CL_604-COMMUNICATIONS挑战者604通讯

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CL_604-COMMUNICATIONS

 

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Table of Contents
For Training Purposes Only
Jan 04
6-i
P I LOT T R A I N I N G GU I D E COMMUNICATIONS
Introduction .........................................................................................................................6-1
Audio Integrating System....................................................................................................6-2
Description ....................................................................................................................6-2
Components and Operation..........................................................................................6-2
Flight Crew Jack Panels..........................................................................................6-2
Ground Crew Interphone-Jack Units.......................................................................6-2
Speakers .................................................................................................................6-2
Controls and Indicators .................................................................................................6-3
VHF Communication System..............................................................................................6-5
Description ....................................................................................................................6-5
Components and Operation..........................................................................................6-5
Transceivers............................................................................................................6-5
Antennas .................................................................................................................6-5
Integrated Avionics Processor System ...................................................................6-5
Controls and Indicators .................................................................................................6-7
HF Communication System ................................................................................................6-8
Description ....................................................................................................................6-8
Components and Operation..........................................................................................6-8
Transceivers............................................................................................................6-8
Antenna Coupler .....................................................................................................6-9
Antenna...................................................................................................................6-9
Selective Calling (SELCAL) ....................................................................................6-9
Controls and Indicators .................................................................................................6-9
Radio Tuning System........................................................................................................ 6-11
Description .................................................................................................................. 6-11
Components and Operation........................................................................................ 6-11
Controls and Indicators ............................................................................................... 6-11
Radio Tuning Unit (RTU)....................................................................................... 6-11
Reversionary/Inhibit Panel .................................................................................... 6-13
Operation .................................................................................................................... 6-14
Display Hierarchy .................................................................................................. 6-14
RTU Failure Indications......................................................................................... 6-19
Self-Test................................................................................................................ 6-19
Overtemperature ................................................................................................... 6-20
Readout................................................................................................................. 6-20
Cockpit Voice Recorder System ....................................................................................... 6-21
Description .................................................................................................................. 6-21
Recorder ............................................................................................................... 6-21
CVR Control Unit................................................................................................... 6-23
Microphone ........................................................................................................... 6-23
COMMUNICATIONS
6-ii For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
Controls and Indicators ............................................................................................... 6-23
Operation .................................................................................................................... 6-24
Test ....................................................................................................................... 6-24
Erase..................................................................................................................... 6-24
Flight Data Recorder System............................................................................................ 6-25
Description .................................................................................................................. 6-25
Components and Operation........................................................................................ 6-25
Recorder ............................................................................................................... 6-25
Controls and Indicators ............................................................................................... 6-27
FDR EVENT Switch .............................................................................................. 6-27
EICAS Messages........................................................................................................ 6-27
Static Dischargers............................................................................................................. 6-28
Description .................................................................................................................. 6-28
List of Figures
Graphic Title Figure
For Training Purposes Only
May 03
6-iii
P I LOT T R A I N I N G GU I D E COMMUNICATIONS
Audio Integrating System Components ..............................................................................6-1
Audio Control Panel ............................................................................................................6-2
VHF Communication System - Block Diagram ...................................................................6-3
HF Communication System - Block Diagram......................................................................6-4
Radio Tuning Unit ...............................................................................................................6-5
Reversionary/Inhibit Panel ..................................................................................................6-6
COM/NAV Selections..........................................................................................................6-7
COM 3 Selections ...............................................................................................................6-8
ADF, ATC and TCAS Selections ........................................................................................6-9
HF Selections.................................................................................................................... 6-10
RTU and COM/NAV Failure Indications............................................................................ 6-11
RTU TEMP Annunciation.................................................................................................. 6-12
CVR System .....................................................................................................................6-13
Cockpit Voice Recorder Panel .......................................................................................... 6-14
Flight Data Recorder System............................................................................................ 6-15
Static Dischargers Location .............................................................................................. 6-16
6-iv For Training Purposes Only
May 03
COMMUNICATIONS P I LOT T R A I N I N G GU I D E
Page Intentionally Left Blank
COMMUNICATIONS
For Training Purposes Only
May 03
6-1
P I LOT T R A I N I N G GU I D E
CHAPTER 6: COMMUNICATIONS Introduction
Communications is a function of the Challenger 604 fully integrated avionics system
and includes the following:
• Audio Integrating System
• VHF Communication System
• HF Communication System
• Radio Tuning System
• Cockpit Voice Recorder (CVR) System
• Flight Data Recorder (FDR) System
• Static Dischargers
COMMUNICATIONS
6-2 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
Audio Integrating System
Description
The audio integrating system provides an interface between crew microphones,
speakers, headphones, and the aircraft’s radio, warning and recording systems. The
audio integrating system also provides an interface between any or all flight crew and
ground crew stations.
