FMGS NAVIGATION

Question 1

1. WHAT DOES IT MEAN WHEN THE ADR FAULT LIGHT ILLUMINATES STEADY ON THE ADIRS CDU?

A. A FAULT IS DETECTED IN AIR DATA REFERENCE
B. NO PRESENT POSITION ENTRY AFTER 10 MN
C. ALIGNMENT HAS BEEN COMPLETED

Answer 1

A. A FAULT IS DETECTED IN AIR DATA REFERENCE

Question 2

2. ON THE PEDESTAL MOUNTED SWITCHING PANEL THE ATT HDG AND AIR DATA SELECTORS ARE AT NORM, MEANING:

A. ADIRU 1 SUPPLIES DATA TO PFD1, ND1 ADIRU 2 SUPPLIES DATA TO PFD2, ND2
B. ADIRU 1 SUPPLIES DATA TO PFD1, ND1 AND RMI VOR/DME ADIRU 2 SUPPLIES DATA TO PFD2, ND2
C. ADIRU 1 SUPPLIES DATA TO PFD1 ADIRU 2 SUPPLIES DATA TO PFD2

Answer 2

B. ADIRU 1 SUPPLIES DATA TO PFD1, ND1 AND RMI VOR/DME ADIRU 2 SUPPLIES DATA TO PFD2, ND2

Question 3

3. TUNING OF VOR/DME AND ILS IS PROVIDED BY:

A. AUTOMATIC TUNING MANUAL TUNING BACK UP TUNING
B. AUTOMATIC TUNING MANUAL TUNING
C. AUTOMATIC TUNING BACK UP TUNING

Answer 3

A. AUTOMATIC TUNING MANUAL TUNING BACK UP TUNING

Question 4

4. IN CASE OF FAILURE OF FMGC1 AND 2:

A. VOR, ILS AND ADF RECEIVERS 1 AND 2 CAN BE TUNED THROUGH RMP1
B. VOR, ILS AND ADF RECEIVERS 1 CAN BE TUNED THROUGH RMP1
C. RMP1 CONTROLS VOR, ILS DME AND ADF RECEIVERS 1 RMP2 CONTROLS VOR, ILS DME AND ADF RECEIVERS 2

Answer 4

C. RMP1 CONTROLS VOR, ILS DME AND ADF RECEIVERS 1 RMP2 CONTROLS VOR, ILS DME AND ADF RECEIVERS 2

Question 5

5. THE ALIGN LIGHT FLASHES:

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

Answer 5

B. DURING THE ALIGNMENT PHASE IN CASE OF IRS ALIGNMENT ERROR

Question 6

6. THE FMCS CONSISTS OF THE FOLLOWING MAIN COMPONENTS:

A. 2 FMGC - 2 MCDU - 2 FAC - 2 FCU CONTROL PANELS
B. 2 FMGC - 2 MCDU - 2 FAC - 1 FCU CONTROL PANEL
C. 2 FMGC - 2 MCDU - 2 FAC - 2 ECAM
D. 2 FMGC - 2 MCDU - 2 ECAM - 1 FCU CONTROL PANEL

Answer 6

B. 2 FMGC - 2 MCDU - 2 FAC - 1 FCU CONTROL PANEL

Question 7

7. NORMAL ELECTRICAL POWER SUPPLIES THE A/C AND THE MCDU CRT IS DARK, WITHOUT ANY OTHER WARNING. IT MEANS:

A. THE FMGC IS OFF
B. THE FMGC HAS FAILED
C. THE MCDU CB IS PULLED
D. THE MCDU “BRT” KNOB IS DIMMED

Answer 7

D. THE MCDU “BRT” KNOB IS DIMMED

Question 8

8. ON THE GROUND, WHEN ELECTRICAL POWER IS INITIALLY SUPPLIED TO THE A/C, THE MCDU WILL AUTOMATICALLY DISPLAY:

A. AIRPORT PAGE
B. INIT A PAGE
C. DATA INDEX PAGE
D. A/C STATUS PAGE

Answer 8

D. A/C STATUS PAGE

Question 9

9. YOU PRESS “ALIGN IRS” PROMPT ON INIT A PAGE. ON THE ADIRS CDU THE ALIGN LIGHTS FLASH BUT NO MESSAGE IS DISPLAYED ON THE CDU:

A. THE SYSTEM CAN ONLY BE USED IN ATT MODE
B. THE SYSTEM IS UNABLE TO ENTER NAV MODE TO COMPUTE COORDINATES: SWITCH IT OFF
C. MAKE A SECOND “PRESENT POSITION” ENTRY

