avalitos

1. (ATA 34) Where does AIMS receive its time from?. A. ELMS. B. MMR's.

2. (ATA 34) Which two Standby Instruments are interchangeable?. A. Standby Altimeter & Standby Airspeed Indicator. B. Standby Attitude Indicator & Standby Altimeter.

3. (ATA 34) What makes the bottom TCAS antenna Omni directional?. A. The system is always onni directional. C The PSEU supplies a gear not up signal.

4. (ATA 34) What happens when the Air Data Inertial Reference Unit (ADIRU) Is initially turned on from the flight deck switch?. A. A self test is carried out for 30 sec only. B. The heading flag is removed before the self test is initiated.

5. (ATA 34) How does the Automatic Direction Finder receiver get tuning data?. A. Using the VOR/ADF switches on the EFIS control panel. B. Manually from the Control Display Unit.

6. (ATA 34) Where does AIMS receive its time from?. A. Captains Clock. B. ELMS. C. MMR's.

7. (ATA 34) What happens if one gyro and two accelerometers fail in the ADIRU?. A. Heading output is lost from the ADIRU. C. A status message is displayed.

8. (ATA 34) How do you display ILS data on the ND?. A. Turn the mode selector to VOR. B. Turn the mode selector to APP.

9. (ATA 34) What test would you do to check for defects in a CDU display?. A. The CDU configuration test. C. The CDU special functions test.

10. (ATA 34) Where is the Terrain Awareness display for EGPWS shown?. A. On the PFD only. C. On the ND only.

11. (ATA 34) The piot-static system get static air pressure from. A. Flush static port on the fuselage. C. Static port on pitot probe.

12. (ATA 34) On the B777 aircraft the FMCF in the right AIMS cabinet is in the: A. CPM (COMM). B. CPM (BASIC).

13. (ATA 34) When either DME interrogator transmits, it sends out a suppression pulse to: A. The ATC transponder & TCAS computer. B. The MMR & TCAS Computer.

14. (ATA 34) What will be shown on PFD if RA NCD occurs: A. Yellow RA flag. C. RA display goes out of view.

15. (ATA 34) During an ADF test from the MAT, the pointer goes to: A. 135. C. 180.

16. (ATA 34) Howlong the SAARU can supply backup navigation function if ADIRU failed?. A. 10 minutes. C. 3 minutes.

17. (ATA 34) What source of Radio Altimeter data has the highest priority to be used for the Captain's PFD if the left RA unit fails?. A. Centre Radio Altimeter transceiver. B. Captain's Radio Altimeter Data will be lost.

18. (ATA 34) If both FMCF's fail, how is the ALTN navigation data to the ND's supplied?. A. The onside CDU supplies the data to the ND's. B. Only the centre CDU supplies data to the left ND.

19. (ATA 34) Airspeed and atitude indicated on standby instruments are catcutated by. A SAARU. B. SADMs. C ADIRU.

20. (ATA 34) What air pressure(s) used by ADIRU and SAARU to catculate airspeed. A. Pitot air pressure. B. Both pitot and static air pressures.

21. (ATA 34) How does the Standby Air Data Modules transmit data. A. ARINC 629 bus. B. ARINC 517 bus. C. ARINC 429 bus.

22. (ATA 34) What is indicated on standby airspeed indicator when aircraft on ground and not moving: A. 30 knots. B. 50 knots.

23. (ATA 34) What tunes the VOR receivers automatically?. A. CDUs. C. AIMS cabinet.

24. (ATA 34) The pitot static system gets static air pressure from?. A. Flush static port on the fuselage. B. Static port on engine cowls.

25. (ATA 34) Airspeed and altitude indicated on standby instruments are calculated by?. A. SAARU. B. SADMs.

26. (ATA 34) Which changes occurs on the standby attitude indicator, when “B/CRS” (backcourse) is selected?. A. The localizer deviation bar goes out of view and the glideslope deviation bar reverses polarity. B. The localizer deviation bar reverses polarity and the glideslope deviation bar goes out of view.

27. (ATA 34) If the alternate V/MMO switch is in the “ALTN” position them the: A. The Air Data & Inertial Reference Units (ADIRU) adjust the Vmo/Mmo curve to compensate for a flight with the landing gear down. B. The Air Data & Inertial Reference Units (ADIRU) use the alternate static ports as input in order calculate the Vmo/Mmo curve, for normal flight.

28. (ATA 34) The TCAS/ATC control panel controls. A. TCAS computer directly and ATC transponders through the TC AS computer. C. ATC transponders and TCAS computer directly.

29. (ATA 34) Where can the ILS be displayed?. A. On the RMI. B. On both NDs and Primary Flight Display (PFD.

