Book7Qs.txt

1. Which of the VDR Radios is used for Data Communications?
a. VDR 1
b. VDR 2
c. VDR 3

c. VDR 3

2. What stops simultaneous transmission on HF1 and HF2?
a. The Interlock Function inside the AMUs
b. The Interlock Function between the Couplers
c. The Interlock Function inside the HF transceivers

b. The Interlock Function between the Couplers

3. What are the power supplies used by AMU 1?
a. 28 VDC ESS and 28 VDC From DC Bus 1
b. 115 VAC ESS and 115 VAC From AC Bus 1
c. 28 VDC ESS and 115 VAC From AC ESS

a. 28 VDC ESS and 28 VDC From DC Bus 1

4. On the Radio and Audio Management Panel, which of the following has the highest priority?
a. INT PTT has priority over RAD PTT
b. RAD PTT and INT PTT have the same priority
c. RAD PTT has priority over INT PTT

c. RAD PTT has priority over INT PTT

On the Radio and Audio Management Panel, which of the following has the highest priority

5. What are the cockpit indications for a CALL from the Ground Mechanic?
a. The MECH light flashes on the overhead panel and a buzzer sound is heard
b. The MECH light flashes on all MPs and a buzzer sound is heard
c. The MECH light come on steady on all RMPs and a buzzer sound is heard

b. The MECH light flashes on all MPs and a buzzer sound is heard

6. Which Crew Members is AMU 2 dedicated to?
a. CAPT and 3RD Occupant
b. F/O and 3RD Occupant
c. F/O and 4TH Occupant

c. F/O and 4TH Occupant

7. On any Radio and Audio Management Panel, how may transmission keys can be selected at any one time?
a. As many as the operator requires
b. A maximum of two at a time
c. Only one can be selected at a time

c. Only one can be selected at a time

On any Radio and Audio Management Panel, how may transmission keys can be selected at any one time

8. Which radio systems is the Avionic Communication Routing System linked to?
a. VDR 1, HF 1, HF 2 and SATCOM
b. VDR 1, VDR 3, HF 1, and SATCOM
c. VDR 3, HF 1, HF 2 and SATCOM

c. VDR 3, HF 1, HF 2 and SATCOM

9. When is the CVR powered?
a. All the time the aircraft is electrically powered
b. On the ground when at least one ENG MASTER SW is ON
c. On the ground when only two or more ENG MASTER SWs are ON

b. On the ground when at least one ENG MASTER SW is ON

NAVIGATION

ADIRUs

10. For each Air Data Inertial Reference Unit, how many Multi Function Probes are installed?
a. One
b. Two
c. Three

a. One

For each Air Data Inertial Reference Unit, how many Multi Function Probes are installed

11. What power supplies are used for Integrated Static Probes?
a. 28VDC for the Digital Converter and 28VDC for anti-icing function
b. 115VAC for the Digital Converter and 115VAC for anti-icing function
c. 28VDC for the Digital Converter and 115VAC for anti-icing function

c. 28VDC for the Digital Converter and 115VAC for anti-icing function

12. After an ADR 2 FAULT indication, what action is required to recover ADR information?
a. F/O selects AIR DATA SW to F/O ON 3
b. F/O selects AIR DATA SW to F/OT ON 2
c. No action required as the switching is automatic

a. F/O selects AIR DATA SW to F/O ON 3

After an ADR 2 FAULT indication, what action is required to recover ADR information