Answer 9

C. MAKE A SECOND “PRESENT POSITION” ENTRY

Question 10

10. THESE MESSAGES APPEAR ON COPILOT SIDE ND “SELECT OFF SIDE RANGE/MODE” & “MAP NOT AVAILABLE”:

A. THE IRS’S HAVE NOT REACHED COMPLETE ALIGNMENT
B. THE F-PLN ENTERED IN CAPTAIN’S FMGC HAS NOT BEEN TRANSFERRED INTO COPILOT’S FMGC
C. SINGLE FMGC OPERATION AND THE TWO EFIS CONTROL PANELS ARE NOT SET AT THE SAME RANGE & MODE

Answer 10

C. SINGLE FMGC OPERATION AND THE TWO EFIS CONTROL PANELS ARE NOT SET AT THE SAME RANGE & MODE

Question 10

17. IN FLIGHT, FOLLOWING A MANUAL POSITION UP-DATING OF THE FMGC

A. IT IS ALSO NECESSARY TO UP-DATE THE IRS POSITION
B. AN IRS CANNOT BE UP-DATED DURING A/C MOTION

Answer 10

B. AN IRS CANNOT BE UP-DATED DURING A/C MOTION

Question 10

11. ENGINES RUNNING, READY TO TAXI, A MESSAGE APPEARS “CHECK GW”. ACCESS TO INIT B PAGE IS NO LONGER AVAILABLE. ON WHICH PAGE IS IT POSSIBLE TO INSERT THE CORRECT GW?

A. T/O PERFORMANCE PAGE
B. PROGRESS PAGE
C. FUEL PREDICTION PAGE

Answer 10

C. FUEL PREDICTION PAGE

Question 11

18. THE EXPEDITE MODE IS ACTIVE. TO DISENGAGE IT, ONE OF THESE STATEMENTS IS NOT CORRECT?

A. PULL THE V/S-FPA KNOB
B. PULL THE SPD KNOB
C. PULL THE ALT KNOB
D. PRESS AGAIN THE EXPED PB TO CANCEL THIS MODE

Answer 11

D. PRESS AGAIN THE EXPED PB TO CANCEL THIS MODE

Question 11

15. A HOLD HAS BEEN ENTERED IN THE F-PLN, SPEED AND NAV ARE MANAGED. YOU WANT TO LEAVE THIS HOLD:

A. USE THE CLR KEY
B. HOLD IS AUTOMATICALLY CANCELLED WHEN OVERFLYING THE FIX
C. ACTIVATE IMM “EXIT*” PROMPT

Answer 11

C. ACTIVATE IMM “EXIT*” PROMPT

Question 11

16. FOR A/C POSITION DETERMINATION, FMGC USES DATA FROM:

A. DME, VOR OR ILS SYSTEMS
B. CLOCKS + GROUND SPEED COMPUTATION
C. 3 ADIRS
D. A & C

Answer 11

D. A & C

Question 11

14. CONTROL OF THE A/C CAN BE AUTOMATIC OR MANUAL. GUIDANCE OF THE A/C CAN BE MANAGED OR SELECTED. HOW DO YOU UNDERSTAND THIS SITUATION MANAGED GUIDANCE - MANUAL CONTROL - SELECTED SPEED?

A. FMGC COMPUTES AND SENDS STEERING ORDERS FOR NAVIGATION PURPOSE. THE PILOT FLIES THROUGH THE SIDE STICK. SPEED IS ADJUSTED IN THE FCU WINDOW.
B. THE AUTOPILOT FOLLOWS THE F-PLN. THE PILOT SETS THE NECESSARY DATA FOR LONGITUDINAL AND LATERAL CONTROL OF THE A/C. THE TARGET SPEED IS COMPUTED AND DISPLAYED BY THE FMGC.

Answer 11

A. FMGC COMPUTES AND SENDS STEERING ORDERS FOR NAVIGATION PURPOSE. THE PILOT FLIES THROUGH THE SIDE STICK. SPEED IS ADJUSTED IN THE FCU WINDOW.

Question 11

12. AIRCRAFT ON RWY CENTERLINE, READY FOR TAKE-OFF. TO PRESET A HDG OF 233°:

A. PULL HDG KNOB TO DISARM NAV MODE SET 233° AND PRESS HDG KNOB TO ENGAGE
B. TURN HDG KNOB, SET 233° AND PULL TO ENGAGE
C. TURN HDG KNOB. SET 233° PULL HDG KNOB WHEN ATC CLEARS TO TURN TO 233°

