Embraer 190 - Aircraft Limitations

77 Questions | Total Attempts: 1214

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Embraer Quizzes & Trivia

LIMITATIONS QUESTIONS MADE FROM AOM VOL. 1 GOOD LUCK!SANTIAGO STOCKER.


Questions and Answers
  • 1. 
    Wich is the Max. Landing Weight (MLW)?  
    • A. 

      51960 KG

    • B. 

      51800 KG

    • C. 

      44000 KG

    • D. 

      40900 KG

  • 2. 
    Wich is the Max. Ramp Weight (MRW)?
    • A. 

      51960 KG

    • B. 

      51800 KG

    • C. 

      44000 KG

    • D. 

      40900 KG

  • 3. 
    Wich is the Max. Takeoff Weight (MTOW)?  
    • A. 

      51960 KG

    • B. 

      51800 KG

    • C. 

      44000 KG

    • D. 

      40900 KG

  • 4. 
    Wich is the Max. Zero Fuel Weight (MZFW)?
    • A. 

      51960 KG

    • B. 

      51800 KG

    • C. 

      44000 KG

    • D. 

      40900 KG

  • 5. 
    The maximum landing gear extended and locked speed is _____ KIAS.
  • 6. 
    The maximum landing gear extension speed is _____ KIAS.
  • 7. 
    The maximum landing gear retraction speed is _____ KIAS.
  • 8. 
    Maximum Altitude For Flap Extension is ________ ft. (no numbers or comas on the answer, e.g: "50000")
  • 9. 
    The maximum flap extended speed for flaps 1 is _____ KIAS.
  • 10. 
    The maximum flap extended seep for flaps 2 is _____ KIAS.
  • 11. 
    The maximum flap extended seep for flaps 3 is _____ KIAS.
  • 12. 
    The maximum flap extended seep for flaps 4 is _____ KIAS.
  • 13. 
    The maximum flap extended seep for flaps 5 is _____ KIAS.
  • 14. 
    The maximum flap extended seep for flaps FULL is _____ KIAS.
  • 15. 
    Maximum Tire Ground Speed is _____ kt.
  • 16. 
    Maximum Takeoff and Landing Tailwind Component is _____ kt.  is ________
  • 17. 
    Maximum crosswind Dry Runway is _____ kt.
  • 18. 
    Maximum crosswind Wet Runway is _____ kt.
  • 19. 
    Maximum crosswind Runway with Compacted Snow is _____ kt.
  • 20. 
    Maximum crosswind Runway with Standing Water/Slush/Wet Snow/Dry Snow is _____ kt.
  • 21. 
    Maximum crosswind Runway with Ice (no melting) _____ kt.
  • 22. 
    Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than _____ kt. 
  • 23. 
    Maximum usable quantity per wing tank is ________ kg.  is
  • 24. 
    Maximum permitted imbalance between wing tanks is ______ kg
  • 25. 
    Minimum fuel tank temperature altitude is ______ ºC
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