General fam Airbus

1. How many frames are added to the A321 respect to A320?. 13 Frames. 15 Frames.

2. What metal is the material used to construct the vertical stabilizer of the A320?. Composite. Descomposite.

3. What is the main difference between the A319/320/321 and A318 vertical stabilizer?. The new rib 12N is on the STA 5970. The New rib 15N is on the STA 2020.

4. The sliding windows and the side fixed windows are contained in the ATA reference number?. 56 Windows. 59 Windows.

5. Each outer wing is fitted with?. Five slats made of aluminum alloy and five CFRP spoilers. Seven slats track.

6. What are the two types of construction of airbus A320?. Monolithic or Sandwich construction. Sandwich or apu.

7. Which computer receives the data from the SDACS to generate amber cautions?. Flight Warning Computer. Flight upper computer.

8. On which display does the warning message appear?. Engine/Warning Display. Engine/Wing slats.

9. What do the visual attention getters consist of?. A red MASTER Warning and amber MASTER Caution in front of each pilot. A blue Master warning and Alberto Master caution in front of each pilot.

10. When is the static inverter operating?. When ON Batteries Only. When OF Batteries only.

11. DC BAT BUS can be supplied by the?. DC Bus 1, DC Bus 2 or Batteries. AC Bus 1, AC Bus 2 or Batteries.

12. In case of an emergency operation, how is the electrical network supplied?. The Emergency Generator (EMER GEN) supplies the aircraft with electrical power. The Emergency wing generator.

13. How is controlled the brightness of the reading light?. Each reading light potentiometer controls the brightness of the corresponding supplementary reading light. Supplementary renting light corresponding.

14. The CIDS controls and monitors the cabin light through the panel called?. Flight Attendant Panel (FAP). Flight Attendant Cockpit panel (FACP).

15. The cockpit panels and instrument lighting controls are located on?. On three different panels and underneath the glareshield. Of two different panels and underneath.

16. (A320) How are supplied the engines after the center tank is empty?. Fuel is supplied from the wing inner cell. Fuel pump fairing wing rh.

17. How are divided the wing tanks?. Outer and Inner cell. One and two cell.

18. Which component controls and monitors the APU?. ECB (Electronic Control Box). EWC (Electronic Wing Control).

19. What is the main function of the APU?. To produce independent pneumatic and electrical power. To produce independent eléctricas wing.

20. Is correct the following statement regarding to engines V2500 installed in the family airbus A320?. All the engines are basically the same. A programming plug on the Electronic Engine Control (EEC) changes the available thrust. The Electronic engine control sistem changes.

21. What does the FADEC system consist of?. The EEC and its peripherals, per engine. The EWC and its Apu generator.

22. Where are located the main components of the fuel system in the engine?. On the left side of the engine. On the Right side of the engine.

23. The pneumatic system operates pneumatically and is monitored by: 2 Bleed Monitoring Computers (BMC 1&2). There is one BMC for each engine bleed system. 1 Bleed Monitoring Computers (BMC 1&2).

24. What is the purpose of the fan air valve?. The FAV blows across the pre-cooler to maintain the temperature within limits. The FAP blows actos the pre-cooler.

25. What is the purpose of IP/HP switching?. To keep air bleed at a sufficient pressure at low engine speed. To keep air bleed at a sufficient pressure wing left.

26. Which hydraulic systems are pressurized by an engine driven pump (EDP)?. Green and Yellow. Blue and Green.

27. In normal operation, what is the blue hydraulic system pressurized by?. An electric pump. An apu generator.

28. Where are the EDP 1 and 2 located?. They are located on the accessory gearbox of engine. Fan plate engine 1.

29. Where are displayed the messages related to Pre-FANS status?. Engine & Warning Display. Engine & Apu generator.

30. How is the pilot noticed when new ATC messages are transmitted to the aircraft?. Two attention getter pushbuttons are operative and indicate ATC incoming messages. Five attention getter are operative ATC.

