Primera

1. (ATA 22) Engaging the AP when bank angle is 5 degrees or less with the F/D off will activated: A. TRK hold will turn to amber colour. B. HDG hold only. C. HDG hold or TRK hold.

2. (ATA 22) If a control wheel actuator fails during autoland, the force limit of the remaining actuator is: A. Half the force limit of a single actuator. B. Two times as high. C. Not affected.

3. (ATA 22) What is the bank angle limit below 200 Ft?. A. 30 degrees. B. 15 degrees. C. 8 degrees.

4. (ATA 22) If a fluorescent light in the Mode Control Panel is degraded: A. A maintenance memo is generated. B. An EICAS Condition message is displayed. C. The MCP microprocessor fails.

5. (ATA 22) Each AFDC computer consists of: A. 3 microprocessors and only 2 of them are used for backdrive commands. B. 2 microprocessors, one for each set of backdrive actuators. C. 3 microprocessors and all the three command the backdrive actuators.

6. (ATA 22) What signals do the A/T arm switches on the MCP supply?. A. Trim Enable logic to the EEC. B. Crab angle protection during Autoland. C. Autothrottle arm to the CPM Comm.

7. (ATA 23) Any ELT of the correct type may be fitted to any aircraft. What makes this possible?. A. Pins must be shorted at the plug connectors to the aircraft wiring. B. The mount/programming module automatically sends user identification data on connection. C. The ELT must be pre-programmed prior to fitting with the code switches on the unit.

8. (ATA 23) The HF couplers receive single phase power trom: A. The Battery buses. B. The Transceivers. C. The AIMS power nodulators.

9. (ATA 23) What is the purpose of the CSS ALL TEST?. A. Collects reat-time failures for 20 seconds and shows them. B. Lets you do special tests for detalled troubleshooting. C. Does a full BITE of the CSS (Cabin Service System).

10. (ATA 23) In what format is the SELCAL code provided?. A. Programming module on the E1-2 rack. B. Coding switche with 16 switches in groups of four. C. Jumpers in the rear of the decoder.

11. (ATA 23) When does the in seat power supply master control unit (MCU) enter the standby mode?. A. On the ground. B. During critical flight phases. C. If the system is overloaded.

12. (ATA 23) What conditiions must be met to allow you to erase the cockpit voice recorder?. A. Aircraft on Ground and Parking brake On. B. Parking brake released and aircraft on Ground. C. Aircraft on Ground and both engines off.

13. (ATA 23) The Ground crew calI horn sounds for 3 sec. What does this signify?. A. The Flight Deck are calling the ground. B. The Equipment cooling system has failed. C. The AC Power is off and the ADIRU'S on.

14. (ATA 23) Panel switches on the P5 & P61 panel directly interface with: A. PDCU units. B. OPBC units. C. OPCF units.

15. (ATA 23) How is the service interphone connected to the flight interphone?. A. Through the RTP's. B. Through the AMU. C. Through the AIM's.

16. (ATA 23) What type of Connection to the PMAT ports has the B-router?. A. ARINC 629 bus. B. ARINC 818 bus. C. 10 Base T interface.

17. (ATA 23) What is the purpose of the Radio Tuning Panel (RTP) crosstalk tuning bus?. A. Allows fault data to be displayed on the panel. B. Allows any RTP to tune any receiver. C. Allows AIMS to control the RTP data.

18. (ATA 23) What type of cameras are fitted to the Flight Deck Entry video surv veillance system?. A. Infrared. B. Ultraviolet. C. High resolution optical.

19. (ATA 23) During a cabin PA test it is found that the normal PA controller is inoperative. To easily restore PA you need to select the alternate PA controller at the: A. CACP. B. ASP. C. CSCP.

20. (ATA 23) In the event of an ACP (audio control panel) or AMU (audio management unit) Station card failure the crew may recover Audio control by: A. Using the Flight deck handset. B. Deselecting the Data Mode on the FDCF. C. Using the Observers audio selector.

