Embraer 190 - Fire Protection

35 Questions | Total Attempts: 1135

SettingsSettingsSettings
Please wait...
Embraer Quizzes & Trivia

FIRE PROTECTION QUIESTIONS MADE FROM AOM VOL. 2GOOD LUCK!SANTIAGO STOCKER.


Questions and Answers
  • 1. 
    The fire protection system provides fire detection and extinguishing capabilities for:
    • A. 

      Engines, APU, Cargo Compartments and Lavatories.

    • B. 

      Engines, APU and Lavatories.

  • 2. 
    The Engine fire DETECTION electrical power is supplied by:
    • A. 

      DC ESS BUSES

    • B. 

      HOT BATT BUS 1 and HOT BATT BUS 2

  • 3. 
    The Engine fire EXTINGUISHING electrical power is supplied by:
    • A. 

      HOT BATT BUS 1 and HOT BATT BUS 2

    • B. 

      DC ESS BUSES

  • 4. 
    The Engine Fire Detection System is monitored by __________________________ . When a fire condition is detected the signal goes to the MAU which generates the associated EICAS messages and alarms.
    • A. 

      One detector loop

    • B. 

      Two detector loops

  • 5. 
    Anytime the fire handle is pulled it commands the following shutoff valves to close:
    • A. 

      The engine fuel shutoff valve; and the engine hydraulic shutoff valves.

    • B. 

      The engine fuel shutoff valve only.

    • C. 

      The engine fuel shutoff valve; the engine hydraulic shutoff valves and; the engine bleed air shutoff valve.

  • 6. 
    A total of ____ fire extinguisher bottles named A and B are installed in the airplane to serve either or both engines. 
    • A. 

      Two

    • B. 

      Three

  • 7. 
    When an engine fire extinguishing bottle is discharged, fire handle illumination may be lost. In this case if the CAS message is still active the fire condition ...
    • A. 

      Persists.

    • B. 

      Does not persists.

  • 8. 
    The  APU fire DETECTION electrical power is supplied by:
    • A. 

      DC ESS BUSES

    • B. 

      HOT BATT BUS 1 and HOT BATT BUS 2

  • 9. 
    The APU fire EXTINGUISHING electrical power is supplied by: – APU fire extinguishing:  
    • A. 

      HOT BATT BUS 1 and HOT BATT BUS 2.

    • B. 

      DC ESS BUS 2

  • 10. 
    The APU Fire Detection System is comprised of ___ detectors loops. 
    • A. 

      Two

    • B. 

      Three

  • 11. 
    When a fire condition is detected the signal goes to the ____ which generates the associated EICAS messages and alarms.
  • 12. 
    When the APU FIRE EXTINGUISHER button is pressed the system:
    • A. 

      Discharges the APU fire bottle, shuts down the APU through the APU FADEC, closes the APU fuel shutoff valve (SOV) and displays an EICAS ADVISORY message APU FIREX BTL DISCH.

    • B. 

      Discharges the APU fire bottle, shuts down the APU through the APU FADEC and displays an EICAS ADVISORY message APU FIREX BTL DISCH.

    • C. 

      Discharges the APU fire bottle, closes the APU fuel shutoff valve (SOV) and displays an EICAS ADVISORY message APU FIREX BTL DISCH.

  • 13. 
    _____ fire-extinguishing bottle is installed in the rear fuselage. 
    • A. 

      One

    • B. 

      Two

  • 14. 
    As soon as the APU EMER STOP pushbutton is pressed the red strip bar is replaced by the white stripe bar indicating that ...
    • A. 

      The APU has shut down.

    • B. 

      The APU fire detection has detect fire.

  • 15. 
    After the APU EMER STOP pushbutton is pressed the APU fire extinguisher pushbutton illuminates indicating that ...
    • A. 

      The extinguisher bottle is not armed.

    • B. 

      The extinguisher bottle is armed.

  • 16. 
    When an APU fire is detected, the upper half of the button illuminates ...
    • A. 

      White.

    • B. 

      Red.

  • 17. 
    If a fire condition is still present and the APU emergency stop button is not pressed, the APU fire extinguisher pushbutton illuminates after ________ indicating that the extinguisher bottle is armed. 
    • A. 

      1 minute

    • B. 

      2 minutes

  • 18. 
    On ground, the APU will automatically shut down __________ after the fire condition is present.
    • A. 

      60 seconds

    • B. 

      10 seconds

  • 19. 
    The forward and aft cargo compartments on the E-JETS are ...
    • A. 

      Class A.

    • B. 

      Class B.

    • C. 

      Class C.

  • 20. 
    _____________________ are protected by the CARGO SMOKE DETECTION SYSTEM and CARGO FIRE PROTECTION SYSTEM. 
    • A. 

      The forward cargo compartment

    • B. 

      The aft cargo compartment

    • C. 

      Both cargo compartments

  • 21. 
    Each cargo compartment has  ________________ smoke detection system. 
    • A. 

      The same

    • B. 

      An independent

  • 22. 
    After fire or smoke is detected in the forward cargo compartment the following actions are automatically commanded by the system:
    • A. 

      Air circulation fan is turned off; The FWD fire extinguishing bottle is armed and; The forward cargo compartment ventilation outflow valve is commanded closed.

    • B. 

      The AFT fire extinguishing bottle is armed.

  • 23. 
    After fire or smoke is detected in the aft cargo compartment the following action is automatically commanded by the system:
    • A. 

      Air circulation fan is turned off; and; The forward cargo compartment ventilation outflow valve is commanded closed.

    • B. 

      The AFT fire extinguishing bottle is armed.

  • 24. 
    The Cargo Fire Extinguishing System is comprised of:
    • A. 

      One high-rate extinguisher bottle and; One low-rate extinguisher bottle.

    • B. 

      Two high-rate extinguisher bottle and; Two low-rate extinguisher bottle.

  • 25. 
    Both extinguisher bottles are installed in the ______________________ and used in either forward or aft cargo compartment.
    • A. 

      Center avionics bay

    • B. 

      Forward avionics bay

Back to Top Back to top