31. Where are passenger oxygen mask stored?. In the Passenger Service Unit (PSU). In the Passenger seat.

32. What is the main purposed of the FLIGHT ATTENDANT PANEL (FAP)?. The FAP is used for control and programming the functions of the CIDS. The FAP is used generator box.

33. What is the function of the door damping and emergency operation cylinder?. To assist normal door operation, but in an emergency acts as an actuator for automatic. To assist normal emergency door.

34. What happens when the arming lever is set to the armed position?. The girt bar stays attached to the cabin floor. The girt bar Stays Doors entry.

35. In the fuel tank, the level of flammability defined in the proposal was established based upon comparison of the safety record of?. Center tank. Wing tank.

36. What is the computer that monitors the FTIS?. IGGS Controller Unit (ICU). Control universal.

37. Where is discharged the OEA in the FTIS?. Overboard. Outboard.

38. Where does the toilet bowl rinsing water come from?. The potable water system. The system water shroud.

39. The toilet system is monitored by: The Vacuum System Controller Function (The VSCF Bite). The hydraulic system (HS).

40. Which surfaces are used to control the roll?. Ailerons and Spoilers 2 to 5 numbered from the wing root to wing tip. Ailerons and spoilers 1 to 3 numbered from the wing root to wing tip.

41. What protections are active in direct law?. All protections are lost in direct law. Protections are los in the law.

42. The two side sticks are used for?. Manual pitch and roll control. Hydraulic pitch and control.

43. What is the purpose of the packs?. The packs are responsible for basic temperature regulation. The packs are inresponsible for basic.

44. What is purpose of the bypass valve?. To modulate the pack discharge temperature. Pack discharge temperature modulate.

45. What happens in case of any duct overheat?. The trim air PRV and the trim air valves will automatically close to isolate the system. The vertical Trim sidewall.

46. What happens in case of loss of the electrical power supply to the engine anti-ice valve?. The valve opens when the engine is running. The valvule closets when the engine.

47. Bleed air from the engines or the APU is supplied to?. Each wing through a pressure regulating and shut off valve called wing anti-ice (WAI) valve. Wing anti-ice and anti-ice precooler.

48. When are the passenger oxygen mask automatically released?. When the cabin reaches 14,000 feet. When the cabin reaches 21,000 feet.

49. When does the chemical oxygen generation start?. By pulling the mask the oxygen generator is activated and produces pure oxygen to the mask for a limit time. The bottle oxygen mask limit time.

50. How can be opened the doors in case of the failure of the container door opening?. Manually with a special tool located in the cabin crew workstation. Overboard.

51. What is the purposes of the RMPS?. To give capability of tuning all communication radios. The valve opens when the engine is running.

52. What is the purpose of the CVR?. The cockpit voice recorder records the last 2 hours of flight crew conversations and communications an aural warning. The Vacuum System Controller Function (The VSCF Bite).

53. What is the system that allows the flight crew members to communicate among themselves and with a ground mechanic?. Flight Interphone. Engine & Warning Display.

54. What are the basic functions of the FACS?. Flight Augmentation and Fault. To modulate the pack discharge temperature.

55. Where are the FMGC functions controlled from?. The FCU and MCDU. The ACW and MCDI.

56. How can be the autopilot disengaged in the cockpit using the side sticks?. When the red TAKEOVER & PRIORITY pushbutton an any side stick is pressed. The cockpit voice recorder records the last 2 hours of flight crew conversations and communications an aural warning.

57. Which hydraulic system powers normal landing gear operation?. Green System. Yellow System.

58. Which hydraulic system powers the nose wheel steering?. Yellow System. Red System.

59. How can the parking brake be hydraulically powered?. Either by yellow high pressure or by the brake accumulator. The girt bar stays attached to the cabin floor.

60. Where is the ENGINE fire detectors located?. On the pylon, the fan and the core. When ON Batteries Only.

61. What does the test pushbutton check?. The TEST buttons are used to test the respective fire detection and extinguishing system operation. All protections are lost in direct law.

62. How is an APU fire on ground normally extinguished?. Automatically. Outer and Inner cell.