Embraer 190 - Standard Operating Procedures Manual (Sopm)

39 Questions | Total Attempts: 489

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Embraer Quizzes & Trivia

GROUND OPERATIONS QUESTION MADE FROM S. O. P. MGOOD LUCK!SANTIAGO STOCKER.


Questions and Answers
  • 1. 
    In order to allow thermal stabilization of the engines, operate them at or near to IDLE for at least __________ before selecting higher thrust settings. 
    • A. 

      1 minutes

    • B. 

      2 minutes

    • C. 

      3 minutes

  • 2. 
    To avoid power interruptions, it is recommended to wait __________ after the N2 stabilizes before shutting the APU down or GPU disconnection, or to use the Electrical Synoptic Page to follow the power transfer.
    • A. 

      30 seconds

    • B. 

      1 minute

  • 3. 
    During start with low oil temperatures, the oil pressure may drop below the minimum oil pressure levels temporarily after start. If the oil pressure remains below minimum levels for more than ___________, the engine must be shut down and the oil heated.
    • A. 

      1 minutes

    • B. 

      2 minutes

    • C. 

      3 minutes

  • 4. 
    TO PREVENT DAMAGE TO NACELLE COMPONENTS, DO NOT ALLOW THE HOT AIR FROM THE GROUND CART TO EXCEED ...
    • A. 

      100°C

    • B. 

      200°C

  • 5. 
    DURING COLD WEATHER OPERATIONS, OIL PRESSURE PEAKS TO FULL SCALE MAY OCCUR DUE TO __________________. OIL PRESSURE SHOULD DECREASE AS THE OIL TEMPERATURE INCREASES. IF THE OIL PRESSURE REMAINS ABOVE NORMAL OPERATING RANGE, THE ENGINE SHOULD BE SHUTDOWN AND THE CAUSE INVESTIGATED. 
    • A. 

      LOW OIL VISCOSITY

    • B. 

      HIGH OIL VISCOSITY

  • 6. 
    With all three hydraulic systems pressurized the Hydraulic P-BIT starts and takes about ___________ to complete.
    • A. 

      One minute

    • B. 

      Two minutes

  • 7. 
    Recommended taxi speed: - Straight / DRY:
    • A. 

      30 kt

    • B. 

      10 kt

    • C. 

      5kt

  • 8. 
    Recommended taxi speed: - Straight / WET or CONTAMINATED:
    • A. 

      30 kt

    • B. 

      10 kt

    • C. 

      5 kt

  • 9. 
    Recommended taxi speed: - Turns / DRY:
    • A. 

      30 kt

    • B. 

      10 kt

    • C. 

      5 kt

  • 10. 
    Recommended taxi speed: - Turns / WET or CONTAMINATED:
    • A. 

      30 kt

    • B. 

      10 kt

    • C. 

      5 kt

  • 11. 
    For economic and environmental reasons, FOD prevention, damage to other airplane and equipment in close proximity of the airplane, etc., it is desirable to limit the thrust to _______ as much as possible and avoid rapid accelerations and decelerations. 
    • A. 

      30% N1

    • B. 

      40% N1

  • 12. 
    For normal operations a setting around _______ will be enough for ground maneuvering.
    • A. 

      30% N1

    • B. 

      40% N1

  • 13. 
    For straight ahead taxiing or for small changes of direction, the use of rudder pedal steering mode may be used. The maximum steering angle of rudder pedal is ...
    • A. 

      +/- 7°.

    • B. 

      +/- 17°.

  • 14. 
    The ________ has the largest arc while turning and determines the minimum obstruction clearance path.
    • A. 

      Wing tip

    • B. 

      Tail tip

  • 15. 
    During ground operations of more than 30 minutes (including taxi in and taxi out) in icing conditions or if increased fan vibration due to fan ice accumulation is present, the engine thrust level must be increased momentarily to a minimum of ______________________________  or until fan vibe level returns to normal.
    • A. 

      54% N1 and held at that thrust level for 30 seconds

    • B. 

      64% N1 and held at that thrust level for 45 seconds

  • 16. 
      The minimum recommended bleed duct pressure prior to start is 40 minus _______ for every 1000 ft above sea level.
    • A. 

      0.5 psi

    • B. 

      1.5 psi

    • C. 

      2.5 psi

  • 17. 
    Engine start using pneumatic cart usually presents ________ ITT values. Consider performing a crossbleed start on the second engine.
    • A. 

      Lower

    • B. 

      Higher

  • 18. 
    Hydraulic System: Warm up must be accomplished before starting the engines in case of reservoir temperatures below ...
    • A. 

      - 8°C.

    • B. 

      -18°C.

    • C. 

      -28°C.

  • 19. 
    In order to improve the chances of a successful engine start, the oil temperature should be raised to at least ...
    • A. 

      -0°C.

    • B. 

      -10°C.

    • C. 

      -20°C.

  • 20. 
     For EMBRAER 190/195 at speeds between _____________, a slight vibration may occur. If this vibration occurs, accelerating or reducing the speed to exit this speed range will improve passenger comfort.
    • A. 

      17 kt and 21 kt

    • B. 

      20 kt and 25 kt

    • C. 

      25 kt and 29 kt

  • 21. 
    For EMBRAER 190/195 during ground operations of more than 30 min (including taxi in and taxi out) in icing conditions or if increased fan vibration due to fan ice accumulation is present, the engine thrust level must be increased momentarily to a minimum of ___ N1 and held at  that thrust level for 30 s or until fan vibe level returns to normal. The engine must be run up momentarily at intervals not to exceed 30 min.
    • A. 

      44%

    • B. 

      54%

    • C. 

      64%

  • 22. 
    When operating with flex takeoff thrust, thrust setting parameters used to establish thrust for takeoff are not considered as operating limits; thrust may be restored to the maximum available level during the takeoff if REF ATTCS was set to ON during takeoff data setting and at least one of the following events occur:
    • A. 

      Difference between both engine N1 values is greater than 15%;

    • B. 

      OEI (One Engine Inoperative);

    • C. 

      Associated Thrust Lever is moved to MAX detent;

    • D. 

      Press TOGA Switch

    • E. 

      Windshear is detected.

  • 23. 
    Make sure that the thrust levers are set to TOGA position before ____, when HOLD mode is activated.
    • A. 

      40 kt

    • B. 

      50 kt

    • C. 

      60 kt

  • 24. 
    During takeoff, the _____ callout has three main proposes: pilot incapacitation check, airspeed crosscheck and the transition from Low to High Energy speed
    • A. 

      60 kt

    • B. 

      80 kt

    • C. 

      100 kt

  • 25. 
    CROSSWIND TAKEOFF   In case of strong crosswind, small lateral control wheel input may be used. Control wheel displacement greater than ___ results in increase in drag due to spoilers deployment.
    • A. 

    • B. 

    • C. 

      12°

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