Comunicación

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

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 De selected. To enable the cabin interphone communication through the CIDS director 1.

ENHANCED. Which busses supply the Integrated Standby Instrument System (ISIS)?. Normally, the DC Ess Bus and alternatively the Hot Battery Bus if the airspeed is greater than 50 knots. Normalv ine ue bus n tane alemanvery ine Du BATTERY Bus. The Hot Battery Bus and above 50 knots, the Service Bus.

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

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

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

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

What component provides control for the Radio Comm and Radio Nav audio signals?. The audio control panel. The radio management panel. The audio switching panel.

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

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

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

The service interphone Amplifier is part of the. CIDS Director. ACP. AMU.

It 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 ACP 1 and ACP 2. the SEL light comes on WHITE on RMP 2 and RMP 3.

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

Which AOA-sensor suppiles ADIRU 21. AOA Sensor 2. AOA Sensor 3. ADIRU 2 is not supplied.

ENHANCED. On the ennanced system ine Cabin intercommunication Data system (CIDs) directors are supplied: By the Hot Battery Bus 702 PP and DC Bat Bus 301 PP. By the DC service bus 601 PP and DC Ess Bus 401 PP. By the DC Ess Bus 401 PP and 115VAC by the AC Ess Bus 401 XP.

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 voice/data switch pressed. By a signal from the ACARS.

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

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

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

Where is the altitude indicated. PFD (PRIMARY FLIGHT DISPLAY). ND (Navigation Display). EN Display (Engine and Warning).

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 alert the flight crew that a SELCAL is being received. To indicate that the VHF/HF system is receiving a SELCAL couc.

How is the TAT/SAT data from ADIRS to ECAM SD provided?. Normally trom the ADIRU 3 and from the ADIRU 2 if the ADIRU 3 fails. ADIRU 1 fails vormally irom une AuIkuT ano womune ADIKU ZIle. Normally from the ADIRU 2 and from the ADIRU 3 if the ADIRU 2 fails.

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).

To establish a Service Interphone Comunication from the Cockpit to the APU... CAB has to be selected on the Audio Control Panel. Serv INT has to be selected on the audio control panel. INT has to be selected on the Audio Control Panel.

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

The cockpit has three radio management panels (RMP) what should happen if RMP # 2 fails?. All the radio communication frequencies can still been tuned from the others RMP. All navigation frequencies can not be controlled. The VHF # 2 and VHF # 3 can not be controlled or tuned.

How failures are transmitted from the RMP to CFDIU?. Via RMP 1. By any RMP individually. Via RMP 2.

Where is the flignt interphone module installed?. Inside of the AMU. Inside of both CIDS Directors. inside of the Director 1.

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

If there is a difference in the comparison of altitude 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.

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

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. Both engine shut down, Parking brake released and erase Pb pressed for 2 seconds. Press the CVR ERASE pushbutton for at least 2 seconds.

Where is the Mute accomplished?. Inside of the speaker assy. inside orme caotorrirst oncer ACH. it is on the RMP.

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. This affects all the type "A" DEUs. This affects all the type "B" DEUs.

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

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

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

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