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1. The elevator is _______ operated
a. mechanically
b. hydraulically |
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________ hydraulic systems are installed on the aircraft.
a. two
b. three |
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3. The steering handle alone can rotate the nosewheel up to ______ degrees.
a. 71
b. 76 |
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4. What is the overall length of the ERJ-145?
a. 20.87m (79’)
b. 29.87m (98’) |
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5. The electrical system is primarily a _______ system.
a. AC
b. DC |
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| 6. What situation will cause the NO SMIKING and FASTEN SEAT BELT signs in the cabin to automatically illuminate? |
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| Deployment of cabin oxygen masks |
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| 7. Can the F/A bypass the cockpit EMER LTS switch and select the emergency lights on? |
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| 8. The PSU TEST causes the Reading Lights and the ______ light at each PSU to come on. |
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| 9. Where is the Landing Gear “Freefall Lever” located? |
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| b. Under a cover door in the cockpit floor on the F/O side |
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| 10. Where are the Display Control Panels (DCPs) located? |
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| 12. Where is the adjustment control for the Rudder Pedals? |
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| It is below the instruments on each pilots' panel |
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| 13. What area is just aft of the Overhead Panel? |
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| 14. How many Environmental Control Units are installed? |
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| 15. The temperature control knob is in the AUTO position when it is ______. |
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| 16. To allow the attendant to control the passenger temperature, the passenger temperature knob should be ________. |
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| 17. To control the passenger temperature manually, the passenger temperature knob should be ________. |
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| 18. What is the purpose of the Dual Temperature Control Valve? |
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| It is positioned to determine how much air is allowed to bypass the cooling process of hte ACM |
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| 19. Through which of the Heat Exchangers does the bleed air flow through first? |
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| 20. The air that flows out of the ACM turbine is _______. |
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| 21. The Recirculation Fan operates to recirculate air ___________. |
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| 22. The conditioned air to the cockpit is mainly provided by the _____ pack. |
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| 23. The conditioned air to the cabin is provided mainly by the ________ pack. |
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| 24. What provides the air conditioning to the individual air outlets? |
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| 25. Which system provides increased airflow through the air conditioning lines by recirculating the cabin air? |
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| 26. Cabin altitude, differential pressure and cabin altitude rate of change indications are displayed on the __________. |
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| 27. What is the cabin altitude limitation while in AUTO? |
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| 28. Which Outflow Valve(s) are controlled when the system is operating in the AUTO mode? |
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| Both valves; the MANUAL (pneumatic) valve is slaved to the AUTO (electro-pneumatic) valve |
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| 29. Which Outflow Valve(s) are controlled when the system is operating in the MANUAL mode? |
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| MANUAL (pneumatic) valve only |
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| 30. Which IC-600 provides the signals for Autopilot operations? |
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| 31. What happens if the TCS button is pressed during autopilot operations? |
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| Autopilot operations are temporarily inhibited |
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| 32. Where is the AP engage annunciator? |
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| 33. How does the pilot know to which Flight Director the AP is coupled? |
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| 34. What are the basic engagement modes of the Autoflight/Flight Director system? |
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| 35. Which of these two modes provides airspeed protection? |
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| 36. What happens if the Heading knob is pressed? |
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| Heading bug is synchronized to the current heading |
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| 37. When a mode is armed, the mode displays on the FMA in _____ color. |
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| 38. How many Transmit buttons can be selected ON at the same time? |
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| 39. Pressing a Microphone Selector button enables transmission AND reception of radio signals through the respective COM unit. |
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| True. The transmit and reception modes are selected by a microphone button |
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| 40. When the DAP is in the Emergency mode, the Captain is connected to COM1 and to NAV ____ |
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| 41. Where does the pilot tune the desired VHF Comm frequency? |
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| 42. What is the purpose of the HOT position of the communication switch on the pilot control wheel? |
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| to allow the crew memebers to communicate without selecting a mic |
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| 43. Does the RMU have a memory feature for storage of communication frequencies? |
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| 44. The DFDR records the aircraft system and flight parameters for the last _____ hours |
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| 45. The DFDR is powered when the _____ switch is turned ON or the aircraft is in flight |
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| 46. The Cockpit Voice Recorder is powered by Essential DC Bus ___. |
