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Refer to the Magnastar C-2000 user guide CA1030 for description/function and operation of the system.
FLIGHT COMPARTMENT PRINTER (OPTIONAL)
DESCRIPTION
The optional flight compartment printer is installed in the copilot side console. The printer has ARINC 429 and standard PC interfaces and is capable of full format and graphic printing of information from Central Aircraft Information Maintenance System (CAIMS) and DATALINK.
COMPONENTS AND OPERATION
The printer can be used to print selected messages and weather data sent to it via the airborne data link system. The printer is also used by the central aircraft information maintenance system to print out certain maintenance faults and status infor-mation.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
06-01-16 FLIGHT DATA RECORDER (FDR) (OPTIONAL)
DESCRIPTION
The solid state flight data recorder (FDR) unit is located in the tail section of the aircraft. The (FDR) records aircraft flight parameters. The FDR includes a digital FDR, an underwater locator device (ULD), and a tri-axial accelerometer.
COMPONENTS AND OPERATION RECORDER UNIT
The recorder unit is housed inside a crash survivable container. Access to the container is through the aft equipment bay.
The unit records data using a solid state non-volatile memory. The unit records the last 25 hours of critical aircraft and flight parameter data. An underwater locator device (ULD) is installed on the front of the recorder and emits a pulsed acoustic signal into the water after ditching of the aircraft.
The ULD beacon is capable of transmitting up to 30 days after activation. The FDR starts to record when one of the following occurs:
-STROBE/BEACON switch is in the BEACON or STROBE position
-Weight-off-wheels as sensed by the proximity sensing electronic unit (PSEU)
If the aircraft experiences impact deceleration, electrical power is removed from the recorder. Removal of power prevents the erasure of the stored digital information.
EVENT (button)
Pressing the EVENT button on the ENGINE panel places an event marker in the FDR data. This can be used when required during system functional testing as required by some regulatory agencies.
UNDERWATER LOCATOR DEVICE (ULD)
The ULD, mounted on the FDR front panel, is a battery-operated underwater acoustic pulse generator. The ULD transmits when submerged under water.
TRI-AXIAL ACCELEROMETER
The tri-axial accelerometer is used for acceleration measurements. It contains three separate seismic sensors that measure vertical, lateral, and longitudinal acceleration near the center of gravity of the aircraft. This data is sent to the DCUs where it is formatted for the FDR.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
06-01-17 EICAS MESSAGES
Communication messages are shown on the EICAS. In the table below is a list of communication system messages. A brief explanation of each message is provided.
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