Examen

Which AOA-Sensor supplies ADIRU 2?. AOA Sensor 2. ADIRU 2 is not supplied. AOA Sensor 3.

A Pitch indication difference between both ND's is monitored and detected by ... Flight Warning Computers (FVC). Air Data Inertial Reference System (ADIRS ). Display Management Computers ( DMC ).

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

Which DMC(s) get information from the ADIRU 3?. All the DMCs. Only DMCs 1 y 2. Only DMCs 1 and 3.

CIDS - If the Director # 2 fails, during a normal operation: Nothing, the Director #1 remains in control. Director # 1 takes over automatically. Director # 1 must be switched on manually.

CIDS - What are the consequences of a rupture in one of the top data lines?. This only disables the half of the DEUs "A" on one cabin Side. This affects all the type "B" DEUs. This affects all the type "A" DEUs.

On the ADIRS control panel, what happen if the mode switch is moved from Off to Nav?. The ON BAT light comes on for 5 seconds, the Align light come ON. The Fault light is ON for 2 minutes. The ON BAT and the Align will still ON for 10 minutes. Then both goes off.

CIDS - Any failure associated with any system related with the CIDS... will illuminate the CIDS Caution light on FAP. will illuminate a caution light in the ACPs. will illuminate the caution light on PRAM panel.

Electrical emergency configuration (loss of both main generators), which ADIRUs could be available?. The ADIRU 2 or ADIRU 3. The ADIRU 1 or ADIRU 2. The ADIRU 1 or ADIRU 3.

What is the purpose of the RMPs?. To enable the frequencies of all the radio communication systems to be selected. To enable the received audio signals and the frequencies. To enable the cabin interphone communication through the CIDS director 1.

CIDS - What are the units directly related with the pax services?. The Decoder Encoder Unit's A. The Decoder Encoder Unit's B. The Auxiliary Attendant Panels.

In the cockpit, if the amber "CAll" light is illuminated in the ACPs and a buzzer sound is heard;. A Selcall is announced. A Mech call is announced. A cabin call is announced.

To establish a Service Interphone Communication from the Cockpit to the APU... INT has to be selected on the Audio Control Panel. CAB has to be selected on the Audio Control Panel. SERV INT has to be selected on the Audio Control Panel.

How is the TAT/SAT data from ADIRS to ECAM SD provided?. Normally from the ADIRU 2 and from the ADIRU 3 if the ADIRU 2 fails. Normally from the ADIRU 3 and from the ADIRU 2 if the. Normally from the ADIRU 1 and from the ADIRU 2 if the ADIRU 1 fails.

Where are the controls for baro correction located?. On the FCU (EFIS Controls Panels). On the MCDUs. On the ECAM Control Panel.

CIDS - Each DEU has to be addressed to the place where it is located. How it is done?. With coding switches located on each DEU mount. With coding switches located on the last DEU mount. With coding switches in the new DEU.

What is the meaning of IR FAULT light illuminated intermittently?. No present position inserted. Attitude information may be recovered in ATT mode. ADIRU Inertial part totally lost.

How failures are transmitted from the RMP to CFDIU?. Via RMP 1. By any RMP individually. Via RMP 3.

The captain wants to use the VHF # 3 for voice communication. How is this action determined?. By pressing the VHF # 3 selection on the Captain RMP. By a signal from the ACARS. By a signal from the voice/data switch pressed.

ENHANCED. On the enhanced system the Cabin Intercommunication Data System (CIDS) directors are supplied: By the DC Service Bus 601 PP and DC Ess Bus 401 PP. Both DC Ess Bus 401 PP and 115VAC by the AC Ess Bus. By the Hot Battery Bus 702 PP and DC Bat Bus 301 PP.

ENHANCED. Which busses supply the Integrated Standby Instrument System (ISIS)?. Normally, the DC Ess Bus and alternatively the Hot Batter Bus if the airspeed is greater than 50 knots. The Hot Battery Bus and above 50 knots, the Service Bus. BATTERY Bus. Bus N 1 and alleratively the DC.

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

CIDS - Which is the purpose of the Terminator on the last DEU?. To match the line impedance of the data bus cable. To reset the DEU position after replacement. To allow the interchange between DEUs receptacle.

The aircraft is in "emergency electrical configuration". Which parts of the audio management system (AMS) are still active?. ACP of captain and first officer. Flight interphone is still available. Only the captain's ACP is still operative. All three audio control panels (ACP) but flight interphone is lost.

If VHF 2 is selected on RMP 1... the SEL light comes on WHITE on RMP 1 and RMP 2. the SEL light comes on WHITE on RMP 2 and RMP 3. the SEL light comes on WHITE on ACP 1 and ACP 2.

If the VHF-1 system is trasmitting for more than 60 sec., What message is shown in the ECAM?. "VHF-1-Emitting". "HF-1-Emitting". "VHF-2-Emitting".

The cockpit has three Radio Management Panels (RMP). What should happen if RMP # 2 fails?. All the radio communications frequencies can still been tuned from the others RMP. The VHF # 2 and VHF # 3 can not be controlled or tuned. All navigation frequencies can not be controlled.

A/C on ground and engines shutdown, what are the conditions to erase the CVR recording?. GND CTL Pb pressed, parking brake is set and pressing the CVR ERASE Pb for 2 seconds. Press the CVR ERASE pushbutton for at least 2 seconds. Both engine shut down, Parking brake released and erase Pb pressed for 2 seconds.

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

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

If there is a difference in the comparison of latitude during the alignment(the first time that the data entry, the indication is: The ALIGN legend flashes on the ADIRS CDU. It will not be shown on the ADIRS CDU. The IR FAULT legend flashes on the ADIRS CDU.

What is the purpose of the SEL light on the RMP?. To indicate that an offside user is selecting a non dedicated communication system. To indicate that the VHF/HF system is receiving a SELCAL code. To alert the flight crew that a SELCAL is being received.

The Service Interphone Amplifier is part of the ... CIDS Director. ACP. AMU.

Where is the Mute accomplished?. Inside of the Capt. or First officer ACP. Inside of the Speaker assy. It is on the RMP.

What component provides control for the Radio Comm and Radio Nav audio signals?. The audio switching panel. The Audio control Panel. The Radio Management Panel.

Where is the Altitude indicated?. PFD (Primary Flight Display). E/W Display (Engine and Warning). ND (Navigation Display).

When is the blue light COCKPIT CALL (in the EXT Power panel), illuminated?. When the Flight Crew is calling the mechanics. When the flight crew is calling the attendant. When the GND SRVCE OVRD push button has been activated.

The Air Data Modules (ADM) transmit pressure data to the ADIRUs from... all pitot probes and the static system. the static ports only. the pitot probes only.

Where is the Flight Interphone module installed?. Inside of both CIDS Directors. Inside of the AMU. Inside of the Director 1.

What is the power source of the HF1 coupler?. The HF1 transceiver (4RE1). The DC ESS SHED BUS (801PP). The AC BUS 2 (202 XP).