Answer 11

C. TURN HDG KNOB. SET 233° PULL HDG KNOB WHEN ATC CLEARS TO TURN TO 233°

Question 12

13. ONE OF THE SRS DISENGAGEMENT CONDITIONS IS NOT TRUE.

A. DISENGAGES AUTOMATICALLY AT FCU ALT
B. DISENGAGES AUTOMATICALLY AT ACCELERATION ALTITUDE
C. DISENGAGES MANUALLY BY PULLING THE SPEED KNOB
D. DISENGAGED BY SETTING A NEW FCU ALTITUDE

Answer 12

D. DISENGAGED BY SETTING A NEW FCU ALTITUDE

Question 13

20. THE ENGAGEMENT OF BOTH AUTOPILOTS IS POSSIBLE:

A. WHEN “LAND” ILLUMINATES GREEN ON FMA
B. WHEN A/C IS STABILIZED AT G/S INTERCEPTION ALTITUDE
C. AS SOON AS THE LOC HAS BEEN INTERCEPTED
D. AFTER APPR PB SWITCH IS PRESSED AND ILLUMINATES

Answer 13

D. AFTER APPR PB SWITCH IS PRESSED AND ILLUMINATES

Question 13

19. WHAT ARE THE BASIC MODES OF THE AP/FD?

A. PITCH AND ROLL
B. V/S AND HDG
C. ALT AND NAV
D. SPD AND HDG

Answer 13

B. V/S AND HDG

Question 14

21. CAN YOU READ THE HDG ON THE PFD?

A. YES
B. NO

Answer 14

A. YES

Question 15

22. A/C IS IN CLEAN CONFIGURATION AND NORMAL LAW. WHEN THE FAC DETECTS A TOO HIGH ANGLE OF ATTACK:

A. STALL WARNING IS ACTIVATED
B. THR LK FLASHES ON FMA
C. ALPHA FLOOR FUNCTION OPERATES

Answer 15

C. ALPHA FLOOR FUNCTION OPERATES

Question 16

23. DURING ILS APPROACH, LAND 3 FAIL-PASSIVE (ALSO CALLED CAT 3 SINGLE) ONE ENGINE: FAILS BELOW 100. FEET RA THIS CAUSES A LANDING CAPABILITY- DOWNGRADING AND YOU MUST GO
    AROUND.

A. TRUE
B. FALSE

Answer 16

B. FALSE

Question 17

24. DURING AN ILS APPROACH THE NAV MODE WILL BE DEACTIVATED AT:

A. GLIDE SLOPE CAPTURE
B. LOCALIZER CAPTURE
C. A & B

Answer 17

B. LOCALIZER CAPTURE

Question 18

25. CAN YOU DISPLAY FD BARS AND FPV AT THE SAME TIME, FOR CROSSCHECKING ON DIFFERENT PFD'S? A. YES B. NO

Answer 18

B. NO

Question 19

26. CERTIFIED FMGS LIMITATIONS. MAX WIND CONDITIONS FOR CAT III AUTOMATIC APPROACH, PERFORMED IN MANAGED SPEED GUIDANCE AND WITH A/THR: HEADWIND /TAILWIND/ CROSSWIND A. 30 KT/ 10 KT/ 20 KT B. 40 KT/ 10 KT/ 15 KT C. 20 KT/ 10 KT/ 20 KT

Answer 19

A. 30 KT/ 10 KT/ 20 KT

Question 20

27. THE CONTINUOUS CAVALRY CHARGE AUDIO IDENTIFIES ONLY ONE OF THE FOLLOWING SITUATIONS: A. OVER SPEED FOR THE ACTUAL A/C CONFIGURATION B. FIRE OR OIL LOW PRESS ON ONE ENGINE C. AUTOPILOT DISENGAGEMENT D. EXCESS CABIN ALTITUDE E. AUTO LAND WARNING, REQUIRING A GO AROUND

Answer 20

C. AUTOPILOT DISENGAGEMENT

Question 21

28. SETTING THE THRUST LEVERS AT IDLE WILL DISENGAGE THE A/THR MODE. A/THR WILL REENGAGE: A. AS SOON AS THE THRUST LEVERS POSITION IS CHANGED B. WHEN A/THR PUSH BUTTON IS PRESSED C. PROVIDED THE LEVERS-ARE -SET IN CLB GATE D. PROVIDED THE LEVERS ARE MOVED FROM IDLE POSITION AND A/THR PUSH BUTTON IS PRESSED

Answer 21

B. WHEN A/THR PUSH BUTTON IS PRESSED

Question 22

29. IN ONE OF THE CASES LISTED BELOW, A/THR DOES NOT DISENGAGE: A. WHEN THE TWO THRUST LEVERS ARE SET AT IDLE POSITION B. PRESSING THE A/THR PUSH BUTTON ON THE FCU C. WHEN THE AURAL WARNING ANNOUNCES "RETARD!" D. PRESSING THE INSTINCTIVE DISCONNECT BUTTON

