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The MFD is the primary radio tuning source for the system.
Lists the main components of the radio communication system.
Describes key functions and selectors on the ACPs.
Toggle switch activates oxygen mask microphone.
Switches for transmitting on selected radio or intercom.
Locations for connecting headsets to the audio system.
Describes the location of hand microphones.
Describes overhead speakers and volume control.
Describes locations for interphone connections for maintenance.
Describes the VHF-4000 transceiver and its frequency range.
Explains how to tune VHF radios using the MFD.
Details COM radio operations via the DCP.
Steps for tuning radios using the CDU.
Explains the function of the tune reversion switch.
Describes how MFD/CDU control is selected.
Describes the HF radio's frequency range and modes.
Details the receiver/transmitter, HF coupler, and antenna.
Procedures for HF tuning via DCP.
HF radio modes and tuning control via MFD menu.
Steps for tuning HF radios using the CDU.
HF transmit/receive modes and preset functionality.
How SELCAL codes are received and displayed.
Provides voice and data comms via satellite.
Details SDU, amplifier, antenna, and control unit.
Data link via VHF, HF, or SATCOM, controlled by FMS CDU.
Lists where static wicks are installed on the aircraft.
Describes CVR unit, audio channels, and control panel.
Explains CVR test procedure and data erasure.
Picks up sounds and voices in the flight compartment.
Stores audio data and aids in locating the recorder.
Describes ELT activation, transmission, and flight deck controls.
Provides private automatic branch exchange for voice/data.
For printing messages and maintenance data.
Describes FDR unit, ULD, and accelerometer.
Details recording triggers and event button function.
ULD and tri-axial accelerometer functions.
Messages related to CVR and FDR failures/faults.
Messages related to SELCAL reception and ELT status.
The MFD is the primary radio tuning source for the system.
Lists the main components of the radio communication system.
Describes key functions and selectors on the ACPs.
Toggle switch activates oxygen mask microphone.
Switches for transmitting on selected radio or intercom.
Locations for connecting headsets to the audio system.
Describes the location of hand microphones.
Describes overhead speakers and volume control.
Describes locations for interphone connections for maintenance.
Describes the VHF-4000 transceiver and its frequency range.
Explains how to tune VHF radios using the MFD.
Details COM radio operations via the DCP.
Steps for tuning radios using the CDU.
Explains the function of the tune reversion switch.
Describes how MFD/CDU control is selected.
Describes the HF radio's frequency range and modes.
Details the receiver/transmitter, HF coupler, and antenna.
Procedures for HF tuning via DCP.
HF radio modes and tuning control via MFD menu.
Steps for tuning HF radios using the CDU.
HF transmit/receive modes and preset functionality.
How SELCAL codes are received and displayed.
Provides voice and data comms via satellite.
Details SDU, amplifier, antenna, and control unit.
Data link via VHF, HF, or SATCOM, controlled by FMS CDU.
Lists where static wicks are installed on the aircraft.
Describes CVR unit, audio channels, and control panel.
Explains CVR test procedure and data erasure.
Picks up sounds and voices in the flight compartment.
Stores audio data and aids in locating the recorder.
Describes ELT activation, transmission, and flight deck controls.
Provides private automatic branch exchange for voice/data.
For printing messages and maintenance data.
Describes FDR unit, ULD, and accelerometer.
Details recording triggers and event button function.
ULD and tri-axial accelerometer functions.
Messages related to CVR and FDR failures/faults.
Messages related to SELCAL reception and ELT status.
General| Manufacturer | Bombardier Aerospace |
|---|---|
| Crew | 2 |
| Passenger Capacity | 8-10 |
| Length | 20.92 m (68 ft 8 in) |
| Wingspan | 19.46 m (63 ft 10 in) |
| Height | 6.20 m (20 ft 4 in) |
| Engines | 2 × Honeywell HTF7000 turbofans |
| Introduction | 2004 |
| Service Ceiling | 13, 716 m (45, 000 ft) |
| Maximum Range | 5, 741 km (3, 100 nmi) |
| Cruise Speed | 850 km/h (530 mph) |
| First Flight | August 14, 2001 |
