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NOTE
Pressing the NAV preselect key highlights the MEMORY window. Rotating the TUNE knob will scroll through the frequencies in MEMORY.
Pressing the transfer key will toggle the Active and Preset frequencies, channeling the NAV receiver to what had been the Preset.
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Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
While on the main tuning page, press the PGE button once to bring the NAV memory page into view.
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An FMS autotuned VOR or ILS frequency is displayed on the main tuning page. To override an FMS autotuned VOR or ILS frequency, toggle the transfer key, or enter a new active frequency.
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Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
The DME simultaneously tracks four selected DME channels for distance, groundspeed and time to station, as well as monitoring two additional channels for ident functions. DME dedicates two of the four channels to the FMS.
In normal VOR/ILS/DME operations, one of the six DME channels is paired with the active frequency and another with a preset frequency. Pushing the DME function key will split the NAV window on the main tuning page, allowing the active DME channel to be selected separate from the active VOR/ILS frequency.
An H (hold) will be displayed to indicate that the distance display is not paired with the VOR/ILS navigation data. When DME hold is no longer required, cycle the DME function button until the split is removed from the NAV window.
DME Hold
ILS/VOR DME Ident
NOTE
Cycling the DME function button will display the following in sequence: VOR/ILS . VOR/ILS and DME . VOR/ILS and TACAN . VOR/ILS.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
ATC Transponder operations are controlled by the adjacent line select keys and the tuning knobs.
Both RMUs will display the same transponder information. If a code or mode is changed on one RMU, the other RMU will track it.
The transponder will go into ident mode for approximately 18 seconds when the ID function key is pushed and an ID annunciator will appear.
A reply annunciator (rectangular box), located in the upper right corner of the ATC window, will turn yellow, whenever the transponder is replying to an interrogation from a ground station or TCAS. When ID button is pressed, the reply annunciator will come on steady for approximately 20 seconds.
Reply Annunciator
Ident Annunciator
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Flight Crew Operating Manual Rev 2A, Apr 11, 2005
The TCAS is an airborne system that interrogates ATC transponders in nearby airplanes to identify and display potential and predicted collision threats, within 700 feet of closest point of approach. TCAS monitors a radius of up to 40 nautical miles about the airplane, computes range, bearing and closure rate of up to 12 other transponder equipped airplanes relative to the “own”airplane. TCAS and ATC transponder modes are set on the RMUs.
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