aircraft systemscaacongo.com/corporate/co_at_fcom/pdf_n_fcom_82u_tf_n_eu... · 2014. 3. 6. ·...

AIRCRAFT SYSTEMS

COMMUNICATIONS

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A318/A319/A320/A321FLIGHT CREW

OPERATING MANUAL

AIRCRAFT SYSTEMSCOMMUNICATIONS

PRELIMINARY PAGES - TABLE OF CONTENTS

82U A318/A319/A320/A321 FLEET DSC-23-PLP-TOC P 1/4FCOM 06 MAR 14

DSC-23-10 Radio CommunicationDSC-23-10-10 General

GENERAL................................................................................................................................................................ A

DSC-23-10-20 VHF/HF/SELCALGENERAL................................................................................................................................................................ AVHF.......................................................................................................................................................................... BHF ...................................................................................................................................................................CSELCAL (Selective calling)..................................................................................................................................... D

DSC-23-10-30 Radio TuningDescription............................................................................................................................................................... ARadio Management Panel ......................................................................................................................................B

DSC-23-10-50 Electrical SupplyBUS EQUIPMENT LIST.......................................................................................................................................... A

DSC-23-20 Intercommunication SystemsDSC-23-20-10 General

GENERAL................................................................................................................................................................ AAudio Management System ................................................................................................................................... BCabin Intercommunication Data System.................................................................................................................C

DSC-23-20-20 ControlsAudio Control Panel.................................................................................................................................................ASIDE STICK RADIO SELECTOR............................................................................................................................BLOUDSPEAKER VOLUME KNOB.......................................................................................................................... CAUDIO SWITCHING................................................................................................................................................D

DSC-23-20-30 Interphone SystemsFlight Crew Interphone System...............................................................................................................................ACabin Interphone System........................................................................................................................................ BSERVICE INTERPHONE SYSTEM........................................................................................................................ C

DSC-23-20-40 Call SystemsGround Mechanic Call............................................................................................................................................. ACabin Call System...................................................................................................................................................B

DSC-23-20-50 Passenger AddressPassenger Address..................................................................................................................................................A

Continued on the following page


OPERATING MANUAL




Continued from the previous page1 DSC-23-20-60 EMER EVAC

EMER EVAC............................................................................................................................................................APURSER STATION................................................................................................................................................. B

DSC-23-20-70 Electrical SupplyBUS EQUIPMENT LIST.......................................................................................................................................... A

DSC-23-30 COCKPIT VOICE RECORDER2 DSC-23-30-10 DESCRIPTION

DESCRIPTION.........................................................................................................................................................A

DSC-23-30-20 CONTROLS AND INDICATORS ON OVERHEAD PANELCONTROLS AND INDICATORS ON OVERHEAD PANEL.................................................................................... A

DSC-23-30-30 ELECTRICAL SUPPLYBUS EQUIPMENT LIST.......................................................................................................................................... A

DSC-23-35 Emergency Locator TransmitterDSC-23-35-10 Controls and Indicators

Controls and Indicators............................................................................................................................................A

DSC-23-40 ACARSDSC-23-40-10 General

Introduction...............................................................................................................................................................ASystem Architecture.................................................................................................................................................B

DSC-23-40-20 Cockpit ArrangementCockpit Arrangement............................................................................................................................................... A

DSC-23-40-30 Operations ModesManual Access to ACARS Functions......................................................................................................................AAutomatic Access To ACARS Functions................................................................................................................ B



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Continued from the previous pageDSC-23-40-40 ACARS Functions

General.....................................................................................................................................................................AFMS..........................................................................................................................................................................BACARS.....................................................................................................................................................................CCFDS....................................................................................................................................................................... DAIDS.........................................................................................................................................................................EAutomatic Downlink of Reports............................................................................................................................... FUplink Messages..................................................................................................................................................... GVoice/ACARS Transfer on VHF 3...........................................................................................................................HWorld Map ACARS Frequencies.............................................................................................................................. I

DSC-23-40-50 Electrical SupplyBus Equipment List..................................................................................................................................................A

DSC-23-46 SATCOMDSC-23-46-30 ELECTRICAL SUPPLY

Bus Equipment List..................................................................................................................................................A

DSC-23-50 Warnings and CautionsWarnings and Cautions........................................................................................................................................... A


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OPERATING MANUAL


PRELIMINARY PAGES - SUMMARY OF HIGHLIGHTS

82U A318/A319/A320/A321 FLEET DSC-23-PLP-SOH P 1/4FCOM 06 MAR 14

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DSC-23-PLP-TOCEMER EVAC

1 Documentation update: Deletion of the "00000805.0004001EMER EVAC" documentary unit.Documentation update: Deletion of the "00000812.0003001DESCRIPTION" documentary unit.Documentation update: Deletion of the "00000812.0006001DESCRIPTION" documentary unit.

DSC-23-PLP-TOCDESCRIPTION

2

Improvement of the technical wording for standardizationpurposes.modification of F/O loudspeaker power from DC ESS to DC BUS2,and suppression of the note concerning the AMU power.Documentation update: Information "N.00000619.0001001.212"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.215"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.218"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.221"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.224"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.227"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.230"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.233"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.236"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"Documentation update: Information "N.00000619.0001001.239"moved from "N.00000619.0001001.186" to"N.00000619.0001001.302"

DSC-23-10-50BUS EQUIPMENT LIST

A 1

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A 3

Documentation update: Deletion of text.DSC-23-30-10DESCRIPTION

A 1 Improvement of the technical wording for standardizationpurposes.

DSC-23-30-10DESCRIPTION

A 2 Documentation update: Addition of "DESCRIPTION" documentaryunit


A 2 Effectivity update: The information no longer applies to MSN 0279,0395.

DSC-23-20-60EMER EVAC

A 1 Effectivity update: The information no longer applies to MSN 0279.



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Continued from the previous pageLocalization

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IndexID Reason



DSC-23-40-10Introduction


DSC-23-40-10System Architecture

B 2 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-20Cockpit Arrangement


DSC-23-40-30Manual Access to ACARS Functions


DSC-23-40-30Automatic Access To ACARSFunctions


DSC-23-40-40General


DSC-23-40-40FMS


DSC-23-40-40ACARS

C 3 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40CFDS

D 4 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40AIDS

E 5 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40Automatic Downlink of Reports

F 6 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40Uplink Messages

G 7 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40Voice/ACARS Transfer on VHF 3

H 8 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-40-40World Map ACARS Frequencies

I 9 Effectivity update: The information no longer applies to MSN 0395.

