Envoy EMB Written Test A

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Author:
nn4beatbox
ID:
254649
Filename:
Envoy EMB Written Test A
Updated:
2014-11-19 13:59:19
Tags:
EMB 140 145 Written Test Envoy
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Description:
EMB 145/140 Envoy (American Eagle) Written Test A
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  1. The Engine Air Inlet Anti-Icing System uses:

    High Pressure Bleed Air
    Low Pressure Bleed Air
    Both High and Low Pressure Bleed Air
    None of the above
    High Pressure Bleed Air
  2. EMB 145 Max Structural Takeoff Weight?
    48,501
  3. Emergency ram air is introduced into the aircraft via:
    • A Ram Air Engine Vents
    • B The same inlets used to cool the heat exchangers in the air conditioning system
    • C Electrically operated emergency side
    vents
    • D ECU boost vents
    The same inlets used to cool the heat exchangers in the air conditioning system
  4. Both the Electropneumatic Outflow Valve and the Pneumatic
    Outflow Valve maintain the same position while in the
    automatic mode.

    True
    False
    True
  5. If the cabin altitude exceeds 10,000 ft. he crew will receive a:

    A. Warning on the PFD
    B. Aural warning "Cabin"
    C. Cabin Altitude on the EICAS becomes red at 10,000 ft.
    D. Both B and C
    Both B and C
  6. How does the ATTCS of the EMB-135/140 differ from that of the EMB-145?

    A. The two systems are identical
    B. The EMB 135/140 is ATTCS capable in both T/O and ALT T/O-1 moes
    C. Only the EMB-145 has ATTCS
    D. None of the above
    B.
    (this multiple choice question has been scrambled)
  7. Minimum operational temperature?

    A. -50 SAT
    B. -65 SAT
    C. -45 SAT
    D. -54 SAT
    B
  8. Max landing gear retraction speed?
    200 kts
  9. Vfe flaps 45
    145 KIAS
  10. Min temp for manual anti-ice operation
    -40 SAT
  11. Max altitude for flap extension?
    20,000 ft.
  12. Minimum altitude with autopilot engaged during an ILS approach is?
    200 ft.
  13. Exterior dimensions of EMB-145?
    98ft. x 66ft. x 22ft.
  14. Which method below will achieve TO RSV on the EMB 135/140 powerplant?

    A. Automatically when the ATTCS is triggered while in T/O mode for takeoff?
    B. Manually selected by the pilot anytime by moving the thrust levers beyond the thrust set detent
    C. Selected by the pilot by pressing the Takeoff button on the control pedestal during a maximum thrust takeoff while in the T/O mode up to 1700 ft AFL after takeoff
    D. All of the above
    D. All of the above
  15. APU is available to supply electrical power and / or pneumatic power:
    7 seconds after having reached 95% rotor speed
  16. Pushing the APU STOP button
    Sends a signal to the ESU in order to simulate an overspeed condition and shuts down the APU
  17. Turning the APU master knob to ON:

    A. both A and B
    B. Energizes the ESU/FADEC
    C. Commands the fuel shutoff valve to open
    D. Opens the start fuel solenoid valve
    A. Both A and B
    (this multiple choice question has been scrambled)
  18. The IC-600 1 serves as the primary unit incorporating autopilot functions with the IC-600 2 serving as the secondary unit (backup).

    True
    False
    False
  19. With the autopilot engaged, how can we select the "vertical speed" mode?

    A. By pressing the VS button
    B. By pressing the FLC button when the pre-selected altitude is below the current altitude
    C. Both A and B
    D. By rotating the pitch control wheel when descending in the SPD select mode
    A. By pressing the VS button
    (this multiple choice question has been scrambled)
  20. What is the purpose of of the TBCH?
    It offers an alternate means to select frequencies for COMM2 and NAV 2 in the event that you lose both RMU's
  21. Which of the following is true?

    A. The flight deck observer can make PA announcements from his/her digital audio panel
    B. In the Pilot to Passenger Mode, the flight deck observer has priority of transmission over flight attendant #1
    C. There is a chime tone associated with the Call function from the pilot to the flight attendant
    D. All of the above
    D.
  22. When depressing the BACKUP INPH button on the ICU the following occurs:

    A. A striped bar inside the button itself illuminates
    B. CABIN and CAB EMERG buttons on the ICU illuminate
    C. PILOT and EMERG PILOT buttons on the Attendant's Call Panel illuminate
    D. All of the above
    D. All of the above
  23. Which battery provides power for APU starting?
    Battery #2
  24. How many minutes of power can both batteries provide for essential loads in case of failure of all generators?
    40 minutes
  25. The engine driven generators will normally come on line when the engine speed reaches:

    A. 10.0% N2
    B. 56.4% N2
    C. 95% plus 7 seconds
    D. none of the above
    B. 56.4% N2
    (this multiple choice question has been scrambled)
  26. The FPMU operates under the authority of the:
    FADEC
  27. What is engine oil tank capacity?

