TEST AVIONICS
Name: TEST
K: A Code:
34 - NAVIGATION
34-00-00 RADIO NAVIGATION CONTROL
PRESENTATION
1. Can VOR 2 frequency be changed through RMP 1?
A - Yes.
B - No.
2. In back-up mode, an ILS can be tuned through:
A - RMP 1 or 2.
B - RMP 1 only.
C - The onside RMP only.
34 - NAVIGATION
34-00-00 DDRMI PRESENTATION
3. From which ADIRU can the DDRMI receive information ?
A - ADIRU 1 or 2.
B - ADIRU 2 or 3.
C - ADIRU 1 or 3.
34 - NAVIGATION
34-10-00 ADIRS PRESENTATION
4. Which ADIRU does not supply DMC 1?
A - ADIRU 1.
B - ADIRU 2.
C - ADIRU 3.
34 - NAVIGATION
34-13-00 AIR DATA PROBES PRESENTATION
5. How do pitot and static probes supply the ADIRUs?
A - Using ADMs which convert pressure into digital format.
B - Directly with total and static pressures.
C - Directly with digital format.
6. Where does ADIRU3 receive TAT information from?
A - Captain TAT sensor.
B - First-Officer TAT sensor.
C - Standby TAT sensor.
7. Which pressure line(s) need(s) to be drained?
A - All pitot lines.
B - All static lines.
C - Only the standby static line.
MST-AE014-4S
34 - NAVIGATION
Rev. 1A (Jan. 20/2005) 1 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
34-10-00 ADIRS CDU PRESENTATION
8. The inertial data, TK/GS, PPOS, WIND, HDG are available on:
A - ATT only.
B - NAV only.
C - ATT or NAV.
9. When does the ALIGN light flash?
A - Within five minutes of NAV mode selection, when present position has not been entered.
B - During the alignment phase in case of IRS alignment error.
C - When alignment has been completed.
34 - NAVIGATION
34-10-00 ADIRUS INTERCONNECTION
10. What must be done in case of ADR1 failure?
A - Set AIR DATA switch to CAPT3 position.
B - Set ATT HDG switch to CAPT3 position.
C - Leave AIR DATA and ATT HDG switches on NORM position.
11. What must be done in case of IR3 failure?
A - Set AIR DATA switch to F/O3 position.
B - Set ATT HDG switch to F/O3 position.
C - Leave ATT HDG switch in NORM position.
12. When AUTO discrete is grounded, where does the IR receive air data from?
A - Input bus A.
B - Input bus B.
C - Internal bus, then from bus A, then from bus B depending on bus validity.
34 - NAVIGATION
34-10-00 ADIRS INDICATIONS ON PFD
13. What is displayed if the inertial vertical speed is not available?
A - A red V/S flag comes on.
B - A degraded V/S data provided by ADR.
C - Nothing.
14. What information is displayed on the airspeed scale?
A - CAS from ADR.
B - CAS from ADR mixed with inertial speed.
C - CAS from ADR, inertial speed if ADR failure.
15. What happens if an altitude failure occurs?
A - The altitude scale goes out of view.
B - A red ALT flag is displayed.
C - A and B.
MST-AE014-4S
34 - NAVIGATION
34-10-00 ADIRS INDICATIONS ON ND
Rev. 1A (Jan. 20/2005) 2 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
16. A heading discrepancy between the NDs is detected by?
A - FWCs.
B - DMCs.
C - ADIRS.
17. How is the drift angle indicated?
A - By a diamond shaped symbol rotating on the heading dial.
B - By the difference between heading reference and actual track symbol.
C - A or B, according to information validity.
34 - NAVIGATION
34-10-00 ADIRS INDICATIONS ON ECAM
DISPLAY UNIT
18. The TAT and SAT data is provided by?
A - ADR1 or ADR3.
B - ADR2 or ADR3.
C - ADR1 or ADR2.
34 - NAVIGATION
34-36-00 MMR SYSTEM PRESENTATION
19. The satellite orbital planes have an inclination of:
A - 60.
B - 55 to the Equator.
C - 45 to the Equator.
20. The control segment is composed of:
A - 3 monitor stations.
B - 5 monitor stations.
