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ATA 23 Communication

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The communication system allows crew members to communicate with each other, ... Coded tone signals are received with incoming HF or VHF transmissions and, when ... – PowerPoint PPT presentation

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Title: ATA 23 Communication


1
ATA 23 Communication
  • The communication system allows crew members to
    communicate with each other, from the cockpit and
    from the ground.
  • They can also communicate with the passengers,
    other aircraft and the ground stations.
  • Speech Communication Systems (23-10)
  • The speech communications system controls the VHF
    and the HF radios. The Radio Control Panels (RCP)
    control and allow for selection of specified
    frequencies and the mode (AM, SSB) for the HF
    system.

2
ATA 23 Communication
  • High Frequency (HF) Communication System (23-11)

3
ATA 23 Communication
  • High Frequency (HF) Communication System (23-11)
  • Each HF communication system provides amplitude
    modulated (AM) and single-side band (SSB) voice
    communications between the airplane and ground
    stations or other airplanes. Propagation
    characteristics of the HF system are suitable for
    long distance communications.
  • Communications take place in the 2 to 30 MHz
    frequency range.
  • Two independent HF communication systems provide
    long-range air-to-ground and air-to-air two-way
    voice communications.
  • The left and right HF communication systems
    operate in the 2.000 to 29.999 MHz frequency
    range on 28,000 channels spaced at 1 KHz in the
    AM (Amplitude Modulated) or USB (Upper Sideband)
    mode, as selected.

4
ATA 23 Communication
  • Very High Frequency (VHF) Communication System
    (23-12)

5
ATA 23 Communication
  • Very High Frequency (VHF) Communication System
    (23-12)
  • Three VHF communications systems are installed on
    the airplane. The systems provide short-range
    line-of-sight voice.
  • Each VHF communications system provides
    amplitude-modulated (AM) voice communications
    with ground stations or other airplanes. The
    systems operate in the 118.00-MHz to 136.975-MHz
    frequency range in 25-kHz increments, or in the
    118.00-MHz to 136.990-MHz frequency range in
    8.33-kHz increments.

6
ATA 23 Communication
  • Airborne Cabin Telephone (23-19)
  • The airborne cabin telephone system allows
    passengers and cabin crew to telephone anywhere
    in the world using international direct dialing
    (IDD).
  • Emergency Locator Transmitter System (ELT)
    (23-24)
  • The emergency locator transmitter (ELT) system
    provides an emergency locator signal to aid in
    search and rescue operations. The ELT transmits
    on international distress frequencies 121.5,
    243.0, and 406.025 MHz.

7
ATA 23 Communication
  • Satellite Communication System (23-25)

8
ATA 23 Communication
  • Satellite Communication System (23-25)
  • The satellite communication (SATCOM) system
    provides voice and data communications capability
    for the flight crew and also provide a
    communication link for passenger voice and data
    communications. The SATCOM system supplies
    full-duplex telephone quality voice
    communications.
  • The SATCOM system operates in the L-band
    frequency range. The uplink frequency
    (satellite-to-airplane) is 1530 to 1559 MHz. The
    downlink frequency (airplane-to-satellite) is
    1626.5 to 1660.5 MHz.
  • The SATCOM system supplies voice/data signals
    over longer distances than the VHF communication
    system. The SATCOM system provides more reliable
    communications over oceanic regions than the HF
    communication system.

9
ATA 23 Communication
  • Satellite Communication System (23-25)

10
ATA 23 Communication
  • Aircraft Communications Addressing and Reporting
    System (23-27)
  • The aircraft communications addressing and
    reporting system (ACARS) provides a ground to air
    and air to ground airborne communications data
    link. The system receives digital data and
    processes it for display to the flight crew and
    formats digital data of airplane parameters and
    operations for transmission to ground stations.
    Messages are coded to identify a specific
    airplane.

11
ATA 23 Communication
  • Aircraft Communications Addressing and Reporting
    System (23-27)
  • The MU encodes the digital data for transmission
    as a series of 1200 Hz and 2400 Hz tones at 2400
    baud (future ACARS systems may operate with
    2400/4800 Hz at 4800 baud).
  • A 1200 Hz tone indicates a bit change from the
    previous bit (0 to 1 or 1 to 0) while a 2400 Hz
    tone indicates no bit change (0 to 0 or 1 to 1).

12
ATA 23 Communication
  • Selective Calling (SELCAL) System (23-28)
  • The SELCAL system allows a ground operator to
    alert a specific airplane. Coded tone signals are
    received with incoming HF or VHF transmissions
    and, when decoded by the designated airplane,
    signal the flight crew of an incoming call.
  • The airplane has its unique four tone code
    resolved with a sixteen bit binary word. Four
    bits of the word determine each tone. Airplane
    wiring is installed to implement the unique 16
    bits for the airplane.

13
ATA 23 Communication
  • Passenger Address and Entertainment (23-30)
  • The Advanced Cabin Entertainment/Service System
    or the Cabin Services System includes these
    systems
  • Passenger Address System (23-31)
  • Video Passenger Entertainment System (23-32)
  • Passenger Service System (23-33)
  • Audio Passenger Entertainment System (23-34)
  • Passenger Flight Information Display System
    (23-38)

14
ATA 23 Communication
  • Service Interphone System (23-41)
  • The service interphone system allows ground
    personnel to communicate with each other from
    various service stations around the airplane.
    They plug a boom/mic headset into jacks located
    at various points. Communication with the Flight
    Deck is possible by paralleling the service
    interphone system with the flight interphone
    system.

15
ATA 23 Communication
  • Cabin Interphone System (23-42)
  • The cabin interphone system allows communication
    from the flight crew to the attendants and
    attendants to flight crew. Microphones/handsets
    in the passenger cabin are located in convenient
    locations for the flight attendants.
  • Ground Crew Call system (23-43)
  • The ground crew call system allows personnel in
    the flight compartment and servicing personnel on
    the ground outside the airplane to gain each
    others attention. They can then establish
    communications with the service interphone and
    the flight interphone systems.

16
ATA 23 Communication
  • Flight Interphone system (23-51)
  • The flight interphone system interfaces with the
    communication radios and allows ground to
    airplane communication to occur. All push-to-talk
    (PTT) microphones, headsets and the oxygen mask
    microphones are part of the flight interphone
    system. This system also interfaces with most of
    the other chapter 23 cabin and crew communication
    systems.
  • Various navigation systems interface with the
    flight interphone system. Included are the
    VOR/ILS, Marker Beacon, DME and ADF. These
    systems provide monitoring signals to the flight
    crew on the headsets or on the flight interphone
    speakers.

17
ATA 23 Communication
  • Static Dischargers (23-61)
  • Static dischargers eliminate radio receiver
    interference which caused by a corona discharge
    emitted from the airplane surfaces as a result of
    precipitation static and engine charging by
    discharging static from the fuselage. This is
    done along the trailing edges of the wings, the
    horizontal stabilizer and the vertical
    stabilizer. This limits the interference that can
    be induced in the radio transceivers.

18
ATA 23 Communication
  • Static Dischargers (23-61)

19
ATA 23 Communication
  • Voice Recorder System CVR(23-71)
  • The voice recorder records the flight crew
    communications and conversation for a maximum of
    30 minutes or 120 minutes. Inputs one through
    three are from the flight crew station
    microphones to the Audio Control Panels (23-51)
    and then to the Audio Management Unit.
  • Input four is from the Remote Monitoring
    microphone in the flight deck overhead. This
    input sends all conversations in the flight
    compartment to the voice recorder. The voice
    recorder data may be erased when the airplane has
    landed and the parking brake is set.
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