21. (ATA 23) The operator can transmit on: A. Only one HF (high frequency) system at a time. B. Both HF systems at one time, at the same frequencies. C. Both HF systems at one time, but at different frequencies.

22. (ATA 23) The passenger address system accepts and sends announcements at these levels of priority: A. Boarding music, Recorded announcements, and Video system audio; Direct access and Cabin interphone; Flight interphone. B. Direct access and Cabin interphone; Flight interphone; Recorded announcements, Video system audio and Boarding music. C. Flight interphone; Direct access and Cabin interphone; Recorded announcements, Video system, audio and Boarding music.

23. (ATA 22) The airplane is in cruise and has no faults. How many backdrive actuators engage when the pilot engages the autopilot?. A. 3. B. 6. C. 2.

24. (ATA 22) How many microprocessors does the MCP have?. A. 1. B. 3. C. 2.

25. (ATA 22) At what radio altitude do the rudder pedal backdrive actuators engage during approach?. A. 1000 feet. B. 400 feet. C. 1500 feet.

26. (ATA 22) The thrust limit mode and thrust limit are displayed on the: A. EICAS. B. ND. C. PFD.

27. (ATA 45) How is data transfered from the AIMs to the MAT (Maintenance Access Terminal)?. A. Over the AVLAN on a fibreoptic bus. B. On an ARINC 629 data bus. C. On an ARINC 429 data bus.

28. (ATA 45) In the engine balancing system of the MAT, how many weight partnumbers and locations can the existing balance weight data list for the fan contain?. A. 30 weight partnumbers and 30 locations. B. 15 weight partnumbers and 15 locations. C. 1 partnumber and 1 location.

29. (ATA 45) What is the function of the AVLAN system?. A. Provides high speed communications between CMCS and aircraft systems. B. Allows external devices such as laptop to communicate with the aircraft systems. C. Provides high speed communications between AIMS and MAT or PMAT.

30. (ATA 45) Which CMC function is normally the Primary?. A. L/H CMCF. B. R/H CMCF. C. Aiternates each Air/Grnd transition.

31. (ATA 45) The engine balancing function of the MAT allows which type of balancing?. A. Fan and high pressure turbine. B. Fan balancing only. C. Fan and low pressure turbine.

32. (ATA 45) When perfoming a MAT test, the test condition shows INHIBITED. How can you find out why the test was inhibited and how to proceed?. A. By selecting the TO TEST Control button. B. By selecting the maintenance message data button. C. By selecting ATA 31 on the FMs CDU.

33. (ATA 45) Where can Onboard engine balancing be carried out?. A. At the AVM unit on the E6 shelf. B. Cannon plug on the AlMS cabinet. C. Using the OEBS through the MAT.

34. (ATA 45) Where can Maintenance Memo's and Scheduled Maintenance Tasks messages be found on the MAT (Maintenance Access Terminal)?. A. Fault History. B. Inbound FDE's. C. Maintenance Planning.

35. What is the purpose of the HF control panel RF sense potentiometer?. A. Controls the sensitivity of the receiver. B. Inhibits the squelch system. C. Control the transceiver outlet to the coupler.

36. What is the VHF system is mainly used for?. A. Long range air to air. B. Short range communications and data transmission line of sight. C. DATA transfer only.

37. What is the basic electrical supply to VHF transceiver range?. A. 28V dc only. B. 115 Vac 400 Hz 3 phase and 28V dc. C. 115 Vac 400 Hz single phase anly.

38 Where is the amplification of interphone signals achieved?. A. The audio selector panel. B. The audio managerment unit (AMU). C. The dedicated Interphone Amplifier Unit.

39. Where is the Reading light control established?. A. ZMU's. B. PA/CI controllers. C. CCCP's.

40. If the Lower Lobe Attendants Rest area is fitted, What connectors must be activated for communication purposes?. A. The ZMU's need configuring to adjust the area control. B. The CMC's LLAR function needs to be activated. C. The OEU data function switch must be selected to the INST position.

41. Which of the following components control passenger information signs?. A. The ZMU's. B. The OEU's. C. The SDƯ's.

42. Where can chimne muting be achieved form?. A. The ZMU mute button. B. The Attenadants panel at L1 door. C. The CMS system.

