Avionics Systems Day 6
Transponder

 Used to help ATC identify aircraft
  operating in controlled airspace
 Transponders operate in the same
  frequency range as ATC radar
 Required to be inspected & tested every
  24 calendar months
The control head of an ATC transponder
Transponder

 When ATC radar interrogates the
  aircraft, the transponder automatically
  responds by sending a four digit
  identification code
Transponder

 The four digit code is registered in the
  ATC computer along with the aircraft
  flight plan
      The controller will see the aircraft
       registration number and four digit code on
       the radar screen
Transponder Functions

 Identification (ident) – simply the four
  digit coded reply
 Altitude reporting – transponder is
  coupled to an encoding altimeter which
  sends the aircraft altitude with the reply
 Collision avoidance – monitors other
  aircraft transponders in the area & will
  determine if a collision is possible
Transponder Operation

 Transponders operate in three modes
 Mode A
     Identification only
 Mode C
     Identification & Altitude reporting (required
      in some airspace)
 Mode S
     Identification, Altitude reporting, & collision
      avoidance
TCAS

 Traffic alerting & Collision Avoidance
  System
     Used with mode S transponders
     Works independently of ground stations
     If a collision course is detected the system
      will display appropriate directions to the
      pilot to prevent the collision
ELT

 Emergency Locator Transmitter
 Battery powered transmitter required on
  all general aviation aircraft
 Produces a locator signal which can be
  used by search & rescue to locate
  downed aircraft
ELT

 Inertia switch activated
      6 G forward
      Also has a manual switch on the ELT, &
       usually in the cockpit
 Frequencies
      121.5 & 243 MHz
      International distress frequencies
ELT

 100 Mile range at 10,000 ft
 48 Hour capacity
 Installed in the tail of the aircraft
      Provides protection from crash damage
       when placed as far aft as possible
ELT

 Must be tested on a regular basis
     Every 12 calendar months
 The test must be performed within the
  first 5 minutes of any hour
     Log book entry should be made after test
ELT Testing

 Tune radio to 121.5
 With the ELT disconnected from the
  antenna turn on the ELT using the switch
     You should hear the siren
 Turn switch to arm position & shake
     You should hear the siren again
 Turn off ELT using the switch
     Do not let the ELT operate for more than 3
      seconds at a time
ELT Battery Check

 Battery must be replaced at the time of
  the expiration date found on the battery
  case
 Or if more than one hour has been
  depleted from the battery
     Check maintenance records in the aircraft
      logbooks
EPIRB

 Emergency & Position Indicating Radio
  Beacon
 New replacement for the ELT
 Will be required by Feb. 2009
 5 Watts of power not ½ watt
 Digital signal
     Identifies owner and aircraft
        Fewer false alarms
        Must be registered with the FAA
EPIRB

 Picked up by satellites
 Can be interfaced with aircraft GPS
     Pinpoint accuracy .031 kilometers
     Old ELT 1260 sq kilometers
 More rapid response time for rescuers
FDR

 Flight Data Recorder
 Device which monitors & records specific
  flight operation parameters for analysis
  after an accident
     The “BLACK BOX”
       Which   is actually bright orange
FDR

 Required on all commercial airliners
  since 1958
 Records the last 25 hours of flight
 Located in the aircraft tail
 Fire & “G” resistant
 Transmits a locator signal so it can be
  found in the wreckage
FDR

 Parameters
     Altitude & Airspeed
     Attitude & Direction
     Vertical acceleration
     Landing gear position
     Flight control position
     Engine power
     Greenwich mean time “ZULU time”
CVR

 Cockpit Voice Recorder
     Records the last 30 minutes of the flight
      deck voice communications
     Microphone in the cockpit
     Recorder in the tail
     Crush & fire resistant
     Transmits a locator signal so it can be
      found
Intercom System

 Cabin interphone system
 Amplified audio signals allow
  communication between members of the
  flight crew or with the passengers
 Public address system
Intercom System

 Service Interphone System
     Allows communication between flight crew
      & ground personnel or mechanics
The End!
(for today)


