Term
| 1. The maximum load in the AFT baggage compartment is: |
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Definition
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Term
| 2. The maximum tire ground speed is: |
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Definition
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Term
| 4. What is the location of each portable fire extinguisher? |
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Definition
One behind the copilot seat
One behind the aft right seat. |
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Term
| 5. Describe the baggage compartment light operation. |
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Definition
| Momentarily pressing the light switch will cause the lights to illuminate for 5 min. If the compartment door is opened. |
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Term
| 6. What is the maximum flap extended speed (VFE) for flap 1? |
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Definition
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Term
| 7. What is the indication when the pitch angel exceeds 50’ nose up or 30’ nose down? |
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Definition
| Red extreme pitch warning chevrons are displayed in the attitude indicator pointing toward the horizon. |
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Term
| 8. When in TO or G/A mode, what must be true for ALT Pre-Select Mode (ALTS) to arm? |
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Definition
| The preselected altitude must be greater than or equal to 400 ft from the TO or G/A altitude. |
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Term
| 9. Concerning a flight display unit, what is true about reversionary mode? |
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Definition
| This is a mode of operation in which both flight instruments (PFD symbology) and EICAS are displayed simultaneously on one unit. |
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Term
| 10. How does the CDI indicate the navigation source? |
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Definition
| Single, magenta needle for GPS navigation; single, green needle for NAV 1; double, green needle for NAV2 |
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Term
| 11. What provides cockpit lighting during an electrical emergency condition? |
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Definition
| The dome light powered by the Emergency Bus. Flashlights |
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Term
| 11. What provides cockpit lighting during an electrical emergency condition? |
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Definition
| The dome light powered by the Emergency Bus. Flashlights |
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Term
| 12. What malfunction brings on the ELECTRICAL EMERGENCY CAS message? |
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Definition
| A loss of both generators in flight. |
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Term
| 13. What is the minimum GPU voltage for battery charging. |
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Definition
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Term
| 14. What is the maximum generator load? |
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Definition
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Term
| 15. To what bus does GPU supply power? |
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Definition
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Term
| 16. Upon completion of the Engine Fire QRH procedure, what does continued illumination of the red light in the Shutoff pushbutton indicate? |
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Definition
| The overheat/fire on that engine still persists. |
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Term
| 17. Describe the baggage smoke detection system. |
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Definition
| The system consists of one detector with two sensors monitoring the aft baggage compartment. |
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Term
| 18. A successful engine fire test consists of: |
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Definition
The red and white lights illuminated in both shutoff pushbuttons, FIRE message displayed in both ITT gauges, E1 FIRE and E2 FIRE CAS messages.
Aural “FIRE, FIRE”. |
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Term
| 19. Which of the following is true concerning the pitch trim system? |
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Definition
| There are two redundant modes of operation: Normal and Backup |
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Term
| 20. What is the purpose of the spring-loaded rudder boost system? |
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Definition
| It provides force assistance to the rudder control system in case of thrust asymmetry |
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Term
| 21. What is the maximum altitude for flaps extended? |
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Definition
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Term
| 22. After extension in flight, how may the speedbrakes be retarded? |
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Definition
By slowing the aircraft below 125 KIAS or advancing bot thrust levers past MAX CRZ.