Components and Operation
The audio integrating system consists of the following components:
• two flight crew jack panels
• three ground crew interphone units (jacks)
• two speakers
• two audio control panels
Flight Crew Jack Panels
Two flight crew jack panels (Pilot and Copilot) are located in the flight compartment.
Ground Crew Interphone-Jack Units
The three ground crew interphone-jack units are installed in the following locations:
• nosewheel well
• main avionics bay
• aft equipment compartment
Each assembly is a metal-case sealed unit which has one microphone jack and one
headphone jack. The microphone jacks in the nosewheel well and aft compartment are
deactivated in flight by the WOW switch.
Speakers
Two independent speakers are mounted in the roof of the flight compartment for the
pilot’s and copilot’s audio systems. The speakers allow audio monitoring without the
use of headphones.
COMMUNICATIONS
For Training Purposes Only
May 03
6-3
P I LOT T R A I N I N G GU I D E
Controls and Indicators
The audio control panels provide controls for selecting and controlling receiver audio
from the COM/NAV systems, and controls for connecting the microphone audio and
keying to the HF/VHF systems.
Audio Integrating System Components
Figure 6-1
HDPH
1 - VHF - 2
1 - DME - 2
1 - NAV - 2 1 - MKR - 2
1 - ADF - 2
R/T
I/C
VOICE
BOTH
SPKR MASK
BOOM
EMER
NORM
PA
VHF 3 1 - HF - 2 INT/SVC
Aft Equipment
Bay
Avionics
Bay
Nosewheel
Well
INTERPHONE
UNIT
Pilot PTT
Switch
JACK PANEL JACK PANEL
AUDIO CONTROL PANEL
Speaker Speaker
P604_06_001
HDPH MIC MIC
I/C
OFF
R/T
NOSE
DN
NOSE
UP
AP
SC
SYNC
I/C
OFF
R/T
NOSE
DN
NOSE
UP
AP
SC
SYNC
Copilot PTT
Switch
HDPH MIC
COMMUNICATIONS
6-4 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Audio Control Panel
Figure 6-2
Public Address (PA)
Flight deck to cabin
communication
1 - VHF - 2
1 - DME - 2
1 - NAV - 2 1 - MKR - 2
1 - ADF - 2
R/T
I/C
VOICE
BOTH
SPKR MASK
BOOM
EMER
NORM
PA
VHF 3 1 - HF - 2 INT/SVC
MIC Selector
Switch
Emergency/Normal
Switch
Norm
Emer
- Services as
selected
- RX/TX on
VHF, audio on nav
and aural warnings
boom and mask
microphone
VHF 1/2/3 COMM
Audio Controls
HF 1/2
Audio Controls
ADF 1/2
Audio Controls
Marker Beacon
Audio Controls
Radio Transmit (R/T)
Intercom (I/C) Switch
R/T
I/C
(Center Off -
Momentary at R/T)
- used for boom or
mask mic
- hot mic for boom
or mask through
intercom system
VOICE / BOTH
Switch
VOICE
BOTH
- voice
information only
- voice and cw
ident
Flight Compartment
Speaker (SPKR)
Audio Control
Mask/Boom Mic Switch
Mask
Boom
- oxygen mask
- boom microphone
DME 1/2
Audio Controls
NAV 1/2
Audio Controls
Intercom/Services
Audio Control
P604_06_002
For All
Audio Controls:
Push ON
Push OFF
Backlit when ON
Rotate for volume
COMMUNICATIONS
For Training Purposes Only
May 03
6-5
P I LOT T R A I N I N G GU I D E
VHF Communication System
Description
The VHF communication system consists of two very high frequency (VHF)
transceivers (VHF 1 and VHF 2) which operate independently. The VHF transceivers
provide amplitude modulated (AM) short-range voice communications in the
frequency range of 118.00 to 151.975 MHz, selectable in increments of 25 KHz/
8.33 KHz.
Components and Operation
The VHF communication system consists of the following components:
• two transceivers
• two antennas
Associated components:
• two radio tuning units (RTUs)
• two audio control panels
• one reversionary / inhibit panel
• integrated avionics processor system (IAPS)
Transceivers
Two VHF-422B transceivers contain the circuits required for transmission and
reception of radio signals, and processing of audio signals.