DSC-23-50Warnings and Cautions



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OPERATING MANUAL


RADIO COMMUNICATION - GENERAL

82U A318/A319/A320/A321 FLEET DSC-23-10-10 P 1/2FCOM A 07 OCT 11

GENERALIdent.: DSC-23-10-10-00000612.0001001 / 10 DEC 09Applicable to: ALL

The communications system comprises the following subsystems :‐ VHF/HF transceivers‐ Radio tuning systems (Radio Management Panels).‐ Audio integrating system (Audio Management Unit, Audio Control Panels).


OPERATING MANUAL


RADIO COMMUNICATION - GENERAL


82U A318/A319/A320/A321 FLEET DSC-23-10-10 P 2/2FCOM 07 OCT 11


OPERATING MANUAL


RADIO COMMUNICATION - VHF/HF/SELCAL

82U A318/A319/A320/A321 FLEET DSC-23-10-20 P 1/2FCOM A to D 07 OCT 11


Either of the two Radio Management Panels (RMPs) (third RMP ) can be used to tune eachtransceiver.To transmit, the flight crew uses the Audio Control Panel (ACP) to select a VHF or HF system. TheACP works through the Audio Management Unit (AMU). Each system is connected to the RMPs, forfrequency selection, and to the AMU for connection to the audio integrating and SELCAL (selectivecalling) systems.

VHFIdent.: DSC-23-10-20-00000614.0001001 / 16 FEB 11Applicable to: ALL

Two identical VHF communication systems (third VHF system ) are installed.Each system has a transceiver in the avionics compartment, and an antenna on the fuselage. OnlyVHF1 functions in EMER ELEC CONFIG. Its range is from 118.0 to 136.975 MHz.VHF has an alarm which indicates if the microphone is stuck. If a microphone is in the emissionposition for more than 30 s, an interrupted tone sounds for 5 s, and the emission is turned off. Toreactivate the emission, the crew releases the push-to-talk button and presses it again.

HF Ident.: DSC-23-10-20-00000615.0001001 / 16 FEB 11Applicable to: ALL

Two identical HF communication systems are optional. Each has a transceiver in the avionicscompartment, and a common tuner and antenna in the vertical stabilizer. Its range is from 2.8 to24 MHz.

SELCAL (SELECTIVE CALLING)Ident.: DSC-23-10-20-00000616.0001001 / 10 DEC 09Applicable to: ALL

Upon receiving a call code corresponding to that of the aircraft, the SELCAL system aurally andvisually advises the flight crew that a ground station is calling the aircraft.The aural warning is inhibited during takeoff and landing.


OPERATING MANUAL


RADIO COMMUNICATION - VHF/HF/SELCAL




OPERATING MANUAL


RADIO COMMUNICATION - RADIO TUNING

82U A318/A319/A320/A321 FLEET DSC-23-10-30 P 1/4FCOM A 11 DEC 13

DESCRIPTIONIdent.: DSC-23-10-30-00000617.0001001 / 13 DEC 12Applicable to: ALL

Identical Radio Management Panels (RMPs):‐ Give the flight crew control of all VHF radio communication systems (HF systems ).‐ Provide backup to the FMGCs for controlling radio navigation systems (Refer to DSC-34-30-10

General).The two RMPs are on the center pedestal (and the third is on the overhead panel).Each RMP can control any VHF (HF ) transceiver. RMP1 and RMP2 are connected directly to allVHF (HF ) transceivers, (whereas RMP3 is connected to them via RMP1 and RMP2). RMPsare connected together so that each RMP is updated to the selections made on the other RMPs.Only RMP1 functions in EMER ELEC CONFIG.

If one RMP fails, the remaining one controls all the VHF (HF ) transceivers.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-10-30 P 2/4FCOM B → 11 DEC 13

RADIO MANAGEMENT PANELIdent.: DSC-23-10-30-00000618.0001001 / 18 JUL 13Applicable to: ALL

(1) Frequency displaysThe ACTIVE display window shows the active frequency of the selected radio, which isidentified by a green light on the selection key.The STBY/CRS (standby/course) display window shows a standby frequency that the pilot canactivate by pressing the transfer key or change by rotating the tuning knobs. (For a descriptionof the CRS function Refer to DSC-34-30-30 Radio Management Panel (RMP)).

(2) Transfer keyPressing this key moves the active frequency to the standby window and the standbyfrequency to the active window.This tunes the selected receiver to the new active frequency.

(3) Radio com selection keysWhen the pilot presses one of these keys:• The ACTIVE window displays the frequency set on that radio.• The STBY/CRS window displays the selected standby frequency or course.• The selected key displays a green monitor light.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-10-30 P 3/4FCOM ← B 11 DEC 13

(4) Frequency selector knobsThe pilot uses these concentric knobs to select the STBY frequency or CRS.The outer knob controls whole numbers; the inner knob controls decimal fractions.

(5) AM pushbuttonIf the aircraft has HF radios and the flight crew has selected an HF tranceiver, this switchselects the AM mode. (The default mode is the SSB, or single side-band mode).This key displays a green monitor light when the AM mode is active.

(6) SEL indicatorThe SEL indicator on both RMPs comes on amber when a transceiver, normally associatedwith one RMP, is tuned by another:• If 2 RMP installed:

‐ VHF1 ( VHF3, HF1 ), tuned by RMP2,‐ VHF2 ( HF2 ), tuned by RMP1.

• If 3 RMP installed:‐ VHF1 tuned by RMP2 or RMP3,‐ VHF2 tuned by RMP1 or RMP3,‐ VHF3, HF1, ( HF2 ) tuned by RMP1 or RMP2.

(7) NAV pushbutton (with transparent switchguard)The pilot presses this key to select navigation receivers and courses through the RMP. It doesnot affect the selection of communication radios and their frequencies. (Refer to DSC-34-30-30Radio Management Panel (RMP), for additional information).

(8) Radio navigation selection keysThe pilot presses one of these keys to select a navigation radio to control through this RMP.This turns on the key’s green monitor light.Refer to DSC-34-30-30 Radio Management Panel (RMP), for additional information.

(9) ON/OFF switchThis switch controls the RMP power supply.Note: RMP3 is able to control VHF and HF transceivers through RMP1 and RMP2 even

when either of the latter is OFF.