    A. 10 quarts
    B. 6 quarts
    C 13 quarts
    D. 13 liters
    C. 13 quarts
  28. The PMA is capable of supplying sufficient power for ignition at engine speeds above:

    A. 10% N1
    B. 10% N2
    C. 5% N2
    D. 14% N2
    B. 10% N2
    (this multiple choice question has been scrambled)
  29. The maximum available thrust for each selected thrust setting is calculated by the:
    FADEC
  30. FADEC A and B may alternate automatically:

    A. The FADEC in control is unable to safely control the engine
    B. At the beginning of each engine ground start
    C. After each engine start
    D. Both A and B
    D. Both A and B
    (this multiple choice question has been scrambled)
  31. In an EMB 135/140 the FADEC will select T/O and in an EMB 145 the FADEC will select T/O-1 mode when the gear is down and locked below:

    A. 15,000 ft.
    B. 14,600 ft.
    C. 10,000 ft.
    D. 12,500 ft.
    A. 15,000 ft.
    (this multiple choice question has been scrambled)
  32. If the thrust lever is inadvertently set below IDLE in flight, the FADEC will command:
    Flight Idle
  33. The Thrust Reversers are actuated:

    A. Electrically
    B. Pneumatically
    C. Mechanically
    D. None of the above
    D. None of the above
  34. A lavatory smoke detector signals smoke activating:

    A. Red alarm on the Smoke Detector Panel
    B. Horn on the Smoke Detector Panel
    C. Warning Message on the EICAS
    D. All of the Above
    D. All of the Above
  35. A Gust Lock system blocks movement of the:
    Elevators
  36. Flaps are operated:
    Electrically
  37. Rudder system #1 is automatically shutoff through the Rudder Electronic Circuit at speeds above:

    A. 200
    B. 180
    C. 150
    D. 135
    D. 135
    (this multiple choice question has been scrambled)
  38. An amber colored ADC 1 and/or ADC 2 appears on the PFD when:

    A. Only one ADC is supplying both sides (captain's and first officer's)
    B. Answer A and B
    C. Automatically appears after a failure of ADC 1 and/or ADC 2
    D. None of the above
    A. Only one ADC is supplying both sides
    (this multiple choice question has been scrambled)
  39. The airspeed trend vector represents the airspeed which the airplane would attain in ____ seconds and is disabled during takeoff.
    10
  40. The reference speed bugs (V1, Vr, V2, Vapp) are displayed in the bottom portion of the airspeed tape below 40 KIAS and they are removed from display at:

    A. V2 + 40 kts
    B. Vap + 42 kts
    C. 240 KIAS
    D. 200 KIAS
    B. Vap + 42 kts
    (this multiple choice question has been scrambled)
  41. Regarding the "low airspeed awareness" scale on the airspeed tape, which of the following is TRUE:

    A. The stick pusher will be activated at the top of the red range
    B. The stick shaker may be activated at the top of the amber range
    C. Both A and B
    D. None of the above
    D. Both A and B
  42. The magenta altitude trend vector will display the altitude which the airplane should attain in ___ seconds if the current vertical speed is maintained.
    6
  43. You will lose both AHRS in an "electrical emergency"

    TRUE/FALSE
    FALSE
  44. The DG Mode of the AHRS will be used when:

    A. Both B and C
    B. Operating in charted areas of unreliable magnetic heading
    C. There is a failure of the Flux valve itself
    D. Tracking true course as opposed to magnetic courses
    A. Both B and C
    (this multiple choice question has been scrambled)
  45. The purpose of the transfer ejector pump is to:
    Help keep the collector box filled
  46. EMB-145 max structural landing weight?
    42,549
  47. By turning the X-Feed selector knob to LOW 2:

    A. The crossfeed valve opens and the right selected electric pump turns off
    B. The crossfeed valve opens and the left selected electric pump turns off
    C. Only the crossfeed valve opens and nothing else
    D. None of the above
    A
  48. There is a fuel low temperature sensor located in each tank

    True/False
    False
  49. With no GPU power or APU power, or any form of generator power, which is true about pressurized refueling?

    A. It can not be accomplished
    B. It can be accomplished, but only by selecting BATTERY on the refueling panel
    C. It can be accomplished because no electric power is needed
    D. None of the above
    B.
    (this multiple choice question has been scrambled)

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