30. (ATA 34) The ATC antennas are interchangeable with which other antennas was?. A. The DME antennas. B. The ADF antennas.

31. (ATA 34) What color are the ADF parters on the ND?. A. White. C. Cyan.

32. (ATA 34) Where are the ILS antennas?. A. Radome, vertical stabilizer tip, AFT NLG. B. Radome only.

33. (ATA 34) What source of radio altimeter data has the highest priority to be used for the Captain´s PFD, if the left RA unit fails?. A. Center radio Altimeter Transceiver. C. Captain´s radio altimeter data will be lost.

34. (ATA 34) How do you clear a message from the CDU scratchpad?. A. Push the backspace LSK CDU on the CDU. B. Push clear (CLR) key on the CDU.

35. (ATA 34) If the ADIRUS fails where is the information received from?. 35. (ATA 34) If the ADIRUS fails where is the information received from?. B. Automatically select the FPA backup mode.

36. (ATA 34) What is the minimum speed to engage the autopilot?. A. 70 Knots. B. 80 Knots.

37. (ATA 34) How many antennas and transceivers has RA system?. A. 6 antennas and 3 transceivers. B. 4 antennas and 2 transceivers.

38. (ATA 34) Where is the CDU test done?. A. Maintenance page in MAT. B. Left CDU.

39. (ATA 34) The weather radar receiver transmitter gets pitch and roll data from which of the following?. A. The ADIRU. C. The AIMS cabinets.

40. (ATA 34) How do the ACT transponders get altitude data?. A. Directly from the CADS systems. B. From the Air Data Inertial Reference Unit (ADIRU.

41. (ATA 34) How does the ground proximity terrain awareness function determine if a there is a terrain conflict?. A. Latitude and longitude only. B. Airplane latitude, longitude, heading and barometric altitude.

42. (ATA 34) How in the VOR autotuning mode?. A. Through ELMS. C. Through AIMS.

43. (ATA 34) What is the maximum the free of the TILT on the WXR antenna?. A. +/- 37 dregree. C. +/- 15 degree.

44. (ATA 34) What is the purpose of the ATC program switching module?. A. To allow for bite checking of the ACT system. B. To set off the unique 24- fit identification code the airplane.

45. (ATA 34) What are mode of weather radar (XWR)?. A. Centered VOR mode, altitude approach mode. C. Expanded approach mode, expander VOR mode, centered MAP mode and expanded MAP mode.

46. (ATA 34) What happens if a single channel fails on a MD&T card?. A. A maintenance message is generated. B. All flight deck annunciators fail.

47. (ATA 34) How is due auto tunning archived?. A. NAV receiver interfacing. B. AIMS interfacing.

48. (ATA 34) The FMC calculate airplane position using three different sources of data -U+ what are the three different sources?. A. GPS position last calculated position and initial reference position. B. Inertial position from the LADIQU, NAV radio position GPS position.

49. (ATA 34) Which GPS data is displayed on the ND?. A. Latitud indication and GPWS system message. C. Terrain awareness display.GPWS system message and GPWS alert message.

50. (ATA 34) What does the weather radar receiver-transmitter receiver pitch why B and roll data. A. To quable auto ignition during flare. C. To stabilizer the antenna in flight.

51. (ATA 34) The page shows the acting NAV DATA BASE?. A. The post INIT page. B. The IDENT page.

52. (ATA 34) Which GPWS mode alerts the pilot that the airplane is in windshear?. A. Mode 3. B. Mode 7.

1. (ATA 44) When is the cellular model (CM) started?. A. After take-off. B. Upon aircraft weight-on-wheels.

2. (ATA 44) From where can maintenance staff access the eXTV system?. A. Maintenance access terminal (MAT). C. Crew Terminal.

3. (ATA 44) Where is accessed to do ESC test?. A. Through the Crew Terminal Left Menu. C. Through the Crew Terminal Main Menu.

1. (ATA 46) Where can you find a list of all LSAP (Loadable Software Aircraft Parts) stored in the EFB Maintenance Page?. A. INTERNAL CONFIG. C. SYSTEM CONFIG.

2. (ATA 46) What is the main hardware component of the onboard network Systemn (ONS). A. Network file server (NFS). B. Local area network (LAN).

3. (ATA 46) During Initial power up it is observed that the EFB DU is flashing and showing the Self test page intermittently for about a minute. What actions would you take?. A. Reload the Operational Software into the L EFB EU. C. This is normal and may be cancelled by pressing the MENU Bezel key.

4. (ATA 46) The EFB EU's have two CPU cores, hosting what software?. A Android & Windows. C. Linux & Windows.

5. (ATA 46) Which page is displayed on the DU after power-up test is completed?. A. SYSTEM CONFIG. B. MAIN MENU.

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