OPERATING MANUAL




82U A318/A319/A320/A321 FLEET DSC-23-10-30 P 4/4FCOM 11 DEC 13


OPERATING MANUAL


RADIO COMMUNICATION - ELECTRICAL SUPPLY

82U A318/A319/A320/A321 FLEET DSC-23-10-50 P 1/2FCOM A → 06 MAR 14

BUS EQUIPMENT LISTIdent.: DSC-23-10-50-00000619.0001001 / 24 FEB 14Applicable to: MSN 0112, 0342

1NORM EMER ELEC

AC DC ACESS

DCESS HOT

VHF1 XVHF2 DC2

VHF3 DC1HF1 AC1HF2 AC2

RMP1 XRMP2 DC2

RMP3 DC1CAPT ACP X

F/O ACP XTHIRD ACP DC1

FOURTH ACP DC1SELCAL DC1

FLT INTERPHONE XCAPT LOUDSPEAKER X(1)

F/O LOUDSPEAKER DC2

RADIOCOMMUNICATIONS

EXT HORN HOT 2

(1) Normal supply is from DC ESS BUS.


OPERATING MANUAL


RADIO COMMUNICATION - ELECTRICAL SUPPLY

82U A318/A319/A320/A321 FLEET DSC-23-10-50 P 2/2FCOM ← A 06 MAR 14

BUS EQUIPMENT LISTIdent.: DSC-23-10-50-00000619.0002001 / 24 FEB 14

2 Applicable to: MSN 0189

3NORM EMER ELEC

AC DC ACESS

DCESS HOT

VHF1 XVHF2 DC2

VHF3 DC1HF1 SHEDHF2 AC2

RMP1 XRMP2 DC2

RMP3 DC1CAPT ACP X

F/O ACP XTHIRD ACP DC1

FOURTH ACP DC1SELCAL DC1

FLT INTERPHONE XCAPT LOUDSPEAKER X(1)

F/O LOUDSPEAKER DC2

RADIOCOMMUNICATIONS

EXT HORN HOT 2(1) Normal supply is from DC ESS BUS.


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - GENERAL

82U A318/A319/A320/A321 FLEET DSC-23-20-10 P 1/4FCOM A to B → 30 MAY 12


Intercommunications is divided into two main systems:‐ The audio management system.‐ The cabin intercommunication data system.

AUDIO MANAGEMENT SYSTEMIdent.: DSC-23-20-10-00000621.0001001 / 14 MAY 12Applicable to: ALL

The audio management system allows the flight crew to use :‐ All the radio communication and radio navigation facilities installed on the aircraft in transmission

and reception mode.‐ The interphone systems‐ The call systems‐ The passenger address systemThe audio management system includes :‐ An audio management unit (AMU)‐ Three audio control panels (ACPs) (fourth and fifth optional)‐ Sockets at each station

• Headset jack and boomset connector (hand microphone connector ) for pilot, copilot, andthird occupant

• Headset jack for fourth occupant‐ One interphone jack at the ground power receptacle‐ Boomsets for the pilot, copilot, and third occupant, and three hand microphones (fourth )‐ Three cockpit oxygen mask microphones‐ One radio press-to-talk switch on each sidestick‐ One SELCAL code selection panel (avionics compartment)‐ Two cockpit loudspeakers with separate volume controls‐ If installed, a jack panel in the electronic compartment that groups the headset jack, service

interphone jack, hand mike connector, and boomset‐ An audio switching facilityIf audio channel 1 or 2 fails due to a failure either in an ACP or the corresponding AMU, the crew canuse the AUDIO SWITCHING selector to select the third audio channel.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-10 P 2/4FCOM ← B → 30 MAY 12


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-10 P 3/4FCOM ← B to C → 30 MAY 12

LOCATION OF COMPONENTS (PILOT’S STATION)

CABIN INTERCOMMUNICATION DATA SYSTEMIdent.: DSC-23-20-10-00000622.0001001 / 15 FEB 11Applicable to: ALL

The Cabin Intercommunication Data System (CIDS) transmits, controls, and processes signals forthe following cabin systems:‐ Cabin and service interphone‐ Passenger address‐ Passenger lighted signs‐ Reading light‐ General cabin illumination


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-10 P 4/4FCOM ← C 30 MAY 12

‐ Emergency evacuation signalling‐ Lavatory smoke indication‐ Passenger entertainment music and video ‐ Escape slide bottle pressure monitoring The CIDS has the following main components:‐ Two CIDS directors connected in parallel, one active, and the other on standby.‐ Forward attendant panel for control of the cabin systems.‐ Programming and test module that allows the system to be reprogrammed after changes are

made in the cabin configuration.

Decoder/Encoder Units (DEUs) linked to the two directors.‐ Type A units (for passengers) installed along each side of the passenger cabin.

The loudspeakers, lighted signs, call buttons, call lights and general illumination ballast units aredivided into small groups, each connected to a type A DEU.

‐ Type B units (for attendants) installed near the exit doors. The Area Call panels, attendanthandsets, slide and door pressure sensors, and attendant indicator panels, are connected to typeB DEUs.


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - CONTROLS

82U A318/A319/A320/A321 FLEET DSC-23-20-20 P 1/4FCOM A → 15 FEB 13

AUDIO CONTROL PANELIdent.: DSC-23-20-20-00000631.0001001 / 14 MAY 12Applicable to: ALL

(1) Transmission keysPressed : The associated channel is selected for transmission.

The three green lines come on.The pilot deselects the channel by pressing the pushbutton again, or byselecting another channel.

CALL : The legend flashes amber (and buzzer sounds) when the SELCAL systemdetects a call.

MECH : The legend flashes amber (and buzzer sounds) for a call from the nose gearbay. The MECH light goes off after 60 s, if it is not reset.

ATT : The legend flashes amber (and buzzer sounds) for a call from a cabinattendant. The ATT light goes off after 60 s, if it is not reset.

(2) Reception knobs‐ Pressing and releasing the knob (knob out) selects the associated audio reception channel

and the integral white light comes on‐ Rotating the knob adjusts the volume


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-20 P 2/4FCOM ← A 15 FEB 13

‐ The INTEG LT knob controls the brightness‐ Pressing the knob (knob stays in) disconnects the associated audio reception channel.Note: To receive DME audio navigation signals that are associated with an ILS or MLS

station: The flight crew must not only select the ILS pb (or LS pb) on the FCU, butalso the VOR reception channel on the ACP. It is possible that the audio signals ofthe VOR, the ILS, and the DME (associated with ILS) could all sound at the sametime.

