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The optional flight compartment printer is installed in the copilot’s side console. The printer has
ARINC 429 and standard PC interfaces and is capable of full format and graphic printing of
information from CAIMS and DATALINK.
GF0610_070
FAULT
LOW
PPR
OPEN
PUSH PUSH TO CLOSE
OPEN
PUSH
The printer can be used to print selected messages and weather data sent to it via the Airborne Data
Link System (ADLS). The printer is also used by the Central Aircraft Information Maintenance
System (CAIMS) to print out certain maintenance fault and status information. This is accomplished
via the Portable Maintenance Access Terminal (PMAT).
GF0610_071
fault reporting can be printed by pressing
the button and a short report will be
printed even if no faults are detected.
PRINT MAINT REPORT Button − active
PRINT MAINT
REPORT
The PMAT can be used to generate an active fault report to the printer by operating the “PRINT
MAINT REPORT” button located on the left forward bulkhead in the flight compartment.
COMMUNICATIONS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
06−10−39
FLIGHT COMPARTMENT PRINTER (IF INSTALLED) (CONT'D)
The printer interfaces with a communication link to the Airborne Data Link System (ADLS) and a
parallel interface from the PMAT.
GF0610_072
PMAT
AIRBORNE DATA LINK SYSTEM
PRINT MAINT PRINTER
REPORT
The printer push-buttons provide the following functions:
GF0610_073
or on when pressed.
door opened, illuminates in
conjunction with the TEST
indicator.
aural/visual alert function.
will illuminate all indicators
followed by a print out of test
results and pattern.
when the printer senses the
last remaining 10 feet of
paper on the supply roll.
advances paper while the
push−button is depressed.
OFF − turns the printer off
FAULT − paper out, printer
ALRT/RST − resets the printer
TEST − during the self−test,
LOW/PPR − illuminates
PPR PPR/ADV − continuously
ADV
LOW
PPR
TEST
ALRT
RST
FAULT
OFF
FAULT
LOW
PPR
OPEN
PUSH PUSH TO CLOSE
OPEN
PUSH
COMMUNICATIONS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
06−10−40
EICAS MESSAGES
GF0610_074a
SELCAL HF 1−2
Annunciated when HF1
or 2 indicates an
incoming message.
ELT TRANSMITTING
Emergency locator
transmitter is
transmitting.
SELCAL VHF 1−2−3
or 2 (or 3 on airplanes
with SB 700−23−002
incorporated) indicates
an incoming message.
ELT TRANSMITTING
FDR ACCEL FAIL
FDR FAIL
Annunciated when VHF1
SELCAL HF 1−2
SELCAL VHF 1−2−3
FDR FAIL
Flight Data Recorder
has failed.
FDR ACCEL FAIL
Flight Data Recorder
accelerometer has
failed.
COMMUNICATIONS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
06−10−41
COMMUNICATIONS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
06−10−42
THIS PAGE INTENTIONALLY LEFT BLANK
CB - COMM SYSTEM
GF0620_001
CB − COMM SYSTEM 1/5
AUDIO PANEL 1B
AUDIO PANEL 2A
AUDIO PANEL 2B
AUDIO PANEL 1A
IN
IN
IN
DC 1
BATT
DC 2
BATT
IN
AIRFONE SYSTEM
AIRFONE REPEATER
IN
DC 1
DC 1
IN
CB − COMM SYSTEM 2/5
DATA LINK
HF 1 COUPLER
HF 1 TRANSCVR
BATT CABIN FEED
IN
IN
IN
BATT
DC 1
DC 2
DC 2
IN
AUDIO PANEL 3B
AUDIO PANEL 3A
IN
DC 1
DC ESS
IN
CB − COMM SYSTEM 3/5
RMU 1 PWR B
RMU 2 PWR A
RMU 2 PWR B
RMU 1 PWR A
IN
IN
IN
DC 1
DC ESS
DC 2
BATT
IN
HF 2 TRANSCVR
HF 2 COUPLER
IN
DC 1
DC 1
IN
CB − COMM SYSTEM 4/5
SATCOM FREQ UNIT
SATCOM HPA FAN
SELCAL
SATCOM DATA UNIIT
IN
IN
IN
DC 1
AC 1 CCBP
AC 4
DC 1
IN
SATCOM ANT CTLR
SATCOM AMP
IN
AC 2 ACPC
DC 1
IN
CB − COMM SYSTEM 5/5
VHF COM 2
VHF COM 1
IN
DC 2
BATT
IN
TRANSPONDER 2
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