Antennas
There are two VHF antennas located as follows:
• VHF 1 antenna - upper side of the fuselage
• VHF 2 antenna - underside of the fuselage
Integrated Avionics Processor System
The integrated avionics processor system (IAPS) is a card cage assembly that
physically houses some avionic line replaceable units (LRUs). The IAPS reads several
avionic buses and distributes data to those LRUs requiring the information. Most
avionics data is processed by this unit.
COMMUNICATIONS
6-6 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
VHF Communication System - Block Diagram
Figure 6-3
AUDIO SYSTEM
VHF COMM
NO. 1
XCVR
VHF COMM
NO. 2
XCVR
IAPS
FMS FMS
DC
BATT
DC
BUS 2
A
C
C
A
B B
VHF 1
ANTENNA
118.00 - 151.975 MHz
VHF 2
ANTENNA
118.00 - 151.975 MHz
PILOT'S RTU
REVERSIONARY /
INHIBIT PANEL
COPILOT'S RTU
VHF 1
ONLY
P604_06_003
INHIBIT PUSH
1-RTU-2 FMS TUNE
1 2
AFCS
SEL
STBY
1 2
ATC
SEL
FMS
TUNE
INHIB
RTU 1
INHIB
RTU 2
INHIB
IDENT
DME-H
1/2
BRT
BRT
116.30
ACT PRE
111.35
NAV1
ACT PRE
121.90 149.10
COM1
373.0
ADF 1 TCAS
TA
ATC1
NEXT
PAGE 5540
TONE
REL
IDENT
DME-H
1/2
BRT
BRT
116.30
ACT PRE
111.35
NAV1
ACT PRE
121.90 149.10
COM2
373.0
ADF 1 TCAS
TA
ATC1
NEXT
PAGE 5540
TONE
REL
COMMUNICATIONS
For Training Purposes Only
May 03
6-7
P I LOT T R A I N I N G GU I D E
Controls and Indicators
The VHF communication system controls and indicators are described in the
following sections of this chapter:
• Audio control panel is described in the Audio Integrating System
• RTU and reversionary / inhibit panel are described in Radio Tuning System
The VHF transceiver is normally tuned by the on-side RTU. The VHF transceiver may
also be tuned by the cross-side RTU or by the FMS. The VHF transceiver supplies an
audio output to the audio system and a digital bus output to the IAPS. The data output
contains the communication frequency which is echoed back to the RTUs.
COMMUNICATIONS
6-8 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
HF Communication System
Description
The HF communication system consists of two high-frequency (HF) transceivers
(HF 1 and HF 2) which operate independently.
Communication range on HF frequencies is longer (potentially global), but less
reliable than on conventional VHF and UHF frequencies, and varies substantially with
factors such as operating frequency, season, time of day, atmospheric noise, and solar
activity.
Components and Operation
The HF communication system consists of the following components:
• two transceivers
• two couplers
• one antenna
Associated components:
• two radio tuning units (RTUs)
• two audio control panels
• one reversionary / inhibit panel
• one SELCAL decoder
• Integrated Avionics Processor System (IAPS)
Transceivers
The transceivers provide signal processing for transmission and reception. The unit
consists of a control module, RF/IF module, frequency synthesizer, frequency
standard, power supply/audio module and a power amplifier.
The transceivers provide amplitude modulated (AM) and single sideband (SSB) longrange
voice communications in the frequency range of 2 to 30 MHz, selectable in
increments of 100 Hz. Limited preset channel selection is also available and a
SELCAL (selective calling) feature is incorporated.
The two HF transceivers are identical and independent. They may be operated
simultaneously in receive mode but only one transceiver at a time can operate in
transmit mode. In a dual HF system configuration, antenna coupler No. 1 and antenna
coupler No. 2 exchange status (interlock) data to ensure that only one transceiver is
connected to the antenna for the transmit mode. When one transceiver is keyed to
transmit, the other transceiver is disconnected from the antenna and is unable to
receive or transmit. Frequency and mode selection is covered in the RTU section.
COMMUNICATIONS
For Training Purposes Only
May 03
6-9
P I LOT T R A I N I N G GU I D E
Antenna Coupler
The antenna coupler matches the impedance of the transceivers to the antenna as
different frequencies are selected and keyed.
Antenna
The antenna is an integral part of the leading edge of the vertical stabilizer. The
antenna is connected to the antenna coupler units via an RF strap.
High voltages and currents are present in this area during
transmissions.