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| 47. The CVR can be erased when the aircraft is on the ground and ____________. |
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| 48. The CVR is equipped with an Underwater Locator Beacon |
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| 49. In order to make a passenger address, the _________ button on the DAP needs to be pressed |
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| 50. What is the difference between pressing CABIN versus CABIN EMER on the ICU? |
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| Nothing; just a different light that illuminates the F/A phone |
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| 51. Where does the pilot enter the assigned Transponder code? |
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| 52. What is the Transponder mode you will use for normal operations? |
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| 53. The left network of the electrical system includes generators _______ |
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| 54. Normally the APU generator is connected in parallel with the generators that supply DC BUS ____. |
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| 55. When operating normally, the APU generator will automatically replace any failed generator |
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| 56. The APU Starter Generator connects or disconnects (released) the APU starter generator when the APU RPM is above |
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| 57. The SHED BUSES OVRD Knob will only function on the ground with at least _______ operating. |
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| 58. On the MFD, a DC bus will indicate green when the bus is energized and _____ when the bus is off. |
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| 59. If DC BUS ____ is lost, the inverter will become inoperative |
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| 60. The AC Power button should remain pressed in at all times |
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| 61. When the AC Button is pressed in, a striped bar will illuminate to indicate it is turned on |
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| 62. Generator current and voltage may be displayed on the ______. |
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| 63. If a generator fails, a reset of the generator may be attempted twice with a 30 second cooling off period |
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| 64. How many engine-driven generators are installed? |
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| 65. What type of power is made by the generators? |
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| 66. The APU Generator is able to provide electrical power when the APU RPM is above _____. |
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| 67. The SHED BUSES OVRD mode will only function________. It requires at least one generator operating. |
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| 68. After APU start, if the APU generator load (amps) exceeds ____ amps, the procedure will direct you to turn off the #1 Battery knob until the load is below 400 amps or 3 minutes have elapsed. |
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| 69. If the Ground Power is selected ON, the aircraft batteries _____ being changed |
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| 70. Which power source has the highest priority? |
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| 71. The normal in flight position of the SHED BUSES Selector Knob is _____. |
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| 72. When on the ground, with at least one generator running, the SHED BUSES may be powered by using the _______ in the OVRD position. |
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| 73. Above ___ RPM, the APU starter generator is available to supply electrical power to the system |
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| 74. During normal operation, the APU generator should be selected off |
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| 75. APU generator voltage and amperage may be monitored on the ____ Electrical page |
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| 76. The Ground Service Bus is energized when the ground power unit is plugged in and the GPU AVAIL button has been pressed] |
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| 77. Ground power will take priority over ______. |
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| 78. External power voltage will be displayed on the ____ |
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| 79. If External power is connected, but the GPU button is not selected ON, the Ground Service bus is____________ |
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| 80. The lavatory is equipped with a smoke detection system only. |
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| 81. How many extinguishing bottles are available to fight an engine fire? |
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| 81. How many extinguishing bottles are available to fight an engine fire? |
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| 82. The pilots will be provided with an EICAS indication in case the lavatory extinguisher has been activated |
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| 83. In case of lavatory smoke detection, a warning message will be displayed on the EICAS |
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| 84. Where is the lavatory smoke detector panel located? |
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| 85. During the Fire System Test, does the APU FIRE message appear on the EICAS? |
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| 86. During the Fire System Test, the light in the Baggage Fire Extinguishing button illuminates |
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| 87. Where is the button that is used to discharge the cargo compartment fire extinguishers? |
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| 88. Which fire bottle instantly fills the baggage compartment with extinguishing agent? |
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| 89. If the fire system test button is pressed for more than ___ seconds while on the ground, the APU will shut down |
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| 90. If the fire test needs to be repeated, wait __ seconds before repeating the test |
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| 91. How many bottle(s) of fire extinguishing agent is available for the APU? |
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| 92. How many bottle(s) of fire extinguishing agent is available for the Engines? |
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| 93. If an APU fire is detected on the ground, the APU will automatically shut down |
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| 94. What indication will be presented to the pilot in case of a loss of pressure in a fire sensor tube? |
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