C - 4 monitor stations and one master control station.
34 - NAVIGATION
34-36-00 MMR DESCRIPTION/OPERATION
21. Which ILS receiver provides the Ground Proximity Warning Computer with data?
A - ILS 2 receiver.
B - ILS 1 receiver.
C - ILS 1 and ILS 2 receivers.
22. Where is ILS 2 data displayed?
A - On Capt ND and F/O PFD.
B - On Capt PFD and F/O ND.
C - On F/O PFD and F/O ND.
23. The primary source of ADIRU3 is:
A - GPS2.
MST-AE014-4S
B - GPS1.
C - GPS1 and 2.
24. The IR portion of the ADIRU provides the FMGC with:
A - IR data, pure GPS data and hybrid GPIR data.
B - VOR/DME data.
Rev. 1A (Jan. 20/2005) 3 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
C - only GPS data.
34 - NAVIGATION
34-36-00 MMR INDICATIONS ON PFD
25. When do the G/S and LOC scales appear on the PFD?
A - When the ILS pushbutton is selected.
B - When G/S and LOC beams are received.
C - A and B.
26. When does the lateral deviation scale flash?
A - When the LOCALIZER receiver is faulty.
B - When the deviation is excessive.
C - When the aircraft is out of range.
27. When does the red ILS flag appear?
A - When both LOC and G/S signals have failed.
B - When ILS frequency is not available.
C - When the ILS is not selected on the FCU.
34 - NAVIGATION
34-36-00 MMR INDICATIONS ON ND
28. What is displayed in ROSE-NAV mode when the ILS pushbutton is selected on the EFIS control panel?
A - An ILS course pointer.
B - A lateral deviation bar.
C - A and B.
29. How is the excessive deviation displayed on vertical scale?
A - The Glide/Slope index disappears.
B - A red "G/S" symbol appears in the middle of the scale.
C - The Glide/Slope index and the scale flash permanently.
34 - NAVIGATION
34-41-00 WR/PWS SYSTEM PRESENTATION
30. Windshear indications are shown:
A - Only on the NDs.
B - On the PFDs and the NDs.
C - On the Upper ECAM DU.
MST-AE014-4S
34 - NAVIGATION
34-41-00 WR/PWS DESCRIPTION/OPERATION
31. Which component controls antenna stabilization?
Rev. 1A (Jan. 20/2005) 4 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
A - ADIRU.
B - Transceiver.
C - Antenna.
32. Which data is used for antenna stabilization?
A - Pitch and roll.
B - Selected tilt angle, antenna azimuth angle and elevation angle.
C - A and B.
33. When is the Windshear function automatically activated?
A - Below 2300ft and one of the two qualifier inputs, of both qualifiers A and B, is valid.
B - Always when a windshear event is encountered.
C - When the AUTO/ON/STBY selector on the ATC/TCAS Control Unit is in STBY position.
34. The Predictive Windshear discrete output is used to:
A - Inhibit the windshear function.
B - Inhibit aural alerts generated by TCAS or GPWS or other FWC warnings.
C - Transmit the aural alert to the Audio Mixing Box.
34 - NAVIGATION
34-41-00 WR/PWS CONTROLS AND DISPLAYS
35. In which mode is the manual gain adjustment recommended?
A - In any mode.
B - In MAP mode.
C - In WX/TURB mode.
36. Can a radar image be displayed in PLAN mode?
A - Yes.
B - No.
37. Does an amber warning mean the loss of radar image?
A - Yes.
B - No.
38. When the radar system switch is in OFF position?
A - The predictive windshear function is not activated.
B - The predictive windshear function is active until the WINDSHEAR/AUTO/OFF is in the AUTO
position.
B - The predictive windshear function is always available.
MST-AE014-4S
34 - NAVIGATION
34-42-00 RADIO ALTIMETER
DESCRIPTION/OPERATION
Rev. 1A (Jan. 20/2005) 5 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
39. In normal operation, how is the height data provided ?
A - By system 1 to Capt PFD and F/O PFD
B - By system 2 to CAPT PFD and F/O PFD
C - By system 1 to CAPT PFD and by system 2 to F/O PFD
40. What happens if Radio Altimeter 1 fails ?
A - RA 2 provides data to the EGPWC.