(3) SELCAL/CALL RESET keyPressing this key extinguishes CALL, MECH, and ATT lights.

(4) ON VOICE keyThis key allows the flight crew to inhibit the audio navigation signals (VOR, ADF)Pressing this key filters out IDENT signals and turns on the green ON light.

(5) INT/RAD switchThis switch operates as a press-to-talk switch for boom mike or oxygen mask mike.INT : Boom and mask mikes transmit on interphone regardless of

which transmission key is selected. For reception on interphone,the crew member must have INT selected (INT reception knobout).

Neutral : Reception is normal. Boom and mask mikes do not transmit.RAD (press and hold) : Boom and mask mikes transmit on the radio selected on the

audio control panel.

(6) Passenger address (PA) function(Refer to DSC-23-20-50 Passenger Address )


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-20 P 3/4FCOM B to C → 15 FEB 13

SIDE STICK RADIO SELECTORIdent.: DSC-23-20-20-00000646.0001001 / 14 MAY 12Applicable to: ALL

This selector has the same function as the INT/RAD switch on the ACP.NEUTRAL (spring-loaded) : Boom and mask mikes are dead.

Reception is normal.RADIO (squeezed) : Boom and mask mikes transmit through the equipment selected by

the transmission key on the ACP.Note: If RADIO is selected on the side stick when the INT/RAD switch is on INT, the radio

function has priority over the interphone function.

LOUDSPEAKER VOLUME KNOBIdent.: DSC-23-20-20-00000662.0001001 / 19 DEC 12Applicable to: ALL

This knob adjusts the volume of the loudspeaker for radio communication.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-20 P 4/4FCOM ← C to D 15 FEB 13

OFF : Loudspeaker does not respond to signals from the aircraft's radioequipment.

Clockwise rotation : Loudspeaker broadcasts signals from the aircraft's radio equipment atincreasing volume.

Note: This knob does not control the loudness of aural alert and voice messages.

AUDIO SWITCHINGIdent.: DSC-23-20-20-00000677.0001001 / 14 MAY 12Applicable to: ALL

The crew can switch to the third ACP if ACP1 or ACP2 fails.When the crew does this, it takes away the third occupant's access to the acoustic equipment.AUDIO 3 XFRD appears in green on the ECAM MEMO display.NORM : Each crew member uses his dedicated communication equipment.CAPT 3: The pilot uses his acoustic equipment and the third occupant's ACP.F/O 3 : The copilot uses his acoustic equipment and the third occupant's ACP.


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - INTERPHONE SYSTEMS

82U A318/A319/A320/A321 FLEET DSC-23-20-30 P 1/6FCOM A → 11 DEC 13

FLIGHT CREW INTERPHONE SYSTEMIdent.: DSC-23-20-30-00000691.0001001 / 03 DEC 13Applicable to: ALL

This system allows the flight crew members to communicate among themselves and, through a jackon the external power panel, with the ground mechanic.EXTERNAL POWER PANEL (FORWARD OF THE NOSE L/G BAY)


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-30 P 2/6FCOM ← A to B → 11 DEC 13

COCKPIT OPERATION FOR GROUND MECHANIC COMMUNICATIONMECH

TRANSMISSIONKEY ON ACP

INT RECEPTIONKNOB ON ACP

INT/RADSW ON ACP

PUSH TO TALKON HANDMIKE

BOOMSETOR OXYGEN

MASKPRESSED OUT

INTOR

RAD-

HANDMIKE PRESSED OUT - PRESSED

CABIN INTERPHONE SYSTEMIdent.: DSC-23-20-30-00000713.0001001 / 13 DEC 12Applicable to: ALL

The system allows the flight crew to communicate with the flight attendants, and the flight attendantsto communicate among themselves.

(1) CAB transmission keyPressed : Three green lines come on.

Boom, mask, and hand mikes may be used for cabin interphone.

(2) CAB reception knobPressed and released(knob out)

: The integral white light comes on.The station receives audio signals from the cabin.Rotating the knob adjusts the volume.

Pressed (knob in) : The white light goes out.The cabin interphone is disconnected.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-30 P 3/6FCOM ← B to C → 11 DEC 13

COCKPIT OPERATION FOR CABIN COMMUNICATIONCAB TRANSMISSION

KEY ON ACPCAB RECEPTION

KNOB ON ACP INT/RAD SW ON ACP PUSH TO TALKON HANDMIKE

BOOMSETOR OXYGEN

MASKPRESSED OUT RAD -

HANDMIKE PRESSED OUT - PRESSED

SERVICE INTERPHONE SYSTEMIdent.: DSC-23-20-30-00000753.0001001 / 19 DEC 12Applicable to: ALL

The system allows for communication between :‐ the flight crew and the service interphone jacks‐ the flight attendant stations and the service interphone jacks‐ the different service interphone jacks.The Service Interphone system has :‐ seven interphone jacks‐ an OVRD switch located on the overhead panel.The audio lines from the interphone jacks are connected to both CIDS directors.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-30 P 4/6FCOM ← C → 11 DEC 13

LOCATION OF INTERPHONE JACKS

CONTROLS AND INDICATORS AT OVERHEAD PANEL


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-30 P 5/6FCOM ← C 11 DEC 13

(1) SVCE INT OVRD pushbutton switchAuto: Ground personnel can communicate with the flight crew by means of the service

interphone jacks 10 s after the aircraft has landed. The landing gear must becompressed.

ON : Communication is possible when the landing gear is not compressed.The ON light is white.

COCKPIT OPERATIONCAB

TRANSMISSIONKEY ON ACP

CABRECEPTION

KNOB ON ACP

INT/RADSW ON ACP


SVCE INTOVRD PB SW

BOOMSET PRESSED OUT RAD –HANDMIKE PRESSED OUT – PRESSED

SEE ABOVECONDITIONS.


OPERATING MANUAL






OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - CALL SYSTEMS

82U A318/A319/A320/A321 FLEET DSC-23-20-40 P 1/8FCOM A → 11 DEC 13

GROUND MECHANIC CALLApplicable to: ALL

Ident.: DSC-23-20-40-A-00000801.0001001 / 10 DEC 09

GENERALThe system allows the flight crew and ground mechanics to communicate with each other.