Selective Calling (SELCAL)
Both HF transceivers are coupled to a SELCAL system, which monitors the selected
HF frequencies for the airplane’s unique SELCAL code without requiring the crew to
continuously monitor the HF audio. If the code is detected, an EICAS message and an
audio alert are triggered to advise the flight crew that a ground station is calling. The
EICAS message is reset when the appropriate HF transceiver is keyed to transmit.
Controls and Indicators
The HF communication system controls and indicators are described in the following
sections of this chapter:
• Audio control panel is described in Audio Integrating System
• RTU and reversionary / inhibit panel are described in Radio Tuning System
CAUTION
COMMUNICATIONS
6-10 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
HF Communication System - Block Diagram
Figure 6-4
AUDIO SYSTEM
SELCAL
IAPS
ANTENNA
COUPLER
#1
ANTENNA
COUPLER
#2
A
B
A
B
HF COMM
NO.1
XCVR
HF COMM
NO.2
XCVR
COPILOT'S RTU
REVERSIONARY /
INHIBIT PANEL
DC
UTILITY
BUS 2
DC
UTILITY
BUS 2
PILOT'S RTU
P604_06_004
DC
BUS 1
DC
BUS 1
INHIBIT PUSH
1-RTU-2 FMS TUNE
1 2
AFCS
SEL
STBY
1 2
ATC
SEL
FMS
TUNE
INHIB
RTU 1
INHIB
RTU 2
INHIB
IDENT
DME-H
1/2
BRT
BRT
116.30
ACT PRE
111.35
NAV1
ACT PRE
121.90 149.10
COM1
373.0
ADF 1 TCAS
TA
ATC1
NEXT
PAGE 5540
TONE
REL
IDENT
DME-H
1/2
BRT
BRT
116.30
ACT PRE
111.35
NAV1
ACT PRE
121.90 149.10
COM2
373.0
ADF 1 TCAS
TA
ATC1
NEXT
PAGE 5540
TONE
REL
COMMUNICATIONS
For Training Purposes Only
May 03
6-11
P I LOT T R A I N I N G GU I D E
Radio Tuning System
Description
The radio tuning system provides integrated control of airplane communication and
navigation radio subsystems. It supports full cross-side and reversionary tuning, thus
allowing single-point control of both on-side and cross-side radios from the pilot or
copilot positions.
Components and Operation
The radio tuning system consists of the following components:
• two radio tuning units (RTUs)
• one reversionary / inhibit panel
For the Flight Management System (FMS) tuning of communications, refer to Chapter
17 Navigation Systems under the heading “TUNE PAGE” in the FMS section.
Controls and Indicators
Radio Tuning Unit (RTU)
Line Select Keys
The RTU has eight panel-mounted line select keys adjacent to the display, four on the
left and four on the right of the display. Each key has a mechanical, momentary,
nonlatching action. The functions performed by these keys vary with each display
presented.
Dedicated Pushbuttons (IDENT, DME-H and 1/2)
There are three dedicated function pushbuttons on the RTU. These pushbuttons have
mechanical, momentary, nonlatching actions, but may have latched functions
implemented by system software.
Tune Knob Cluster
Two concentric knobs are used to tune frequencies (or select codes) for the RTU —
both knobs are rate-aided. The functions controlled by the tuning/code knobs include:
• active frequency/code
• preset frequency/code
• numbered preset channels in the preset field only
• HF COM squelch/emission mode values
COMMUNICATIONS
6-12 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
The function to be tuned is selected using the line select keys. A tuning window is
displayed around the frequency/code to be tuned to confirm the selection.
Tuning Window
The tuning window is displayed as a rectangle around the frequency/code to be tuned
or modified. The default position for the tuning window on the primary top level
display is the VHF COM preset frequency.
When no activity is detected from the line select keys or tuning/
code knobs for 20 seconds, the display page reverts to the
primary top level display and the tuning window is placed at the
default position.