Answer 22

C. WHEN THE AURAL WARNING ANNOUNCES "RETARD!"

Question 23

30. THE LOC PB, ON THE FCU, IS PRESSED TO ARM LOC MODE. THIS MODE IS USED FOR: A. PERFORMING A PUBLISHED LOCALIZER APPROACH B. TRACKING A VOR BEAM DURING AN APPROACH C. PERFORMING THOSE NON-PRECISION APPROACHES VOR-ADF-R NAV D. APPROACHING ON AN ILS WITH NO G/S E. A & D

Answer 23

E. A & D

Question 24

31. WHAT DOES A TRIPLE CLICK MEAN DURING AN ILS APPROACH? A. A LEVEL 3 WARNING TO THE CREW B. A PRIMARY FAILURE IS OCCURRING, PREPARE FOR GO AROUND C. FLAPS ARE SET AT 3 AND THE LANDING GEAR IS NOT DOWN D. LANDING CAPABILITY DOWNGRADING WARNING

Answer 24

D. LANDING CAPABILITY DOWNGRADING WARNING

Question 25

32. THE ACTIVE F-PLN IS ERASED WHEN: A. THE PILOT CALLS THE A/C STATUS PAGE B. THE WHEELS TOUCH THE RUNWAY AT LANDING C. THE A/C HAS BEEN ON GROUND FOR 30 SECONDS FOLLOWING THE LANDING D. ONE ENGINE IS SHUT DOWN AT PARKING PLACE

Answer 25

C. THE A/C HAS BEEN ON GROUND FOR 30 SECONDS FOLLOWING THE LANDING

Question 26

33. FOLLOWING A DUAL ENGINE GENERATOR FAILURE, EMERGENCY GEN SUPPLIES THE A/C: A. FMGC1 IS AVAILABLE (NAV FUNCTION ONLY) INSTEAD OF FMGC1 ONLY IS AVAILABLE B. FMGC 2 ONLY IS AVAILABLE C. BOTH FMGCS ARE AVAILABLE D. NO FMGC IS AVAILABLE

Answer 26

A. FMGC1 IS AVAILABLE (NAV FUNCTION ONLY) INSTEAD OF FMGC1 ONLY IS AVAILABLE

Question 27

34. IN WHICH CASE ARE AP/FD, ATS AND LANDING CAPACITIES TOTALLY LOST? A. 2 IRS'S FAILURE OR 2 ADR'S FAILURE B. 2 RA'S FAILURE C. 2 ILS'S FAILURE D. BOTH FAC’S FAILURE

Answer 27

A. 2 IRS'S FAILURE OR 2 ADR'S FAILURE

Question 28

35. THE MANDATORY PARAMETER USED BY THE ALPHA FLOOR DETECTION IS: A. A/C MINIMUM SPEED B. A/C WEIGHT C. A/C MAXIMUM SPEED D. A/C ANGLE OF ATTACK

Answer 28

D. A/C ANGLE OF ATTACK

Question 29

36. RUDDER TRAVEL LIMITATION IS A FUNCTION OF: A. FAC ONLY B. FAC IN NORMAL AND ELAC IN ALTERNATE C. ELAC ONLY

Answer 29

A. FAC ONLY

Question 30

37. WHEN THE TWO YAW DAMPER FUNCTIONS ARE ENGAGED: A. YAW DAMPER 1 HAS PRIORITY, YAW DAMPER ACTUATOR 2 IS SLAVED B. YAW DAMPER 2 HAS PRIORITY, YAW DAMPER ACTUATOR 1 IS SLAVED C. YAW DAMPER 1 AND 2 ARE ACTIVE, THE TWO ACTUATORS PRESSURIZED D. A HYDRAULIC DEVICE GIVES PRIORITY TO YAW DAMPER 1

Answer 30

A. YAW DAMPER 1 HAS PRIORITY, YAW DAMPER ACTUATOR 2 IS SLAVED

Question 31

38. THE SAFETY TESTS ARE AUTOMATICALLY PERFORMED: A. ON GROUND, AT COMPUTER POWER UP B. IN CASE OF DISCREPANCY BETWEEN 2 COMPUTERS C. IN FLIGHT WHEN A FAILURE OCCURS D. IN FLIGHT AT AUTOPILOT ENGAGEMENT