Ident.: DSC-23-20-40-A-00000800.0001001 / 09 AUG 13

CONTROLS AND INDICATORS ON OVERHEAD PANELThe here above is applicable to the CALLS panel on the overhead panel.

MECH pbPressed (and held) : COCKPIT CALL lights up blue on the external power panel in the nose

L/G bay.An external horn sounds.

Released : COCKPIT CALL remains lighted.The ground mechanic can extinguish it by pressing the RESET buttonon the external power panel. The external horn stops sounding.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-40 P 2/8FCOM ← A → 11 DEC 13

Ident.: DSC-23-20-40-A-00000802.0001001 / 19 DEC 12

CONTROLS AND INDICATORS ON THE EXTERNAL POWER PANEL

(1) COCKPIT CALL pushbuttonPressed : This calls the cockpit.

The MECH lights flash amber on the ACPs and a buzzer sounds.Released: The MECH lights go out after 60 s if they are not reset on the ACPs.

The buzzer stops.

(2) COCKPIT CALL lightThe blue light appears when cockpit calls the ground mechanic. An external horn alsosounds.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-40 P 3/8FCOM ← A to B → 11 DEC 13

(3) RESET pushbuttonPressed: The COCKPIT CALL light goes out.

CABIN CALL SYSTEMApplicable to: ALL

Ident.: DSC-23-20-40-B-00000803.0001001 / 10 DEC 09

GENERALThe cabin call system is for communication between the cockpit and the cabin.

Ident.: DSC-23-20-40-B-00000798.0001001 / 09 AUG 13

CALLS FROM THE COCKPITThe pushbuttons described here below are installed on the CALLS panel located on the overheadpanel.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-40 P 4/8FCOM ← B → 11 DEC 13

PURS /FWD/MID /EXIT /AFT PUSHBUTTON

When pressed, the following aural and visual alerts will trigger in the cabin:‐ Two lights come on in pink on the related area of the CALLS panel, as applicable.‐ On the Attendant Indication Panel (AIP), the “CAPTAIN CALL” message appears and a light

comes on in green.‐ A high-low chime sounds in the related section of the cabin, as applicable.

ALL pb

When pressed, all the stations simultaneously respond, as indicated above.EMER pb-sw (GUARDED)

When pressed, the following aural and visual alerts will trigger in the cabin:‐ Two pink lights flash on all area call panels.‐ The “EMERGENCY CALL” message appears on all AIPs.‐ A high-low chime sounds three times, on all of the loudspeakers.Also, on the cockpit CALLS panel, the ON light flashes in white and the CALL light flashes inamber.


OPERATING MANUAL




The following aural and visual alerts will trigger in the cockpit, when an emergency call is madefrom the cabin to the cockpit:‐ On the EMER pb-sw: The ON light flashes in white, and the CALL light flashes in amber.‐ The ATT lights will flash on all Audio Control Panels (ACPs).‐ Three buzzers will sound consecutively (for approx. three seconds each).The cabin call system will reset, when the cabin crewmember hangs up the handset.

TT light

When the TT pb on the FWD or AFT Attendant Panel is pressed, the TT light on the cockpitCALLS panel comes ON and a buzzer sounds three times in the cockpit.

ATTND ADV pb

When pressed, in the case of an imminent takeoff or landing, the ON light comes on in blue, inaddition to a green light on the area call panel in the cabin.


OPERATING MANUAL




Ident.: DSC-23-20-40-B-00000799.0001001 / 14 MAY 12

CALLS FROM THE CABIN

(1) CPT keyWhen pressed, the following aural and visual alerts will trigger in the cockpit:‐ The ATT lights will flash on all Audio Control Panels (ACPs).‐ A buzzer (inhibited during takeoff and landing) will sound.In the cabin, the “CAPTAIN” message will appear on the Attendant Indication Panel (AIP) forwhich the CPT key was pressed.

(2) EMER CALL key When pressed, the following aural and visual alerts will trigger in the cockpit:‐ On the EMER pb-sw: The ON light flashes in white, and the CALL light flashes in amber.‐ The ATT lights will flash on all ACPs.‐ Three buzzers (inhibited during takeoff and landing) will sound consecutively.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-20-40 P 7/8FCOM ← B 11 DEC 13

In the cabin, the “EMERGENCY CALL” message will appear on all AIPs.


OPERATING MANUAL






OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - PASSENGER ADDRESS


PASSENGER ADDRESSIdent.: DSC-23-20-50-00000804.0001001 / 18 DEC 12Applicable to: ALL

The passenger address allows all crew members to make announcements to passengers in thecabin through loudspeakers. It can be operated from the cockpit (with ACP or handset) or from thecabin (attendant stations).CONTROLS AND INDICATORS

(1) PA transmission keyPressed and held : The flight crew may use a boom, mask, or hand mike to make an

announcement.Three green lines come on.

Note: The flight crew may use a cockpit handset to make PA announcements withoutaction on the ACPs.

(2) PA reception knobPressed and released(knob out)

: The message goes to the loudspeakers, and the integral whitelight comes on.The flight crew can turn the knob to adjust the volume.

Pressed (knob in) : The PA reception to the loudspeakers is disconnected.The white light goes out.


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - PASSENGER ADDRESS


COCKPIT HANDSETThe cockpit handset at the bottom of the pedestal is for PA announcements.

PA FROM COCKPITPA TRANSMISSION

KEY ON ACPPA RECEPTIONKNOB ON ACP


PUSH TO TALKON HANDSET

BOOMSETOR

OXYGENMASK

PRESSED OUT

HANDMIKE PRESSED OUT PRESSEDHANDSET PRESSED


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - EMER EVAC


EMER EVACIdent.: DSC-23-20-60-00000805.0001001 / 19 DEC 12


(1) COMMAND pb (guarded)ON : In the cockpit : ‐ EVAC light flashes red.

‐ Horn sounds.In the cabin : ‐ EVAC lights flash at FWD and AFT attendant panels.

‐ Evacuation tone sounds.OFF: The alert is stopped.The EVAC light flashes red when the alert is activated.

(2) HORN SHUT OFF pbPressing this button silences the cockpit horn.

(3) CAPT and PURS/CAPT swCAPT and PURS : The alert may either be activated from the cockpit or the cabin.CAPT : The alert may only be activated from the cockpit.