Radio Tuning Unit
Figure 6-5
NOTE
IDENT
DME-H
1/2
BRT
BRT
116.30
ACT PRE
111.35
NAV1
ACT PRE
121.90 149.10
COM1
373.0
ADF 1 TCAS
TA
ATC1
NEXT
PAGE 5540
STBY
TONE
REL
Tuning Knobs
Concentric knobs to select
frequencies or codes
Brightness (BRT) Control
Controls brightness of
displays
Line Select Keys
These keys can
function as:
- frequency
selector
- mode selector
- function selector
- line selector
depending on the
display
- page selector
Active Frequency Readout
Indicates frequency set at
COM radio (active)
Preset or Recall Frequency Readout
Pre
Recall
- frequency was changed by tuning
knobs; i.e. preset
- frequency was swapped with
active frequency
ATC Identification
(IDENT)
Pushbutton
Pushed at ATC
controller request,
causes an additional
identification pattern
on ATC ground
radar screen
DME-HOLD
(DME-H)
Pushbutton
When pushed,
holds DME at
current frequency
and allows
navigation receiver
to be independently
retuned
Left Side / Right Side
(1/2) Pushbutton
Push to select left side (1)
or right side (2) radios, for
tuning. Arrows indicate
side selected
P604_06_005
COMMUNICATIONS
For Training Purposes Only
Jan 04
6-13
P I LOT T R A I N I N G GU I D E
Active and Preset Frequencies/Codes
The preset frequency/code appears on the right side of the subdisplay. If the preset
frequency/code has been tuned or otherwise modified, a PRE annunciator is displayed
above it. If the active and preset frequencies/codes are swapped, a RECALL
annunciator appears above the preset frequency/code. Additionally, if the tuning
window surrounds the preset frequency/code, an arrow appears to the right of the PRE
or RECALL annunciator to indicate that the next press of the associated line select key
will cause the active and preset frequency/code to swap.
Reversionary/Inhibit Panel
The reversionary/inhibit panel allows selective deactivation of either or both RTUs,
and/or inhibits the FMS from tuning the COM/NAV systems.
Reversionary/Inhibit Panel
Figure 6-6
RTU 1 (2) INHIBIT Switch/Lights
RTU 1
RTU 2
- when pressed in (latched), light comes on,
disables RTU 1 and enables direct cross-side
tuning of off-side radios (RTU 2 controlling COM 1,
NAV 1, etc.)
- when pressed in (latched), light comes on,
disables RTU 2 and enables cross-side tuning of
off-side radios (RTU 1 controlling COM 2, NAV 2).
FMS TUNE INHIB Switch/Light
When pressed in (latched), light comes
on and prevents RTUs from being
tuned by either FMS.
P604_06_006
INHIBIT PUSH
1-RTU-2 FMS TUNE
1 2
AFCS
SEL
STBY
1 2
ATC
SEL
FMS
TUNE
INHIB
RTU 1
INHIB
RTU 2
INHIB
COMMUNICATIONS
6-14 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
Operation
The operation of the RTU is presented in a sequence that shows the top page followed
by the hierarchy of the selected system.
Display Hierarchy
The RTU display is two-level tiered for the VHF COM/NAV, ADF, ATC and TCAS
systems as follows:
• primary top level display
• main display page
The RTU display is three-level tiered for the auxiliary VHF COM (3) transceiver as
follows:
• primary top level display
• secondary top level display
• auxiliary VHF COM main
The RTU display is four-level tiered for the HF COM system as follows:
• primary top level display
• secondary top level display
• HF COM main
• number preset pages
COMMUNICATIONS
For Training Purposes Only
Sept 04
6-15
P I LOT T R A I N I N G GU I D E
.
COM/NAV Selections
Figure 6-7
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF1 TCAS
TA
ATC1
NEXT
PAGE 4567
TONE
REL
25 SEL
IDENT
DME-H
1/2
BRT
BRT
ACT PRE
108.50 149.10
NAV1
MKR
RETURN
TONE
SENS
DME
108.50
LO HI
IDENT
DME-H
1/2
BRT
BRT
ON
SQUELCH
ACT PRE
123.45 134.92
COM1
RETURN
TONE
OFF
KNOB SEL
8.33 25
PRIMARY TOP LEVEL DISPLAY
FREQ Change Swap Key
TUNE
SWAP
- tune window in view,
use tuning knob. Tune
window not in view, push
key, then use tuning knobs.
PRE label comes ON.
- push key to
interchange preset and
active frequencies. RECALL
label comes ON.
COM Source
Annunciator
NAV Main Page
Used to select
navigation frequencies
DME Frequency Readout
Indicates frequency of
DME receiver
MKR SENS Readout
Used to adjust marker
beacon sensitivity
Frequency Readout
Indicates active NAV
frequency
COM PAGE
NAV PAGE
P604_06_007
Line Select Key
Toggles between 8.33 /
25 kHz modes of operation
COMMUNICATIONS
6-16 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
COM 3 Selections
Figure 6-8
IDENT
DME-H
1/2
BRT
BRT
ON
SQUELCH
ACT PRE
123.45 134.92
COM1
RETURN
TONE
OFF
KNOB SEL
8.33 25
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF1 TCAS
TA
ATC1
NEXT
PAGE 4567
TONE
REL
IDENT
DME-H
1/2
BRT
BRT
123.45
ACT PRE
134.92
COM3
ACT PRE
19.4560 8.0040
HF1
TONE
UV
SQ0
23.4687
RETURN
Return Key
When pushed, returns
to top level page. All
changes carried
forward.