B - FMGC 1 provides data to the EGPWC.
C - The EGPWC no longer receives Radio Altitude.
34 - NAVIGATION
34-42-00 RA INDICATIONS ON PFD AND
AUTOMATIC CALL OUT
41. With DH of 100ft entered on the MCDU, when will the radio altitude indication become amber?
A - At 100 ft.
B - At 200 ft.
C - At 400 ft.
42. When does the red RA flag appear on the PFD?
A - When one RA fails.
B - When both RAs fail and the slats are extended.
C - When both RAs fail below 2500ft.
34 - NAVIGATION
34-43-00 TCAS PRESENTATION
43. Which aircraft are detected by the TCAS ?
A - All.
B - Only ATC Mode S equipped A/C.
C - ATC equipped A/C.
34 - NAVIGATION
34-43-00 TCAS DESCRIPTION/OPERATION
44. The TCAS/ATC control panel controls:
A - ATC transponders and TCAS computer directly.
B - ATC transponders directly and TCAS computer through the ATC transponders.
C - TCAS computer directly and ATC transponders through the TCAS computer.
45. The TCAS receives heading, pitch and roll data from:
A - ADIRU 1.
B - ADIRU 1 or 3 according to AIR DATA switch status.
C - Selected ATC transponder.
MST-AE014-4S
34 - NAVIGATION
34-43-00 TCAS CONTROL PANEL D/O
46. With mode selector in TA position:
A - Only traffic advisories are provided.
Rev. 1A (Jan. 20/2005) 6 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
B - All traffic indications are provided.
C - No TCAS information is provided.
34 - NAVIGATION
34-43-00 TCAS INDICATIONS ON PFD AND
AURAL ALERTS
47. The PFD presents TCAS indications:
A - On the V/S scale in case of TA and RA detection.
B - On the SPEED scale as Preventive Advisoriy.
C - On the V/S scale only in case of RA detection.
48. The colour of the V/S indications change to:
A - red when in presence of a corrective RA detection
B - green when a in presence of corrective RA detection
C - red or green when in presence of a corrective RA detection depending on the sector band in
which they are.
34 - NAVIGATION
34-43-00 TCAS INDICATIONS ON ND
49. A RA is represented on the ND with:
A - a red square
B - A red circle
C - a white filled diamond shape.
34 - NAVIGATION
34-48-00 EGPWS DESCRIPTION/OPERATION
50. What happens to the EGPWS when the stall warning is triggered?
A - All modes are inhibited.
B - Mode 4 is inhibited.
C - Mode 5 is inhibited.
51. What happens when the G/S p/b is pressed in on the GPWS control panel?
A - The Glide/Slope mode is inhibited.
B - Only Glide/Slope mode is valid.
C - The self test sequence is initiated.
52. What happens when the TERR ON ND p/b is pressed in?
A - The ND displays the terrain image.
B - The terrain image is superposed with the radar image on the ND.
C - The radar image is present until a terrain caution or warning is detected.
53. The EGPWS has priority over:
MST-AE014-4S
A - All systems.
B - Auto call out, low speed warning and TCAS.
C - Stall and windshear.
34 - NAVIGATION
Rev. 1A (Jan. 20/2005) 7 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
34-48-00 EGPWS MODES
54. If the voice message "TERRAIN, TERRAIN" is heard, in which mode and configuration are you?
A - In mode 2A, with flaps down or in the glide slope beam.
B - In mode 2B, with flaps down or in the glide slope beam.
C - In mode 2A, with flaps not down and not in the glide slope beam.
55. Which synthetic voice is broadcast in case of anexcessive rate of descent?
A - SINK RATE.
B - TERRAIN TERRAIN.
C - GLIDE SLOPE.
34 - NAVIGATION
34-48-00 EGPWS INDICATIONS ON ND
56. A yellow high density indication means that:
A - An unknown terrain is being overflown.
B - Terrain is between 1000 ft and 2000 ft above A/C altitude.
C - There is no close terrain.
57. When a Terrain Warning Alert is triggered:
A - The red GPWS warning comes on with "TERRAIN ALERT" alert caution.
