曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
of the beacon. The unit is equipped with a battery having a life expectancy of 6 years.
CFO0601002_007
MICROPHONE
STANDBY COMPASS WITH ALL RADIOS ON SWUNG
TO FLY
STEER
N 30 60 E 120 150 S 210 240 W 300 330
BY
AREA MICROPHONE
COMMUNICATIONS
Volume 2 Flight Crew Operating Manual Sep 13/2004
06-01-16 CSP 100-6 REV 1
EMERGENCY LOCATOR TRANSMITTER
DESCRIPTION
The emergency locator transmitter (ELT) is a self contained battery operated unit, located in the top left side of the aft fuselage.
When the aircraft is subjected to excessive longitudinal forces, the ELT is automatically activated and transmits on
121.5 (VHF), 243.0 MHz (UHF) and 406.025 MHz. When the ELT is transmitting, an ELT ON (C) CAS message
is illuminated.
The flight deck ELT switch is normally set to ARM. The ON position is for system test, or to manually activate the ELT.
The RESET position resets the ELT.
An ELT buzzer is installed in the rear fuselage section near a venting cutout. It is installed so that the buzzer alarm will not
distract the flight crew, but will be audible during ground operations and servicing when the engines are not operating.
CABIN COMMUNICATION SYSTEM (OPTIONAL)
DESCRIPTION
The cabin communication system option provides a private automatic branch exchange switching network. This network
routes voice and data communications for up to nine optional active devices (handsets/FAXs/modems/data link, etc.) in the
airplane and provides two air-to-ground channels. The systems includes connections of basic telephone/telecomputing
equipment to UHF antenna and SATCOM links. If a data link device is installed on the airplane, the cabin communication
system has the capability to communicate with the data link device using an internal modem.
COMPONENTS AND OPERATION
The digital radio components consist of: one UHF antenna, a duplexer and one airborne radio telecommunication unit.The
digital handset is located in the flight compartment and has a backlit LCD display and telephone style keypad to dial calls
and select various options. A credit card reader (for optional billing) is built into the handset and a two-button increase/
decrease volume control (side of handset) is also installed.
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 information.
CFO0601002_009
ON
ARM
RESET
ELT
FOR AVIATION
EMER USE ONLY
UNAUTHORIZED OPERATION
PROHIBITED
COMMUNICATIONS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 06-01-17
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_Challenger_Global_00-Communications(9)