If one of the cabin CMD pb is pressed, only the cockpit horn sounds for3 s.

(4) CMD pbPressing this button activates the alert, if the cockpit switch is at the CAPT & PURS position.Pressing it again stops the alert.

(5) RESET pbPressing this button silences the EVAC tone.


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - EMER EVAC

82U A318/A319/A320/A321 FLEET DSC-23-20-60 P 2/2FCOM ← A to B 06 MAR 14

(6) EVAC lightThis light flashes when the alert is activated.

PURSER STATIONIdent.: DSC-23-20-60-00000808.0001001 / 19 DEC 12Applicable to: ALL


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - ELECTRICAL SUPPLY

82U A318/A319/A320/A321 FLEET DSC-23-20-70 P 1/2FCOM A 06 MAR 14

BUS EQUIPMENT LISTIdent.: DSC-23-20-70-00000809.0001001 / 15 FEB 11

1 Applicable to: MSN 0112-0189

NORM EMER ELEC

AC DC ACESS

DCESS HOT

CIDS1 GND/FLT XCIDS2 GND/FLT XCABIN INTERCOM

DATA SYS DEU (A/B) GND/FLT X

BUS EQUIPMENT LISTIdent.: DSC-23-20-70-00000809.0002001 / 15 FEB 11Applicable to: MSN 0342

NORM EMER ELEC

AC DC ACESS

DCESS HOT

CIDS1 GND/FLT X HOT2CIDS2 GND/FLT X HOT2CABIN INTERCOM

DATA SYS DEU (A/B) GND/FLT X


OPERATING MANUAL


INTERCOMMUNICATION SYSTEMS - ELECTRICAL SUPPLY


82U A318/A319/A320/A321 FLEET DSC-23-20-70 P 2/2FCOM 06 MAR 14


OPERATING MANUAL


COCKPIT VOICE RECORDER - DESCRIPTION


DESCRIPTIONIdent.: DSC-23-30-10-00000812.0001001 / 13 FEB 14Applicable to: MSN 0112

1The cockpit voice recorder (CVR) records :‐ direct conversations between crew members in the cockpit‐ all aural warnings sounded in the cockpit‐ audio communications received and transmitted‐ intercommunications conversations between crew members‐ announcements transmitted over the passenger address system, if PA reception is selected on the

third audio control panel.Only the last 2 h of recording are retained.The CVR system consists of :‐ a remote microphone behind the overhead panel‐ a crashproof four-track recorder, equipped with an underwater locating beacon, in the aft section

of the aircraft‐ a control panel on the overhead panel.It is energized automatically :‐ on the ground during the first 5 min after the aircraft electrical network is energized‐ on the ground with one engine running‐ in flightOn the ground, it is stopped automatically 5 min after the last engine shutdown provided the CVRjack is not used.On the ground, the crew can energize the CVR manually by pressing the GND CTL pushbutton.

DESCRIPTION

2 Ident.: DSC-23-30-10-00000812.0002001 / 13 FEB 14Applicable to: MSN 0189-0342

The cockpit voice recorder (CVR) records :‐ direct conversations between crew members in the cockpit‐ all aural warnings sounded in the cockpit‐ audio communications received and transmitted‐ intercommunications conversations between crew members‐ announcements transmitted over the passenger address system, if PA reception is selected on the

third audio control panel.Only the last 2 h of recording are retained.


OPERATING MANUAL


COCKPIT VOICE RECORDER - DESCRIPTION

82U A318/A319/A320/A321 FLEET DSC-23-30-10 P 2/2FCOM ← A 06 MAR 14

The CVR system consists of :‐ a remote microphone behind the overhead panel‐ a “hot mike” function, which records the crew members voice directly from their microphone, even

if the push to talk switch is not activated.‐ a crashproof four-track recorder, equipped with an underwater locating beacon, in the aft section

of the aircraft‐ a control panel on the overhead panel.It is energized automatically :‐ on the ground during the first 5 min after the aircraft electrical network is energized‐ on the ground with one engine running‐ in flightOn the ground, it is stopped automatically 5 min after the last engine shutdown provided the CVRjack is not used.On the ground, the crew can energize the CVR manually by pressing the GND CTL pushbutton.


OPERATING MANUAL


COCKPIT VOICE RECORDER - CONTROLSAND INDICATORS ON OVERHEAD PANEL


CONTROLS AND INDICATORS ON OVERHEAD PANELIdent.: DSC-23-30-20-00000816.0001001 / 06 FEB 14Applicable to: ALL

(1) GND CTL switch (spring-loaded)ON : The CVR, DFDR, and QAR are on.

The ON light comes on blue.AUTO : The CVR, DFDR, and QAR are on, according to the logic. (Refer to

DSC-23-30-10 DESCRIPTION).

(2) CVR ERASE pushbuttonPressed for2 s

: This completely erases the tape, if :‐ The aircraft is on the ground, and‐ The parking brake is on.

(3) CVR TEST pushbuttonPressed andheld

: This activates the test, if the CVR is on (the GND CTL pushbutton pressed,or during the first 5 min after energization of the aircraft electrical network),and the parking brake is on.Refer to PRO-NOR-SOP-06 Overhead Panel - RCDR for additionalinformation.


OPERATING MANUAL


COCKPIT VOICE RECORDER - CONTROLSAND INDICATORS ON OVERHEAD PANEL




OPERATING MANUAL


COCKPIT VOICE RECORDER - ELECTRICAL SUPPLY


BUS EQUIPMENT LISTIdent.: DSC-23-30-30-00000817.0001001 / 16 MAR 11Applicable to: ALL

NORM EMER ELEC

AC DC ACESS

DCESS HOT

CVR CTL SHEDCOCKPIT VOICERECORDER CVR SHED


OPERATING MANUAL


COCKPIT VOICE RECORDER - ELECTRICAL SUPPLY




OPERATING MANUAL


EMERGENCY LOCATOR TRANSMITTER - CONTROLS AND INDICATORS


CONTROLS AND INDICATORSIdent.: DSC-23-35-10-00000899.0002001 / 19 DEC 12Applicable to: MSN 0189

(1) ELT swThe guard keeps this switch in the ARMED position.ON : The Emergency Locator Transmitter (ELT) transmits an emergency signal.ARMED : In the case of impact, the ELT transmits an emergency signal (on 121.5, 243

and 406.025 MHz).