B - "TERRAIN ALERT, PULL UP" alert warning is heard continuously associated with a red GPWS warning
and the red "TERR AHEAD" message on ND.
C - the amber G/S warning comes on with a cyan "TERR" message on ND.
34 - NAVIGATION
34-51-00 DME DESCRIPTION/OPERATION
58. What is the suppressor coaxial between DME and ATC used for ?
A - To inhibit DME operation.
B - To prevent simultaneous transmission and to interrupt reception of the other systems.
C - To prevent simultaneous transmission and to inhibit the transmission of the other systems.
59. Where is the DME 1 information displayed ?
A - On CAPT PFD and F/O PFD.
B - On CAPT PFD, CAPT and F/O ND and DDRMI.
++.
34 - NAVIGATION
34-51-00 DME INDICATIONS ON PFD AND ND
MST-AE014-4S
60. What does it mean when dashes are displayed instead of DME1 distance indication on the ND ?
A - DME1 interrogator has failed.
B - DME1 interrogator is not receiving the ground station signal.
C - There is no DME station collocated to the VOR station selected.
Rev. 1A (Jan. 20/2005) 8 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
61. When the VOR-D pushbutton is pressed in, on the EFIS control panel,the ND shows:
A - The DME and the VOR/DME ground stations included in the data base.
B - Only the VOR/DME ground stations.
C - The DME and the VOR/DME ground stations included in the flight plan.
34 - NAVIGATION
34-52-00 ATC DESCRIPTION/OPERATION
62. The ATC transponders and DME transponders are:
A - Connected by ARINC buses to exchange distance data.
B - Connected by a suppressor coaxial which transmits an analog signal preventing simultaneous
transmission.
C - Not connected.
63. If ADIRU 2 fails, is the ATC 2 transponder still able to operate in altitude reporting mode?
A - Yes, because altitude data is automatically received from ADIRU 3.
B - Yes, because altitude data will be recovered after manual switching of the AIR DATA selection to
ADIRU 3.
C - No, ATC 2 will be definitively lost.
34 - NAVIGATION
34-53-00 ADF DESCRIPTION/OPERATION
64. How are the antenna amplifiers supplied ?
A - By the 28 DC NORM BUS.
B - By the 115 VAC NORM BUS.
C - By + or - 12 VDC through the ADF Receiver.
65. If FMGC 1 has failed, is the ADF 1 receiver tuned ?
A - Yes, from the opposite FMGC.
B - Yes, through RMP1.
C - No, ADF 1 cannot be tuned.
34 - NAVIGATION
34-53-00 ADF INDICATIONS ON ND
66. What is displayed in case of Non Computed Data?
A - A RED flag.
B - Dashes in place of identification.
C - The ground station characteristics and pointer disappear.
67. What is displayed in case of ADF failure?
A - The pointer symbol and the ADF flag appear in RED.
B - The ground station characteristics and pointer disappear and the RED ADF flag appears.
MST-AE014-4S
C - No ADF indications on ND.
34 - NAVIGATION
34-55-00 VOR/MKR DESCRIPTION/OPERATION
Rev. 1A (Jan. 20/2005) 9 of 2
By:Eduardo. Flores
TEST AVIONICS
Name: TEST
K: A Code:
68. To which of the following is the MKR Antenna connected ?
A - VOR/MKR receiver 2.
B - VOR/MKR receiver 1.
C - VOR/MKR receivers 1 and 2.
69. If FMGC 2 has failed, is VOR 2 receiver tuned ?
A - Yes, from the opposite FMGC.
B - Yes, from the opposite FMGC but after switching.
C - No, the VOR 2 cannot be tuned.
34 - NAVIGATION
34-55-00 VOR INDICATIONS ON ND
70. In which ND mode is the VOR course deviation information displayed ?
A - In ROSE-VOR mode.
B - In ROSE-NAV mode.
C - In any mode.
71. When is the "M" symbol displayed in the VOR characteristics ?
A - When the VOR is tuned from the MCDU.
B - When the VOR is tuned from the RMP.
C - When a failure occurs.
MST-AE014-4S
Rev. 1A (Jan. 20/2005) 10 of 2
By:Eduardo. Flores