By moving the speedbrake switch to the closed position or extending the flaps. |
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Term
| 23. Which statement is true concerning the stall warning protection system? |
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Definition
| The Stick Pusher is hydraulically actuated |
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Term
| 24. Concerning aircraft fueling, which of the following answer is correct? |
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Definition
| The fuel tanks may be fully or partially refueled through the pressure refueling system or by gravity filler caps on the top surface of each wing. |
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Term
| 25. The function of the fuel tank vent system is to: |
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Definition
| Keep the pressure differential between the fuel tanks and the atmosphere within structural limits. |
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Term
| 26. Inter wing balancing of fuel load is achieved by: |
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Definition
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Term
| 27. What is the purpose of the AUTO position of the DC electric fuel boost pump switch? |
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Definition
| The electric fuel pumps are automatically actuated during engine start, crossfeed, and as a backup when primary ejector pumps fail. |
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Term
| 28. What is the purpose of the hydraulic system accumulator? |
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Definition
| To supply additional flow demand during simultaneous brake application and ground spoiler actuation or during pressure transients where the engine-driven pump capacity is exceeded. |
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Term
| 29. What systems use hydraulic power? |
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Definition
| Landing gear, main brakes, spoilers, spring-loaded rudder booster, and stall pusher |
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Term
| 30. The hydraulic system is checked for proper hydraulic fluid quantity by: |
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Definition
| Following the Hydraulic System Check procedure under the Servicing and Maintenance section of the POH |
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Term
| 31. What happens to the hydraulic system if the hydraulic fluid exceeds the operational temperature? |
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Definition
| HYD HI TEMP CAS message will be displaced and both hydraulic shutoff valves will close. |
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Term
| 32. What systems are affected by turning the wing/stab anti-ice on? |
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Definition
| Wing/stab anti-ice system and stall warning protection system |
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Term
| 33. When should the anti-ice systems be turned on? |
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Definition
| All anti-ice systems should be on with the temperature at or below 5 degrees Celsius in visible moisture |
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Term
| 34. If electrical power is no longer available to the engine anti-ice system, it will default to: |
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Definition
| The open position ensuring the EAI system provides continuous bleed or heat to the engine inlet fall safe open. |
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Term
| 35. Which statement correctly describes emergency brake operation? |
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Definition
| The emergency parking brake is mechanically actuated and provides pressure to all brakes, allowing the pilot to modulate brake pressure in emergency situations. |
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Term
| 36. In the event of BRK FAIL CAS message, which of the following statements is correct? |
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Definition
| Brakes will be available, but you will need to use the emergency/parking brake handle to apply them. |
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Term
| 37. What is used to extend the landing gear manually? |
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Definition
| Gravity and aerodynamic forces |
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Term
| 38. How is the crew alerted when the engine fire detector senses a fire/overheat? |
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Definition
| By a FIRE message on the respective ITT gauge, a red light in the engine shutoff pushbutton, an aural “Fire, Fire,” and an ENG 1 / 2 FIRE CAS message |
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Term
| 39. What does TAWS use to provide altitude input? |
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Definition
| Information from the CPS receiver |
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Term
| 40. The oxygen system consists of: |
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Definition
| One oxygen tank for both the passengers and passenger drop-down masks and crew quick dropping masks. |
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Term
| 41. Which statement is true concerning the crew oxygen masks? |
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Definition
| There are three modes of operation Emergency, Normal, and 100%. The mask is usually left in the 100% mode. |
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Term
| 42. Upon Engine failure, what must be done to initiate auto-relight? |
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Definition
| Nothing. Auto relight will begin in any thrust lever position |
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Term
| 43. How are the igniters energized for ground start? |
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Definition
| With the temperature above 0 degrees Celsius the igniters will alternate between A and B for each successive start. If the temperature is 0 degrees Celsius or below, both A and B will be used. |
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Term
| 44. Automatic thrust reserve (ATR) is enabled by: |
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Definition
| Making an ATR ON selection via soft keys on the MFD (G1000) or on GTC (G3000) |
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Term
| 45. What is the power source of the FADEC? |
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Definition
| The permanent magnet alternator (PMA) primarily, and 28VDC from the electrical system for engine start and as a back-up power source. |
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Term
| 46. How can the pressure regulating, and shutoff valves (PRSOVs) be manually controlled? |
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Definition
| Via the BLEED 1 & 2 switches on the pneumatics panel |
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Term
| 47. What happens if the DUMP button is pressed? |
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Definition
| The outflow valve is opened, and the recirculating fans are turned off. |
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Term
| 48. What must be true to power the air conditioning system on the ground? |
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Definition
| The aircraft must be powered by GPU, and one generator must be on |
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Term
| 49. What is the source of cooling air to the heat exchangers? |
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Definition
| Ram air through the ram air valve in flight, air passing through the ground cooling fan on the ground |
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Term
| 50. What is the maximum differential over pressure? |
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Definition
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