(2) ON and ELT lightThese lights come on amber either when the emergency signal is transmitted, or during ELTautotest.

(3) TEST/RESET pbPressing this pushbutton starts the ELT auto test.


OPERATING MANUAL


EMERGENCY LOCATOR TRANSMITTER - CONTROLS AND INDICATORS


Note: If the ELT is unduly triggered in ARMED mode (by an external impact, hard landing,etc.), select the TEST/RESET position to reset the ELT and stop signal transmission.


OPERATING MANUAL


ACARS - GENERAL

82U A318/A319/A320/A321 FLEET DSC-23-40-10 P 1/2FCOM A to B 06 MAR 14

INTRODUCTIONIdent.: DSC-23-40-10-00000915.0001001 / 15 FEB 11


The Aircraft Communication Addressing and Reporting System (ACARS) allows the direct exchangeof data between aircraft and airline ground computers via VHF 3.Aircraft to ground messages (downlink) comprise operational, maintenance, monitoring, performanceand cabin data.Ground to aircraft messages (uplink) contain crew information (wind for example), or might requestdata transmissions which are either sent automatically or by crew action.Automatic report downlinks are carried out by ACARS Management Unit [MU), which is programmedaccording to airline needs (Buyer Furnishing Equipment).Due to highly customized programming, the ACARS functions may vary from one airline to anotherand are therefore, not described in detail.

SYSTEM ARCHITECTUREIdent.: DSC-23-40-10-00000916.0001001 / 01 OCT 12


The ACARS system consists of a Management Unit (MU), connected to the following elements:


OPERATING MANUAL


ACARS - GENERAL




OPERATING MANUAL


ACARS - COCKPIT ARRANGEMENT


COCKPIT ARRANGEMENTIdent.: DSC-23-40-20-00000931.0001001 / 19 DEC 12


ACARS operation is performed through the already available cockpit equipment:‐ ECAM for operational indications.‐ MCDU for control of ACARS related functions.‐ PRINTER for hard-copies.The connector for portable data loader is in the avionics bay.


OPERATING MANUAL


ACARS - COCKPIT ARRANGEMENT




OPERATING MANUAL


ACARS - OPERATIONS MODES


MANUAL ACCESS TO ACARS FUNCTIONSIdent.: DSC-23-40-30-00000950.0001001 / 17 MAR 11


ACARS functions are manually selected through the MCDU. They are obtained for the FMGC,CFDS or AIDS by selecting the corresponding key. Cabin management functions (if available) areaccessible through the cabin installed system.

Pressing a system key will display the system pages, as defined in the airline customized MUprogramming.


OPERATING MANUAL


ACARS - OPERATIONS MODES

82U A318/A319/A320/A321 FLEET DSC-23-40-30 P 2/2FCOM B 06 MAR 14

AUTOMATIC ACCESS TO ACARS FUNCTIONSIdent.: DSC-23-40-30-00000960.0001001 / 15 FEB 11


Automatic data transmission can be initiated by the MU, the aircraft systems' programming, oran uplink message. There is no cockpit indication and no crew action is required. It is a dialoguebetween ground and aircraft computers.


OPERATING MANUAL


ACARS - ACARS FUNCTIONS


GENERALIdent.: DSC-23-40-40-00000979.0001001 / 15 FEB 11


Data and reports of a particular system are available through Airbus-defined interfaces (SellerFurnishing Equipment).


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 2/10FCOM B → 06 MAR 14

FMSIdent.: DSC-23-40-40-00000980.0001001 / 19 DEC 12


(1) This key selects the related system.

(2) This key gives access to TO data (Uplink only).

(3) This key gives access to wind data (F-PLN page).


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 3/10FCOM ← B to E 06 MAR 14

(4) This key gives access to F-PLN initialization and wind data (Uplink only).

(5) This key gives access to pre and post flight reports, and the ACARS print/program (downlinkonly).For operations (Refer to DSC-22_20 Auto Flight - Flight Management / 70 AOC Functions).

ACARSIdent.: DSC-23-40-40-00000976.0001001 / 15 FEB 11


The ACARS key displays airline-defined functions (Example : Message transmissions, and eventtimes).

CFDSIdent.: DSC-23-40-40-00000977.0001001 / 15 FEB 11


(Refer to DSC-45-20 Maintenance Menu)The CMS ACARS interface permits to downlink the following data:‐ Post flight report (on ground), or current flight report (in flight), which concerns:

• All failure messages, detected by BITE;• The warnings displayed to the crew during the last or current flight leg.Reports can be downlinked, upon crew or ACARS MU request.

‐ Avionics data, which concerns the individual system BITE data (manual downlink only).‐ Failure messages and warnings (broadcast data transmitted in real-time to the MU).‐ Class 3 reports (on ground) containing all Class 3 failures, detected during the last flight leg. The

report can be downlinked, upon crew or ACARS MU request.

AIDSIdent.: DSC-23-40-40-00000978.0001001 / 15 FEB 11


The AIDS ACARS interface transmits to the ACARS MU the data for the following applications:‐ Aircraft Performance Monitoring (APM),‐ Engine Condition Monitoring (ECM),‐ APU Health Monitoring (AHM).Any of the AIDS DMU reports can be downlinked (transmitted to the MU):‐ Manually on the ground, or in flight, upon crew request,‐ Automatically in real-time,‐ Upon ACARS MU (ground or automatic) request.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 4/10FCOM F 06 MAR 14

AUTOMATIC DOWNLINK OF REPORTSIdent.: DSC-23-40-40-00000972.0001001 / 15 FEB 11


ACARS provides the automatic downlink of reports. Each report, generated by a peripheral system,may be downlinked depending on each airline’s MU programming.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 5/10FCOM G → 06 MAR 14

UPLINK MESSAGESIdent.: DSC-23-40-40-00000973.0001001 / 14 MAY 12


There are two types of uplink messages :• Messages not indicated to the crew :

No indication is given to the crew, neither for uplink messages nor for downlink answers.It is a dialogue between ground and aircraft computers.

• Messages indicated to the crew by :‐ The “ACARS MSG” advisory (pulsing green) on ECAM Memo

Note: A steady green “ACARS STBY” advisory is displayed, in case of ACARS'communications loss between the aircraft and ground.