PRIMARY TOP LEVEL DISPLAY
AUX COM
Preset Display
Frequency Readout
Indicates active VHF
frequency
Squelch Readout
Squelch Key
FREQ Change Swap Key
TUNE
SWAP
- tune window in
view, use tuning knob. Tune
window not in view, push
key, then use tuning knobs.
PRE label comes ON.
- push key to
interchange preset and
active frequencies. RECALL
label comes on.
SECONDARY PAGE
COM 3 PAGE
P604_06_008
AUX COM Display
25 SEL
COMMUNICATIONS
For Training Purposes Only
May 03
6-17
P I LOT T R A I N I N G GU I D E
ADF, ATC and TCAS Selections
Figure 6-9
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF1 TCAS
TA
ATC1
NEXT
PAGE 4567
TONE
REL
IDENT
DME-H
1/2
BRT
BRT
REL
ALT
MODE
TCAS
RETURN
TONE
ABS
TEST
BELOW
NORM
TRAFFIC
AUTO STBY
TA ONLY
ON
OFF
ABOVE
IDENT
DME-H
1/2
BRT
BRT
ALT
4567
ATC
RETURN
TONE
ON OFF
410
STBY
IDENT
DME-H
1/2
BRT
BRT
MODE
238.0
ADF1
RETURN
TONE
TONE
TEST
OFF ON
ADF ANT
PRIMARY TOP LEVEL DISPLAY
MODE Key
ANT
ADF
Selects either ADF or
ANTENNA functions:
- used for range
navigation, optimum
station tuning, or
monitoring commercial
broadcast
- selects directional
antenna which seeks
signal source
TONE Key Switch
ON
OFF
Selects tone circuit
either ON or OFF.
- superimposes an
aural signal on
unmodulated carrier
waves to aid in precise
frequency selection.
- shuts off aural
signal.
ADF PAGE
TEST Line Key
ATC PAGE
TCAS PAGE
ATC Code
Display
ALT
Annunciator
ALT Mode Key
ON
OFF
Selects altitude readout
- reported altitude is
displayed
- reported altitude
goes out
Tune Window
ATC Main Page
Selects ATC modes and
frequencies
RETURN Line Key
Mode Of Operation
Readout
ATC 1/2
STBY
Indicates active mode of
operation
ATC IDENTIFICATION (ID)
Pushbutton
Pushed at ATC controller
request, causes an additional
identification pattern on ATC
ground radar screen
Altitude Display
TCAS MODE Select Key
AUTO
STBY
TA ONLY
Selects TCAS modes of
operation
- displays TA/RA
automatically (above
900 ft) or RA only (below
900 ft)
- STANDBY mode
- only traffic
advisories are displayed
Altitude Tag Key
REL
ABS
Selects altitude readout
type on MFD traffic symbols
- relative to own
aircraft altitude
- absolute with respect
to barometric altitude
Traffic Display Select Key
ON
OFF
Selects display mode:
displays all transponder
equipped traffic
displays threat traffic only
–
–
Altitude Range Select Key
BELOW
Selects range values:
– -9900 ft to +2700 ft.
NORM – -2700 ft to + 2700 ft.
ABOVE – -2700 ft to + 9900 ft.
TCAS Test Key
Initiates TCAS self-test on the ground only
ADF Main Page
Selects ADF modes and
frequencies
P604_06_009
COMMUNICATIONS
6-18 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
HF Selections
Figure 6-10
IDENT
DME-H
1/2
BRT
BRT
ACT PRE
22.3576 8.0040
HF1
UV
SQ3
RETURN
TUNE
EMER FREQ
PRESET ITU
LO
POWER
MED HI
PRESET
PAGE
TEST
SIMPLEX
DUPLEX
IDENT
DME-H
1/2
BRT
BRT
14
8.0040
ACT
23.4687 8.0040
HF1
UV
SQ3
23.1040
RT
RETURN
26.9436
AM
26.9436
22.1040
LV
15
16
R
T
NEXT
PAGE
LV
13
IDENT
DME-H
1/2
BRT
BRT
123.45
ACT PRE
134.92
COM3
ACT PRE
19.4560
HF1
TONE
UV
SQ0
RETURN
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF1 TCAS
AUTO REL
ATC
NEXT
PAGE 4567
STBY
TONE
PRIMARY TOP LEVEL DISPLAY
HF Display HF Preset
Display
HF Main Page
Used to select HF
frequencies and modes
FREQ Key
Push once to directly tune
HF with tuning knobs
MODE KEYS
SQ
UV
LV
AM
SIMPLEX
DUPLEX
PRESET PAGE
EMER FREQ
PRESET ITU
POWER
TEST
Push key adjacent to
desired mode:
- COM squelch
- upper sideband voice
- lower sideband voice
- amplitude
modulation
- RX and TX
modes paired
- RX and TX
modes separated
-
company frequencies
- 6 channel
preset select
- selects
maritime channels
- selects power
level
- initiates test
function
Frequency Select Knobs
Outer knob is cursor control
moving cursor box within tune
window.