Day 6

  • 1.
  • 2.
    Transponder  Used tohelp ATC identify aircraft operating in controlled airspace  Transponders operate in the same frequency range as ATC radar  Required to be inspected & tested every 24 calendar months
  • 3.
    The control headof an ATC transponder
  • 4.
    Transponder  When ATCradar interrogates the aircraft, the transponder automatically responds by sending a four digit identification code
  • 5.
    Transponder  The fourdigit code is registered in the ATC computer along with the aircraft flight plan  The controller will see the aircraft registration number and four digit code on the radar screen
  • 6.
    Transponder Functions  Identification(ident) – simply the four digit coded reply  Altitude reporting – transponder is coupled to an encoding altimeter which sends the aircraft altitude with the reply  Collision avoidance – monitors other aircraft transponders in the area & will determine if a collision is possible
  • 7.
    Transponder Operation  Transpondersoperate in three modes  Mode A  Identification only  Mode C  Identification & Altitude reporting (required in some airspace)  Mode S  Identification, Altitude reporting, & collision avoidance
  • 8.
    TCAS  Traffic alerting& Collision Avoidance System  Used with mode S transponders  Works independently of ground stations  If a collision course is detected the system will display appropriate directions to the pilot to prevent the collision
  • 10.
    ELT  Emergency LocatorTransmitter  Battery powered transmitter required on all general aviation aircraft  Produces a locator signal which can be used by search & rescue to locate downed aircraft
  • 12.
    ELT  Inertia switchactivated  6 G forward  Also has a manual switch on the ELT, & usually in the cockpit  Frequencies  121.5 & 243 MHz  International distress frequencies
  • 13.
    ELT  100 Milerange at 10,000 ft  48 Hour capacity  Installed in the tail of the aircraft  Provides protection from crash damage when placed as far aft as possible
  • 14.
    ELT  Must betested on a regular basis  Every 12 calendar months  The test must be performed within the first 5 minutes of any hour  Log book entry should be made after test
  • 15.
    ELT Testing  Tuneradio to 121.5  With the ELT disconnected from the antenna turn on the ELT using the switch  You should hear the siren  Turn switch to arm position & shake  You should hear the siren again  Turn off ELT using the switch  Do not let the ELT operate for more than 3 seconds at a time
  • 16.
    ELT Battery Check Battery must be replaced at the time of the expiration date found on the battery case  Or if more than one hour has been depleted from the battery  Check maintenance records in the aircraft logbooks
  • 17.
    EPIRB  Emergency &Position Indicating Radio Beacon  New replacement for the ELT  Will be required by Feb. 2009  5 Watts of power not ½ watt  Digital signal  Identifies owner and aircraft  Fewer false alarms  Must be registered with the FAA
  • 19.
    EPIRB  Picked upby satellites  Can be interfaced with aircraft GPS  Pinpoint accuracy .031 kilometers  Old ELT 1260 sq kilometers  More rapid response time for rescuers
  • 21.
    FDR  Flight DataRecorder  Device which monitors & records specific flight operation parameters for analysis after an accident  The “BLACK BOX”  Which is actually bright orange
  • 22.
    FDR  Required onall commercial airliners since 1958  Records the last 25 hours of flight  Located in the aircraft tail  Fire & “G” resistant  Transmits a locator signal so it can be found in the wreckage
  • 23.
    FDR  Parameters  Altitude & Airspeed  Attitude & Direction  Vertical acceleration  Landing gear position  Flight control position  Engine power  Greenwich mean time “ZULU time”
  • 24.
    CVR  Cockpit VoiceRecorder  Records the last 30 minutes of the flight deck voice communications  Microphone in the cockpit  Recorder in the tail  Crush & fire resistant  Transmits a locator signal so it can be found
  • 25.
    Intercom System  Cabininterphone system  Amplified audio signals allow communication between members of the flight crew or with the passengers  Public address system
  • 28.
    Intercom System  ServiceInterphone System  Allows communication between flight crew & ground personnel or mechanics
  • 31.