Answer 31

A. ON GROUND, AT COMPUTER POWER UP

Question 32

39. WHEN THE TWO RUDDER TRIM FUNCTIONS ARE ENGAGED: A. RUDDER TRIMS 1 AND 2 CONTROL THEIR MOTORS TOGETHER B. RUDDER TRIM 1 CONTROLS THE SINGLE TRIM MOTOR C. RUDDER TRIM 1 CONTROLS IT’S MOTOR, RUDDER TRIM 2 IS IN STANDBY D. A MECHANICAL DEVICE GIVES PRIORITY TO RUDDER TRIM 1

Answer 32

C. RUDDER TRIM 1 CONTROLS IT’S MOTOR, RUDDER TRIM 2 IS IN STANDBY

Question 33

40. THE FMGC FUNCTIONS ARE: A. FLIGHT GUIDANCE AND FLIGHT ENVELOPE PROTECTION B. FLIGHT MANAGEMENT AND FLIGHT ENVELOPE PROTECTION C. FLIGHT MANAGEMENT AND FLIGHT GUIDANCE D. FLIGHT ENVELOPE PROTECTION AND YAW AXIS CONTROL

Answer 33

C. FLIGHT MANAGEMENT AND FLIGHT GUIDANCE

Question 34

41. THE TRIM FUNCTION OF THE FAC IS: A. A PITCH TRIM B. A RUDDER TRIM C. AN AILERON TRIM D. A PITCH TRIM AND A RUDDER TRIM

Answer 34

B. A RUDDER TRIM

Question 35

42. IN FLIGHT, IN CASE OF TEMPORARY LOSS OF ELECTRICAL POWER ON FAC2, FAC 2 P/B "FAULT" COMES ON AND, A. IT WILL BE AUTOMATICALLY RESET B. IT CAN BE MANUALLY RESET AND THE SAFETY TESTS ARE PERFORMED C. IT CAN BE MANUALLY RESET BY MEANS OF A PUSHBUTTON ON THE FLIGHT CONTROL OVERHEAD PANEL D. THERE IS NO WAY TO REENGAGE FAC 2

Answer 35

C. IT CAN BE MANUALLY RESET BY MEANS OF A PUSHBUTTON ON THE FLIGHT CONTROL OVERHEAD PANEL

Question 36

43. THE AFS COMPUTERS ARE: A. FMGC AND ELAC B. FMGC AND SEC C. FMGC AND FAC D. ELAC AND SEC

Answer 36

C. FMGC AND FAC

Question 37

44. WITH AP1 AND AP2 NOT ENGAGED, FD1 AND FD2 ENGAGED AND A/THR ACTIVE: A. FMGC1 CONTROLS ENGINE 1, FMGC2 CONTROLS ENGINE 2 B. FMGC1 CONTROLS BOTH ENGINES C. FMGC2 CONTROLS BOTH ENGINES D. FLIGHT CONTROLS AND ENGINES ARE CONTROLLED BY ONLY ONE FMGC

Answer 37

B. FMGC1 CONTROLS BOTH ENGINES

Question 38

45. THE AUTOPILOT DOES NOT DISENGAGE IN CASE OF OVERRIDE ON: A. THE SIDESTICK IN ROLL B. THE SIDESTICK IN PITCH C. THE RUDDER PEDALS D. THE THREE AXES

Answer 38

C. THE RUDDER PEDALS

Question 39

46. IN NORMAL OPERATION, WITH THE TWO MCDU SHOWING THE SAME PAGE, A MODIFICATION MADE BY THE PILOT ON MCDU1 IS SENT TO MCDU2: A. DIRECTLY B. VIA FMGC1 C. VIA FMGC1 AND FMGC2 D. VIA FMGC1, FMGC2 AND RMP2

Answer 39

C. VIA FMGC1 AND FMGC2

Question 40

47. THE FLIGHT GUIDANCE FUNCTIONS ARE: A. AUTOPILOT, FLIGHT PLAN, AUTOTHRUST B. AUTOPILOT, PERFORMANCE, FLIGHT PLAN C. AUTOPILOT, FLIGHT DIRECTOR, AUTOTHRUST, D. FLIGHT MANAGEMENT, AUTOPILOT, AUTOTHRUST

Answer 40

C. AUTOPILOT, FLIGHT DIRECTOR, AUTOTHRUST,

Question 41

48. THE POSITION OF THE AIRCRAFT, USED IN THE FLIGHT PLAN IS COMPUTED: A. FG PART OF THE FMGC B. FM PART OF THE FMGC C. THE DMC D. THE MCDU

Answer 41

B. FM PART OF THE FMGC

Question 42

49. THE FLIGHT DIRECTOR IS ENGAGED: A. BY PRESSING THE FD P/B ON THE FCU B. AUTOMATICALLY AT SYSTEM POWER UP C. BY SELECTING A MODE ON THE FCU D. BY SELECTING THE INIT PAGE ON THE MCDU