STANDBY NAV

13. Which MMR is used to supply the ISIS with ILS DATA?
a. MMR 1 and MMR 2
b. MMR 2 Only
c. MMR 1 Only

c. MMR 1 Only

14. Which ADIRU normally supplies the ISIS with IR DATA?
a. ADIRU 1
b. ADIRU 2
c. ADIRU 3

c. ADIRU 3

15. Which ADIRU is used as the backup for the ISIS IR DATA?
a. ADIRU 1
b. ADIRU 2
c. ADIRU 3

a. ADIRU 1

RADIO NAV TUNING

16. How is manual tuning of a Radio Nav System indicated to the crew?
a. The RADIO NAV information on the ND changes colour
b. The RADIO NAV information on the ND changes size
c. By an M on the ND next to the RADIO NAV information

c. By an M on the ND next to the RADIO NAV information

17. How is back up tuning of a Radio Nav System indicated to the crew?
a. The RADIO NAV information on the ND changes colour
b. The RADIO NAV information on the ND changes size
c. By an R on the ND next to the RADIO NAV information

c. By an R on the ND next to the RADIO NAV information

18. In normal operation, how are the Radio Navigation Systems Tuned?
a. Automatically by their own side RMP
b. Automatically by the master Flight Management Computer
c. Automatically by their own side Flight Management Computer

c. Automatically by their own side Flight Management Computer

MMR

19. When is ILS information displayed on a PFD?
a. As soon as valid ILS information is available
b. When the LS P/B is pressed on the EFIS Control Panel
c. When selected through the Multi Function Displays

b. When the LS P/B is pressed on the EFIS Control Panel

20. Where is GPS information displayed?
a. On the MFDs, NDs and ISIS
b. On the MFDs, PFDs and ISIS
c. On the PFDs, NDs and ISIS

a. On the MFDs, NDs and ISIS

21. After landing gear extension, when is the ILS TUNE/TEST inhibit issued?
a. Below 500 Ft
b. Below 700 Ft
c. Below 900 Ft

b. Below 700 Ft

22. When is A information displayed on the PFDs?
a. From ground level up to 2500 Ft
b. From ground level up to 5000 Ft
c. From ground level up to 7500 Ft

a. From ground level up to 2500 Ft

23. To what altitude is RA information valid for user systems?
a. 2500 Ft
b. 5000 Ft
c. 7500 Ft

b. 5000 Ft

VOR/MKR/DME

24. Where is DME information displayed?
a. On the PFDs and on the NDs
b. On the NDs and the ISIS
c. On the PFDs and the ISIS

a. On the PFDs and on the NDs

25. Where is MKR information displayed?
a. On the PFD only
b. On the ND only
c. On the ISIS only

a. On the PFD only

AESS

26. What are the TCAS display limits when BLW is selected on the AESS CP?
a. Minus 2700 feet to Plus 2700 feet from current A/C Altitude
b. Minus 2700 feet to Plus 9000 feet from current A/C Altitude
c. Minus 9000 feet to Plus 2700 feet from current A/C Altitude

c. Minus 9000 feet to Plus 2700 feet from current A/C Altitude

27. Apart from the I/0 and Alert Priority module, how are the other four modules grouped together?
a. WRX/TAWS Group and TCAS/ATC Group
b. WRX/ATC Group and TCAS/TAWS Group
c. WRX/TCAS Group and TAWS/ATC Group

a. WRX/TAWS Group and TCAS/ATC Group

Apart from the I/0 and Alert Priority module, how are the other four modules grouped together

AFS

28. With all engines operating, what happens when an ALPHA FLOOR condition is detected?
a. A Master Warning is issued for the crew to take action
b. A/THR is engaged active, with full thrust on engines 2 and 3
c. A/THR is engaged active, with full thrust on all engines

c. A/THR is engaged active, with full thrust on all engines

With all engines operating, what happens when an ALPHA FLOOR condition is detected

29. How are Selected AP/FD Targets shown on the PFDs?
a. By using the colour MAGENTA
b. By using the colour CYAN
c. By using the colour AMBER

b. By using the colour CYAN

30. With all ADIRUs, PRIMs and FCU operative, when can the AP be engaged on the ground?
a. No engines operating with G and Y hydraulic pressures
b. No engines operating and low hydraulic pressure
c. No engines operating with one hydraulic system operating

b. No engines operating and low hydraulic pressure

With all ADIRUs, PRIMs and FCU operative, when can the AP be engaged on the ground