43. What is the purpose of the ALL TEST?. A. Lets you do special test for detailed troubleshooting. B. Does a full BITE of the CSS. C. Collects real-time failures for 20 seconds and shows them.

44. What is the first test you should run if there is a CSS problem?. A. All test. B. Quick test. C. Engineering test.

45. What functionality do you lose if a cabin interphone controller (CIC) fails?. A. There is no lighting control in the cabin. B. There is no entertainment audio available at the passenger seat. C. There is no cabin interphone capability.

46. How do you connect the cabin interphone system to the service interphone system?. A. Use the Service Interphone switch on the P5 overhead panel. B. Can not connect the cabin interphone system to the service interphone system. C. Use the speed dial function on the centre contral display unit (CDU).

47. What system is used to answer a call to the flight deck from the ground?. A. The flight interphone system. B. The service interphone switch. C. The VHF communication system.

48. Where is the ground crew call horn located?. A. Left main wheel wel. B. Right main wheel well. C. Nose wheel well.

49. How is a reset performed when a SELCAL call is received on the right high frequency (HF)Radio?. A. You push the right HF switch on the radio tuning panel. B. You reselect the HF MIC switch on the radio tuning panel. C. You push the cancel switch on the radio tuning panel.

50. The SELCAL reset signal comes from what LRU?. A. Audio management unit (AMU). B. Passenger address/cabin interphone controller. C. Satelite data unit (SDU).

51. What unit interfaces the SATCOM audio channels to connected to the crew microphone system ?. A. The RFU'S. B. The AMU's. C. The SDU's.

52. The purpose of the passenger telecommunication unit is to?. A. interface the Satellite Data Units (SDU's) to the RFU's. B. Aliow or gain adjustments to the system. C. Configure the leiecommunication system whena seat configuration change is accomplished.

53. Where can the SDU and SATCOM LRU fail annunciation be located?. A. On the front or the RFU. B. On the front face of the SDU. C. Through the CWNC's.

54. An HF antenna coupler fault indicates what condition?. A. Home/Tune sequence faults or arcing in the coupler. B. Overheat condilion in the coupler. C. Open circuit in the control bus.

55. The transceivers receive airlground relay inputs to calculate which of the following?. a. Flight leg faults in the memory. b. Error message inhibit system due to ground interference. C. aircraft ground operations to inhibit certain frequencies that may cause injury to personne.

56. What is the purpose of the Radio tuning Panel (RTP) cross talk busses. a. Allow for error to be calculated. b. Allow for synchronised tuning data so any RTP can control any transceiver. c. Allow for data cross loading after replacement of a transceiver.

57. Where does the left HF Coupler receive its power from. a. A single phase 115V AC from the left HF Trans ceiver. b. Three phase 115VAC from the left HF Transceiver. c. 28VDC power from the right transceiver for interlock.

58. If an ACARS 'REJECTED' messages occurs what does this mean?. A. The message data did NOT download. B. The message data is full and cannot accept any more data. C. The Message downloaded successtully but has not been read by the crew.

59. Which of the following statements is correct? The cockpit voice recorder records: A. 15 hours of voice conversations. B. 60 minutes of voice conversations. C. 2 hours of voice conversations.

60. What are the conditions of the Ground Mode Relay and the Parking Brake Relay to allow you to erase the cockpit voice recorder?. A. Ground Mode Relay-in AlR and Parking Brake Relay Brake ON. B. Ground Mode Relay-In AlR and Parking Brake Relay Brake OFF. C. Ground Mode Relay-In GROUND and Parking Brake Relay Brake ON.

61. When do you need to re-install the configuration database?. A. When you test any CSS component. B. When you replace any CSS component. C. When you replace any CSS component, except peripherals (lights, speakers, cabin attendant handsets (CAHs) etc.).

62. What functionality do you lose if an overhead electronics unit (OEU) fails?. A. There is no passenger address available. B. There is no lighting control in the cabin. C. There is no lighting control for lights connected to the failed OEU.