Answer 42

B. AUTOMATICALLY AT SYSTEM POWER UP

Question 43

50. WITH AUTOPILOT ENGAGED, THE RUDDER IS NORMALLY CONTROLLED BY: A. THE FMGC B. THE FAC C. THE ELAC D. THE SEC

Answer 43

B. THE FAC

Question 44

51. THE NORMAL FMGC OPERATION IS: A. ONLY ONE FMGC CAN OPERATE AT A TIME B. FMGC 1 HAS PRIORITY, FMGC 2 IS IN STANDBY C. FMGC'S OPERATE ACCORDING TO MASTER/SLAVE PRINCIPLE D. FMGC'S OPERATE INDEPENDENTLY

Answer 44

C. FMGC'S OPERATE ACCORDING TO MASTER/SLAVE PRINCIPLE

Question 45

52. THE FCU ALLOWS: A. MODIFICATION OF THE FLIGHT PLAN OF FM PART B. SELECTION OF FG FUNCTIONS MODES C. SELECTION OF RADIO-NAV FREQUENCIES D. IRS ALIGNMENT

Answer 45

B. SELECTION OF FG FUNCTIONS MODES

Question 46

53. IN CRUISE, LATERAL AP ORDERS ARE EXECUTED BY: A. AILERONS AND SPOILERS B. AILERONS AND RUDDER C. RUDDER AND SPOILERS D. AILERONS, SPOILERS AND RUDDER

Answer 46

D. AILERONS, SPOILERS AND RUDDER

Question 47

54. WITH THE AIRCRAFT IN FLIGHT, AP ENGAGED AND A/THR ACTIVE, THE A/THR MODE: A. CAN BE CHOSEN BY THE PILOT ON THE FCU B. CAN BE CHOSEN BY THE PILOT ON THE MCDU C. DEPENDS ON THE AP LATERAL MODE D. DEPENDS ON THE AP LONGITUDINAL MODE

Answer 47

D. DEPENDS ON THE AP LONGITUDINAL MODE

Question 48

55. WITH THE AIRCRAFT IN FLIGHT, A/THR NOT ENGAGED, THRUST LEVERS ON CLB GATE, AN ALPHAFLOOR IS DETECTED: A. A/THR DOES NOT GET ENGAGED BECAUSE THE ENGINES ARE ALREADY IN CLB THRUST B. A/THR AUTOMATICALLY ENGAGES, BUT IS NOT ACTIVE C. A/THR AUTOMATICALLY ENGAGES AND CONTROLS THE ENGINES WITH CLB THRUST D. A/THR AUTOMATICALLY ENGAGES AND CONTROLS THE ENGINE WITH TOGA THRUST

Answer 48

D. A/THR AUTOMATICALLY ENGAGES AND CONTROLS THE ENGINE WITH TOGA THRUST

Question 49

56. THE FAC COMPUTES RUDDER TRAVEL LIMIT: A. ONLY WHEN AP IS ENGAGED B. ONLY AT LOW SPEED C. ONLY IN CASE OF ELAC FAILURE D. AT ANY TIME

Answer 49

D. AT ANY TIME

Question 50

57. WITH AP ENGAGED IN LAND MODE, THE YAW DAMPER ACTUATOR IS CONTROLLED BY: A. A YAW ORDER COMPUTED BY THE FAC B. A DUTCH ROLL DAMPING ORDER COMPUTED BY THE FAC C. A TURN COORDINATION ORDER COMPUTED BY THE FAC D. AN AP YAW ORDER COMPUTED BY THE FMGC, VIA THE FAC

Answer 50

D. AN AP YAW ORDER COMPUTED BY THE FMGC, VIA THE FAC

Question 51

58. ON THE FMA, ON THE SECOND LINE OF THE LONGITUDINAL ZONE: A. ALT CAN BE ONLY IN GREEN OR MAGENTA B. ALT IN CYAN INDICATES THAT ALT MODE IS ACTIVE C. ALT IN CYAN INDICATES THAT ALT MODE IS ARMED D. ALT IN CYAN INDICATES THAT ALT MODE IS ACTIVE OR AN FM ALTITUDE CONSTRAINT

Answer 51

C. ALT IN CYAN INDICATES THAT ALT MODE IS ARMED

Question 52

59. WITH THE THRUST LEVERS IN THE CLB GATE, A/THR DISENGAGES; THE ENGINES THRUST: A. EQUALS CLB THRUST LIMIT B. IS FROZEN AT THE EXISTING THRUST C. CORRESPONDS TO THE THRUST LEVERS POSITION D. PROGRESSIVELY BECOMES EQUAL TO THE THRUST LEVERS POSITION

