2

1- Both FMGCs are inoperative. How are the VOR frequency and course selected?. Manually via the RAD NAV page on MCDUs. Manually via STANDBY NAV key on RMPs. Automatically via the backup nav stored on the MCDUs.

2- Where is displayed the AP, FD, and A/THR engagement status?. On the upper area of E/W-DU. On the upper area of PFDs. On the upper area of NDs.

3- The STBY probes, STATIC and PITOT are connected to.. ADIRU 2. all the three ADIRUs. ADIRU 3.

4- How do the pitot and static probes supply the ADIRUs?. By using an Air Data Module ADM. (digital conversion). Directly with Pitot and Static pressures. By using an Air Data Module ADM. (analog conversion).

5- The ADIRU 3 sends information to.. Only DMC 2 and DMC 3. DMC 1, DMC 2 and DMC 3. Only DMC 1 and DMC 3.

6- When does the ALIGN light flash?. When the present position has not been entered after 10 minutes. When alignment has been completed. During the alignment phase in case of IRS is lost.

7- Which system calculates, using different sensors, the aircraft present position?. The Flight Management part of the FMGCs. The Flight Envelope function of the FACs. The ADIRUs only.

8- Which ADIRU does not supply the DMC 1?. ADIRU 1. ADIRU 3. ADIRU 2.

9- Normally, ADIRU 1 supplies the following EIS-Display Units: Captain's PFD, FO's ND. Captain's PFD and ND. Captain's ND, FO's PFD.

10- CIDS - Where are the Directors located?. In the vertical stabilizer compartment. in the Aft Avionics compartment, rack 80 VU. in the Aft Cargo compartment.

11- Where are the TAT and SAT indicated?. In the PFD. In an analog indicator. In the ECAM SD.

12- Where is the SELCAL CODE assigned to the aircraft selected?. On a selcal code panel located on the overhead panel. On a selcal code panel located above the electronics rack 80VU. On the MCDU.

13- The message "VHF CONT EMITTING" is activated... ...on ECAM in case of transmitting VHF longer than 30s. ...on ECAM in case of transmitting VHF longer than 35s. ...on ECAM in case of transmitting VHF longer than 60s.

14- How is possible to see the GPS data?. On the ND when the PLAN mode is selected. On the MCDU via the CMS in the NAVIGATION menu. On the MCDU via DATA INDEX and GPS MONITOR page.

15- ADIRU 3 receives TAT information from... the Captain's and First Officer's TAT sensors. the Captain's TAT sensor. the standby TAT sensor.

16- The characteristic tone of the Outer Marker Modulation is... 400Hz. 1300 MHz. 112 Hz.

17- The VHF communication system allows..... Only allowed to listen. Long distance voice communication. Short distance voice communication.

18- Which computers process the yaw damper order if the autopilot is not engaged?. Either the ELAC or the FAC (Flight Augmentation Computer). Either the FMGC (Flight Management Guidance and Computer) or the ELAC (Elevator Aileron Computer). The FMGCs and the FACs.

19- The comunication systems are used for: Comunications betwen flight crew and cabin crew. Only comunications betwen flight crew. Comunications betwen aircraft/aircraft, aircraft/ground station, all flight crew and intercomunications betwen cabins (cockpit and passengers cabin).

20- What are the ADIRU's operation modes?. Vertical speed and TAS modes. Navigation (NAV) and Attitude (ATT). Attitude and Hold modes.

21- During the final approach the Pilot set both Thrust Lever to the IDLE stop.What happens with the autothrust system?. The A/THR pb is ON and the function remain engaged but is not active. The A/THR function disengages and the ATHR pb light is OFF. The autothrust remains engaged and the ASYM message is displayed on PFDs.

22- CIDS - How are the DEUs A connected to the Directors?. By means of 4 Middle Line data buses. By means of 2 Top Line data buses. By means of 4 Top Line data buses.

23- The ATIMS is composed of... ATSU (Air Traffic Service Unit), 2 DCDUs (Datalink Control and Display Units), 2 ATC Message pushbuttons. 2 ATSUs, 2 Antennas, 2 DCDUs (Datalink Control and Display Units), 2 ATC Message pushbuttons. Data Link MU, 2 DCDUs (Datalink Control and Display Units), 2 ATC Message pushbuttons.

24- How can the initiation of Modes 1 to 5 of the Enhanced GPWS (Ground Proximity Warning System) be inhibited?. By switching of the "GPWS-SYS" P/B (Control Panel) to OFF-Position. By switching of the "GPWS-TERR ON" P/B (Instrument Panel) to OFF-Position. By switching of the "GPWS-TERR" P/B (Control Panel) to OFF-Position.

25- Tuning of VHF 1 is possible: through any RMP. through any Audio Control Panel. only through RMP 1.

26- The FAC reset function is: Automatic by means of FMGC. Manual by means of FLT/CTL/FAC pushbutton Sw. It is automatic itself.

27- Where are the windshear indications shown?. PFDs and NDs. DDRMI. Only on the NDs.

28- What is the purpose of the Radio Management Panels (RMP)?. To select the audio signals from ther radio navigation syetems. To tune the frequencies of the radio communication systems and Standby Nav for radio navigation aids. To enable and select the received audio signal.

29- ENHANCED. At the enhanced system the Flight Attendant Panel (FAP) includes: The Vacuum System Control Function (VSCU). The OBRM, CAM and PRAM modules. The BITE test for the Drainmast Heat Control Unit.

30- Where is the DME system information shown?. In the PFDs, NDs and DDRMI. Only in the PFDs. In the ECAM displays only.

31-Where is the Fault Isolation Detection System (FIDS) active?. In the FAC 2. In the FAC 1. In the AIDS.

32- The installation of Static and Pitot pressure line(s) , which one(s) need(s) to be drained?. All the Stby lines (Pitot and static). All the Pitot lines. Only the Standby Static line.

33- The TAT information for ADIRU# 1 and #3 is delivered by: The #3 TAT sensor. The number 1 TAT sensor. The number 2 TAT sensor.

34- The Auto Pilot is engaged and the Pilot wants to control flight parameters manually by means of FCU, he must do the following: Disconnect the auto pilot. Rotate and pull the associated selector knob. Push and rotate the selector knob.

35- What is the Audio Management Unit?. It is a computer to improve the audio for the passenger. It is an interface between the users and the Radio Communication and Radio Nav systems. It is an equipment for radio communication.

36- The A/P can be engaged: 5 seconds after the lift off. On ground with both engines running. Only in cruise phase.

37- When do the G/S and LOC scales appear on the PFD?. When ILS is captured. When the ILS pushbutton is selected. When G/S and LOC beams are received.

38- What is the purpose of the "ON VOICE" button located on the ACPs (Audio Control Panel)?. Supression of Morse-Identification of the NAV Receivers. Filtering the backround noise for the Headsets. Activation of squelch for the Communication Transceivers.

39- What is the purpose of the ATSU system?. Provides phone services for the pax. Provides FAX communications for the flight crew only. Provides voice and data communications through the VHF 3 system, HF, SATCOM.

40- When are both Radio Altimeters operating?. In Approach only. Always. During Take-Off only.