31. What is the make up of the Flight Management System?
a. Two Flight Management Computers
b. Three Flight Management Computers
c. Four Flight Management Computers

b. Three Flight Management Computers

32. How are the Flight Management Computers normally configured?
a. FMC-A Master, FMC-B Slave, FM-C Spare
b. FMC-A CAPT, FMC-B F/O, FM-C Spare
c. FMC-A Master, FMC-B Slave, FM-C Slave

b. FMC-A CAPT, FMC-B F/O, FM-C Spare

33. What is the A/THR mode when the ALPHA FLOOR condition is active?
a. A/TH engaged and active, with CL thrust selected
b. A/TH engaged and active, with MCT thrust selected
c. A/TH engaged and active, with TOGA thrust selected

c. A/TH engaged and active, with TOGA thrust selected

LIGHTS

34. What happens to the cabin general lighting in the event of a FAP failure?
a. It is set to 100% brightness
b. It is set to 50% brightness
c. It is set to 25% brightness

b. It is set to 50% brightness

35. Which unit synchronises the Beacon Lights and the Strobe Lights?
a. The Strobe Lights Power Supply Unit
b. The Upper Beacon Light Power Supply Unit
c. The Lower Beacon Light Power Supply Unit

c. The Lower Beacon Light Power Supply Unit

36. What happens to the cabin general lighting in the event a Cabin Decompression?
a. It is set to 100% brightness
b. It is set to 50% brightness
c. It is set to 25% brightness

a. It is set to 100% brightness

37. What signal is used to automatically turn off the Runway Turn Off Lights?
a. The Left Body Gear Downlocked Signal
b. The Right Body Gear Downlocked Signal
c. The Nose Landing Gear Downlocked Signal

c. The Nose Landing Gear Downlocked Signal

38. On the FAP, when is the cabin Main ON/OFF button active?
a. In Flight only
b. On the ground only
c. In flight or on the ground

b. On the ground only

39. What signal is used to automatically turn off the Taxi and Take Off Lights?
a. The Left Body Gear Downlocked Signal
b. The Right Body Gear Downlocked Signal
c. The Nose Landing Gear Downlocked Signal

c. The Nose Landing Gear Downlocked Signal

CABIN

40. Which LRUs are used the interface between the directors and the cabin crew function?
a. The MP FAPs
b. The DEU As
c. The DEU Bs

c. The DEU Bs

Which LRUs are used the interface between the directors and the cabin crew function

41. Which source has the highest priority over the PA System?
a. The cabin handsets
b. The cockpit handset
c. The cockpit acoustic equipment

c. The cockpit acoustic equipment

42. In normal operation, what is the configuration of the CIDS Directors?
a. DIR 1 Active with DIR 2 in Hot Standby and DIR 3 in Cold Standby
b. DIR 1 Active with DIs 2 and DIR 3 in Hot Standby
c. DIR 1 Active with DIR 2 and DIR 3 in Cold Standby

b. DIR 1 Active with DIs 2 and DIR 3 in Hot Standby

43. On the DEU B Connection Box, what is represented by the AMBER light?
a. That the DC SERV BUS power is available
b. That the DC ESS BUS power is available
c. That there is a failure of the connection box

b. That the DC ESS BUS power is available

44. Which areas are monitored by the CIDS Smoke Detection Function?
a. The Cargo compartments and the Lavatories
b. The Cargo and Avionic compartments
c. The Avionic compartments and the Lavatories

b. The Cargo and Avionic compartments

45. What happens to the Cabin Lights when the CIDS is in Emergency Mode?
a. They are set to 100% Brightness
b. They are set to 50% Brightness
c. They are set to 250% Brightness

b. They are set to 50% Brightness

ATC

46. Where is the ATC Data Link Application hosted?
a. CPIOM-D1
b. CPIOM-D2
c. CPIOM-D3

a. CPIOM-D1

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