Answer 52

B. IS FROZEN AT THE EXISTING THRUST

Question 53

60. WHEN TAKE-OFF MODE IS ENGAGED: A. A/THR AUTOMATICALLY ENGAGES AND IS ACTIVE B. A/THR AUTOMATICALLY ENGAGES BUT IS NOT ACTIVE C. A/THR DOES NOT AUTOMATICALLY ENGAGE AND THE ENGINES ARE CONTROLLED BY THE THRUST LEVERS D. A/THR DOES NOT AUTOMATICALLY ENGAGE AND THE ENGINES ARE CONTROLLED BY THE LAST THRUST TARGET

Answer 53

B. A/THR AUTOMATICALLY ENGAGES BUT IS NOT ACTIVE

Question 54

61. ADIRU 3 CAN SUPPLY INFORMATION TO: A. DMC 1 AND DMC 2 ONLY B. DMC 1 AND DMC 2 ONLY C. DMC 2 AND DMC 3 ONLY D. DMC 1, DMC 2 AND DMC 3

Answer 54

D. DMC 1, DMC 2 AND DMC 3

Question 55

62. AIR DATA MODULES (ADM) SUPPLY PRESSURE INFORMATION TO THE ADIRU'S FROM: A. ALL PITOT PROBES AND STATIC PORTS B. THE PITOT PROBES ONLY C. THE STATIC PORTS ONLY D. THE CAPTAIN AND FIRST OFFICER PITOT PROBES AND STATIC PORTS ONLY

Answer 55

A. ALL PITOT PROBES AND STATIC PORTS

Question 56

63. ADIRS 3 RECEIVES TAT INFORMATION FROM: A. THE CAPTAIN'S TAT SENSOR B. THE FIRST OFFICER'S TAT SENSOR C. THE CAPTAIN AND FIRST OFFICER'S TAT SENSORS D. THE STAND-BY TAT SENSOR

Answer 56

A. THE CAPTAIN'S TAT SENSOR

Question 57

64. THE BARO CORRECTION OR REFERENCE SELECTED IS SENT TO EACH ADIRU VIA: A. THE MASTER FMGC B. THE FCU C. THE RMPS D. THE DMCS

Answer 57

B. THE FCU

Question 58

65. EACH ADIRU RECEIVES TWO ANALOGUE INPUTS. THEY ARE: A. ANGLE OF ATTACK (AOA) AND TOTAL AIR TEMPERATURE (TAT) B. ANGLE OF ATTACK (AOA) AND BARD CORRECTION OR REFERENCE C. TOTAL AIR TEMPERATURE (TAT) AND BARO CORRECTION OR REFERENCE D. FMGC STATUS AND BARO CORRECTION OR REFERENCE

Answer 58

A. ANGLE OF ATTACK (AOA) AND TOTAL AIR TEMPERATURE (TAT)

Question 59

66. IN NORMAL OPERATION THE ADIRU'S ALIGNED USING INFORMATION FROM: A. THE ADIRS CDU B. THE CFDS C. THE FCU D. THE MCDU

Answer 59

D. THE MCDU

Question 60

67. IF ADIRU 2 FAILS, THE CORRECT ACTION IS: A. SET ATT HDG AND AIR DATA SELECTORS TO CAPT-3 B. SET ATT HDG AND AIR DATA SELECTORS TO F/O-3 C. SET ATT HDG SELECTORS TO CAPT-3, AIR DATA SELECTOR TO F/O3 D. SET ATT HDG SELECTORS TO F/O-3, AIR DATA SELECTOR TO CAPT3

Answer 60

B. SET ATT HDG AND AIR DATA SELECTORS TO F/O-3

Question 61

68. IN NORMAL OPERATION ADIRU 1 SUPPLIES INFORMATION TO: A. THE CAPTAIN'S PFD AND THE FIRST OFFICER'S ND B. THE CAPTAIN'S ND AND THE FIRST OFFICER'S PFD C. THE CAPTAIN'S PFD AND ND D. THE FIRST OFFICER'S PFD AND ND

Answer 61

C. THE CAPTAIN'S PFD AND ND

Question 62

69. IN ROSE NAV MODE WITH VOR 1 SELECTED, THE ND DISPLAYS WHAT VOR INFORMATION? A. DEVIATION BAR, SELECTED COURSE AND THE BEARING POINTER B. BEARING POINTER ONLY C. DEVIATION BAR AND SELECTED COURSE ONLY D. DEVIATION BAR AND BEARING POINTER ONLY