Inner knob changes digits
within cursor box
HF Active Display
NEXT PAGE Line Key
Allows selection of
preset channels 1-16
Preset Page Number
Preset Page Line Keys (4)
Simplex Frequency Display
Preset Operating Mode
(AM/LV/UV)
Duplex Receive
Frequency Display
Duplex Transmit
Frequency Display
HF PRESET PAGE
P604_06_010
UP Select Key
Scrolls through HF
pages.
Freq Change/Swap Keys
Pushed, moves tune window
to ____ line (default position).
Tuning knobs used to change
frequency. Pushed again,
swaps active and preset
frequencies.
SIMPLEX
DUPLEX
UV
UV
8.0040
23.1040
RT
UV
COMMUNICATIONS
For Training Purposes Only
May 03
6-19
P I LOT T R A I N I N G GU I D E
RTU Failure Indications
RTU and COM/NAV Failure Indications
Figure 6-11
Self-Test
On power-up, the RTU performs a self-test. Should the RTU fail the self-test, the
screen will go blank and an RTU FAILURE annunciator will appear in the center of
the screen.
IDENT
DME-H
1/2
BRT
BRT
ACT PRE
108.15
NAV1
ACT PRE
134.92
COM1
ADF 1 TCAS
ATC
FAIL
TONE
DME - -
IDENT
DME-H
1/2
BRT
BRT
RTU FAILURE
RTU Failure
Message (red)
Comes on in center
of CRT. RTU detects
internal failure during
self-test
P604_06_011
COMMUNICATIONS
6-20 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Overtemperature
The internal temperature is constantly monitored. If the temperature exceeds the
internal threshold, the RTU TEMP annunciator is displayed.
Readout
When a value is selected, it is not displayed on the RTU unless it has been accepted by
the addressed system or unit and returned to the RTU. If the echoed data does not
match the new value selected within two seconds, the displayed data is replaced by
dashes indicating that the selection has failed.
RTU TEMP Annunciation
Figure 6-12
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF 1 TCAS
AUTO REL
ATC
NEXT
PAGE 4567
STBY
TONE
RTU
TEMP
P604_06_012
COMMUNICATIONS
For Training Purposes Only
May 03
6-21
P I LOT T R A I N I N G GU I D E
Cockpit Voice Recorder System
Description
The cockpit voice recorder (CVR) system is a high-fidelity recorder which records the
flight crew conversations, radio communications and flight compartment sounds on
three separate channels. A fourth channel is used for synchronization with the flight
data recorder (FDR). The system operates in conjunction with the audio integrating
system. The CVR consists of the following components:
• one recorder
• one CVR control unit
• one microphone
Recorder
The recorder is designed to continuously acquire and store, in a solid-state memory,
audio data for a minimum of 30 minutes. The solid-state memory has no moving parts
to ensure maximum reliability.
COMMUNICATIONS
6-22 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
CVR System
Figure 6-13
HEADSET
COCKPIT VOICE
RECORDER
ERASE
HOLD
5 SEC
TEST
COCKPIT VOICE RECORDER PANEL
VOICE RECORDER
MICROPHONE
VOICE RECORDER UNIT
Underwater
Locating Device
P604_06_013
COMMUNICATIONS
For Training Purposes Only
Sept 04
6-23
P I LOT T R A I N I N G GU I D E
CVR Control Unit
The CVR control unit contains a meter, an ERASE and a TEST Pushbutton, and a
headset monitor jack.
Microphone
The remote area microphone is mounted on the overhead panel behind a grille. The
microphone picks up flight compartment conversations and sounds, and feeds them
into the recorder.
