 

      True

    • B. 

      False

  • 18. 
    The Seminole is equipped with this type of flap system
    • A. 

      Electrical

    • B. 

      Hydraulic

    • C. 

      Pneumatic 

    • D. 

      Manual

  • 19. 
    The Piper Seminole has the following wing flaps positions:
    • A. 

      0

    • B. 

      5

    • C. 

      10

    • D. 

      20

    • E. 

      25

    • F. 

      30

    • G. 

      36

    • H. 

      40

    • I. 

      46

  • 20. 
    Pitot tube and static port are combined together and located on the:
    • A. 

      Nose

    • B. 

      Left wing

    • C. 

      Right wing

    • D. 

      Tail

  • 21. 
    Total usable fuel on the Piper Seminole is:
    • A. 

      100 gals (50 per side)

    • B. 

      108 gals (54 per side)

    • C. 

      110 gals (55 per side)

    • D. 

      116 gals (58 per side

  • 22. 
    The electrical system on the Piper Seminole is:
    • A. 

      12 Volt

    • B. 

      14 Volt

    • C. 

      24 Volt

    • D. 

      28 Volt

  • 23. 
    How many alternators is the Piper Seminole equipped with?
    • A. 

      1 on the left engine

    • B. 

      1 on the right engine

    • C. 

      2, one on each engine

    • D. 

      None

  • 24. 
    The inboard stall warning detector provides stall warning at:
    • A. 

      Flaps 0

    • B. 

      Flaps 10 & 25

    • C. 

      Flaps 25 & 40

    • D. 

      Flaps 40

  • 25. 
    The squat switch has two functions on the Piper Seminole when it is on ground:
    • A. 

      Prevents the propeller from feathering

    • B. 

      Removes power from the hydraulic pump

    • C. 

      Disable radio communications 

    • D. 

      Deactivates the stall warning

Back to Top Back to top