Answer 62

A. DEVIATION BAR, SELECTED COURSE AND THE BEARING POINTER

Question 63

70. IN ROSE ILS MODE, THE ND DISPLAYS WHAT ILS INFORMATION: A. G/S AND LOC SCALES B. DEVIATION BAR AND SELECTED COURSE C. DEVIATION BAR, SELECTED COURSE AND G/S SCALE D. DEVIATION BAR, SELECTED COURSE, G/S AND LOC SCALES

Answer 63

D. DEVIATION BAR, SELECTED COURSE, G/S AND LOC SCALES

Question 64

71. IN THE EVENT OF NO ADF1 RECEPTION, WITH ADF1 SELECTED ON ND: A. THE BEARING POINTER GOES OUT OF VIEW AND ADF FLAG IS DISPLAYED B. THE BEARING POINTER GOES OUT OF VIEW AND STATION ID IS REPLACED BY RED CROSSES C. THE BEARING POINTER GOES RED AND STATION ID IS REPLACED BY FREQUENCY D. THE BEARING POINTER GOES OUT OF VIEW AND STATION ID IS REPLACED BY FREQUENCY

Answer 64

D. THE BEARING POINTER GOES OUT OF VIEW AND STATION ID IS REPLACED BY FREQUENCY

Question 65

72. IN ROSE VOR MODE, IN THE EVENT OF VOR RECEIVER FAILURE: A. THE VOR INFORMATION AND THE COURSE POINTER BECOME RED B. THE VOR INFORMATION BECOMES RED AND THE COURSE POINTER DISAPPEARS C. THE VOR INFORMATION AND THE COURSE POINTER DISAPPEAR D. THE VOR INFORMATION FLASHES AND THE COURSE POINTER DISAPPEARS

Answer 65

B. THE VOR INFORMATION BECOMES RED AND THE COURSE POINTER DISAPPEARS

Question 66

73. DURING TAKE-OFF AND GO AROUND, THE SPEED WINDOW ON THE FCU DISPLAYS: A. THE- SPEED-MANUALLY INSERTED BY THE CREW INTO THE FCU AND THE LIGHT IS OUT B. THE SPEED MANUALLY INSERTED BY THE CREW INTO THIS MCDU AND THE LIGHT IS ILLUMINATED C. DASHES AND THE LIGHT IS ILLUMINATED: MANAGED SPEED SUCH AS V2 OR MEMORIZED VAPP ARE AUTOMATICALLY USED BY THE FMGS

Answer 66

C. DASHES AND THE LIGHT IS ILLUMINATED: MANAGED SPEED SUCH AS V2 OR MEMORIZED VAPP ARE AUTOMATICALLY USED BY THE FMGS

Question 67

74. THE FOLLOWING AP/FD LATERAL MODES ARE MANAGED: A. NAV, HDG, APPR, LOC, RWY, RWY TRK B. HDG, NAV, APPR, LOC, GA TRK C. NAV; APPR, LOC; RWY, RWY TRK, GA TRK

Answer 67

C. NAV; APPR, LOC; RWY, RWY TRK, GA TRK

Question 68

75. IN APPROACH, “LAND" ILLUMINATES GREEN ON FMA WHEN RADIO ALTITUDE IS: A. 700 FEET B. 400 FEET C. 1,000 FEET D. 200 FEET

Answer 68

B. 400 FEET

Question 69

76. ON THE GROUND, THE ENGAGEMENT OF THE AUTOTHRUST FUNCTION: A. MUST BE CARRIED OUT MANUALLY BY THE CREW BEFORE TAKE OFF B. IS PERFORMED AUTOMATICALLY UPON THE SECOND ENGINE START C. IS PERFORMED AUTOMATICALLY AT THE ENGAGEMENT OF THE TAKE OFF MODES

Answer 69

C. IS PERFORMED AUTOMATICALLY AT THE ENGAGEMENT OF THE TAKE OFF MODES

Question 70

77. CLIMBS AND DESCENTS ARE ALWAYS LIMITED: A. BY FLIGHT PLAN (T/C) AND (T/D) POINTS B. BY THE ALTITUDE MANUALLY SELECTED ON THE FCU C. BY THE AIRCRAFT WEIGHT CALCULATED BY THE FMGC

Answer 70

B. BY THE ALTITUDE MANUALLY SELECTED ON THE FCU

Question 71

78. IN FLIGHT, THE FMGS POSITION CAN BE UPDATED: A. WHENEVER A DME STATION IS SELECTED BY THE PILOT B. USING DATA FROM THE SELECTED NDB, VOR OR DME STATIONS C. AUTOMATICALLY WITH THE DME'S THROUGH THE AUTOTUNING FUNCTION

Answer 71

C. AUTOMATICALLY WITH THE DME'S THROUGH THE AUTOTUNING FUNCTION