‐ A message on the MCDU (ACARS MSG WAITING, for example) or the MCDU MENU lightcomes on, if the MCDU is not in the mode where uplink messages can be displayed in order toselect the correct mode (FMGC, ACARS, AIDS, CFDS)

‐ Hard copy from the cockpit printer, depending on the MU programming.Example of uplink message indications with MCDU in FMS mode :


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 6/10FCOM ← G 06 MAR 14


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 7/10FCOM H → 06 MAR 14

VOICE/ACARS TRANSFER ON VHF 3Ident.: DSC-23-40-40-00000974.0001001 / 19 DEC 12


VHF 3 can be used in VOICE mode, in case of a :‐ VHF 1, or VHF 2, failure‐ ACARS CALL

The green pulsing “ACARS CALL” advisory indicates that a message requesting a voiceconversation has been received from the ground.The green “VHF 3: VOICE” advisory indicates that the VHF 3 transceiver operates in voice mode,therefore the ACARS communications are interrupted.Depending on MU programming, the ACARS frequency may be either automatically tuned by theACARS MU or manually tuned through the RMPIn this case, the ACARS/VOICE transfer is made directly on any of RMPs (without using MCDU).


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 8/10FCOM ← H 06 MAR 14

It is possible to return to ACARS mode by pressing again the RMP’s transfer key again.


OPERATING MANUAL



82U A318/A319/A320/A321 FLEET DSC-23-40-40 P 9/10FCOM I 06 MAR 14

WORLD MAP ACARS FREQUENCIESIdent.: DSC-23-40-40-00000975.0001001 / 15 FEB 11


The table below defines the world zone abbreviations, indicates their associated Service Provider,MCDU label, and ACARS frequency.ABBREVIATION SERVICE PROVIDER MCDU LABEL FREQUENCY Family

SP SITA PACIFIC SIT-PAC 131.550 MHz SITA

SN SITA NORTHAMERICA SIT-NAM 136.850 MHz SITA

SL SITA LATIN AMERICA SIT-LAM 131.725 MHz SITASE SITA EUROPE SIT-E/A 131.725 MHz SITADE DEPV BRAZIL DEPV 131.550 MHz SITAAV AVICOM AVICOM 131.450 MHz SITAAM ARINC AMERICA ARI-AM 131.550 MHz ARINCAE ARINC EUROPE ARI-EUR 136.925 MHz ARINCAF ARINC AFRICA ARI-AFR 126.900 MHz ARINCAK ARINC KOREA ARI-KOR 131.725 MHz ARINCAS ARINC ASIA ARI-ASI 131.450 MHz ARINC


OPERATING MANUAL






OPERATING MANUAL


ACARS - ELECTRICAL SUPPLY


BUS EQUIPMENT LISTIdent.: DSC-23-40-50-00000996.0001001 / 15 FEB 11Applicable to: ALL

NORM EMER ELEC

AC DC ACESS

DCESS HOT

ACARS AC1


OPERATING MANUAL


ACARS - ELECTRICAL SUPPLY




OPERATING MANUAL


SATCOM - ELECTRICAL SUPPLY


BUS EQUIPMENT LISTIdent.: DSC-23-46-30-00013271.0001001 / 18 MAR 11Applicable to: ALL

NORM EMER ELEC

AC DC ACESS

DCESS HOT

SATCOM AC1


OPERATING MANUAL


SATCOM - ELECTRICAL SUPPLY




OPERATING MANUAL


WARNINGS AND CAUTIONS

82U A318/A319/A320/A321 FLEET DSC-23-50 P 1/2FCOM A → 06 MAR 14

WARNINGS AND CAUTIONSIdent.: DSC-23-50-00001119.0003001 / 15 FEB 11

1 Applicable to: MSN 0112-0189

E/WD: FAILURE TITLEconditions

AURALWARNING

MASTERLIGHT

SD PAGECALLED

LOCALWARNING

FLTPHASEINHIB

CIDS 1 + 2 FAULTVHF 1(2)(3) EMITTINGHF 1(2) EMITTINGTransmitter emitting more than 60 s

SINGLECHIME

MASTERCAUTION

SATCOM FAULTACARS FAULTHF 1(2) DATA FAULTVHF 3 DATA FAULTSATCOM DATA FAULT

NIL NIL

NIL NIL 3, 4,5, 7, 8

MEMO DISPLAYThis display shows “AUDIO 3 XFRD” in green, if the AUDIO SWITCHING selector is not onNORM.ACARS , the display shows:‐ "ACARS CALL" in green, pulsing, if ACARS has received a message from the ground

requesting a voice communication.‐ "VHF 3: VOICE" in green, if VHF 3 is operating in voice mode and ACARS communication is

interrupted.‐ "ACARS MSG" in green, pulsing, if ACARS has received a message from the ground‐ ACARS STBY in green, if ACARS communications between the aircraft and the ground are lost.SATCOM , the display shows "SATCOM ALERT" in green, when a message with a prioritylevel below 4 is received from the ground.


OPERATING MANUAL


WARNINGS AND CAUTIONS

82U A318/A319/A320/A321 FLEET DSC-23-50 P 2/2FCOM ← A 06 MAR 14

HF and ATSU , the display shows “HF VOICE”, pulsing in green for 10 s and then steady,when all the HF radios are in voice mode.

WARNINGS AND CAUTIONSIdent.: DSC-23-50-00001119.0001001 / 15 FEB 11Applicable to: MSN 0342

E/WD: FAILURE TITLEconditions

AURALWARNING

MASTERLIGHT

SD PAGECALLED

LOCALWARNING

FLTPHASEINHIB

CIDS 1 + 2 FAULTVHF 1(2)(3) EMITTINGHF 1(2) EMITTINGTransmitter emitting more than 60 s

SINGLECHIME

MASTERCAUTION

ACARS FAULT NIL NIL

NIL NIL 3, 4,5, 7, 8

MEMO DISPLAYThis display shows AUDIO 3 XFRD in green if the AUDIO SWITCHING rotary selector is not onNORM.In addition, ACARS the display shows:‐ ACARS CALL pulsing in green, if ACARS has received a message from the ground requesting

a voice communication‐ VHF 3: VOICE in green, if VHF 3 is operating in voice mode and ACARS communication is

interrupted‐ ACARS MSG in green, pulsing, if ACARS has received a message from the ground‐ ACARS STBY in green if ACARS communications between the aircraft and the ground are lost

aircraft systemscaacongo.com/corporate/co_at_fcom/pdf_n_fcom_82u_tf_n_eu... · 2014. 3. 6. ·...

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