Controls and Indicators
For controls and indicators, refer to the CVR control unit section.
Cockpit Voice Recorder Panel
Figure 6-14
HEADSET
COCKPIT VOICE
RECORDER
ERASE
HOLD
5 SEC
TEST
Test Pushbutton Switch
Press to test Voice Recorder System. A green light
will illuminate. If headset is plugged into unit, a test
tone will be heard.
Erase Pushbutton Switch
When pressed for at least two seconds, erases all
recorded information, provided the airplane has landed
and the parking brake is set.
Headset Monitor Jack
With headset plug in, allows monitoring of tone
transmission during test and audio signals
being recorded.
P604_06_014
COMMUNICATIONS
6-24 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
Operation
The CVR constantly records when power is supplied to the system. The only way to
preserve specific recorded information is to pull the CVR circuit breaker or otherwise
shut down the system.
Test
Incorporated into the CVR is a built-in-test-equipment (BITE) utility program which
provides a go/no-go indication.
The self-test is initiated by pressing the TEST Pushbutton on the CVR control unit.
This causes a test tone to be applied to each channel individually. The test tone is
processed, stored in memory and read from memory. The tone is then checked for
expected frequency and amplitude.
Visual indication of the test is provided on the test meter. The test meter provides an
indicator signal which is the go/no-go display.
The phone jack permits monitoring of the actual recorded audio as well as the tone
bursts during test.
Erase
The ERASE Pushbutton will bulk-erase the entire memory, provided that the parking
brake is set and the WOW interlocks are closed. The bulk-erase Pushbutton must be
held for more than two seconds for the bulk-erase to take place.
COMMUNICATIONS
For Training Purposes Only
May 03
6-25
P I LOT T R A I N I N G GU I D E
Flight Data Recorder System
Description
The flight data recorder (FDR) is a solid-state system that records airplane flight
parameters for future retrieval and analysis.
The FDR puts a digital stream of data from the data concentrators into a solid-state
memory module which has a capacity to retain 25 hours of data. When the memory
module is full, the data is progressively overwritten by the most recent data being
recorded.
Components and Operation
The FDR system consists of the following components:
• one recorder
• one FDR EVENT switch
Recorder
The recorder solid-state memory has no moving parts. This ensures maximum
reliability. Recorded data may also be retrieved (downloaded) for analysis purposes.
The FDR is automatically turned on when the right engine start switch is pushed. It
then starts to record data from the data concentrator unit (DCU). This data is fed back
to the originating DCU. If the DCU is unable to synchronize with the data returned
from the FDR for longer than 8 seconds, the FDR FAIL status message will be
displayed on the EICAS.
The FDR shuts down when power is removed from the system by pulling the FDR
circuit breaker or by shutting down the aircraft.
COMMUNICATIONS
6-26 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Flight Data Recorder System
Figure 6-15
PASS SIGNS EMER LTS
NO SMKG SEAT BELTS
ON
OFF
ARM
FDR
EVENT
ON
OFF
AUTO
ON
OFF
AUTO
O
A A
Underwater
Locating
Device
FLIGHT DATA
RECORDER UNIT
FDR Event Switch
Push to mark a specific
date/time on flight data
recordings
P604_06_015
COMMUNICATIONS
For Training Purposes Only
May 03
6-27
P I LOT T R A I N I N G GU I D E
Controls and Indicators
FDR EVENT Switch
The FDR EVENT switch is located on the PASS SIGNS/EMER LTS/FDR EVENT
panel. When pushed, the switch sends a signal to the data concentrators which place a
marker in the recorder memory to facilitate data retrieval. An event marker can be
added to the FDR any time the FDR is operating.
EICAS Messages
MESSAGE MEANING AURAL WARNING
(IF ANY)
FDR EVENT Confirm the flight data recorder has set a marker in response
to activation of the button on the control panel.
SELCAL HF 1/2
A call for this aircraft has been detected on the respective
high-frequency radio. Message will be canceled when that
radio is keyed to reply.
“SELCAL”
FDR FAIL Indicates the flight data recorder is inoperative.
EICAS Messages
Table 6-1
COMMUNICATIONS
6-28 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Static Dischargers
Description
The aircraft is equipped with a system of wicks on the aft-facing surfaces and
horizontal stabilizer tips. Each wick consists of a base and a discharger. The 24 (26 as
per SB 604-23-006) dischargers allow gradual bleed-off of static electrical charges
from the airframe to prevent radio interference.
Static Dischargers Location
Figure 6-16
P604_06_016

kakabrazil

学习了。。。