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An optional database loading kit (PCD-3000) is available. This kit allows simultaneous database loading of up to three FMSs.
Data Base Unit
Figure 17.10.75
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Synchronized/Independent Operation
Dual-FMS system have provisions for operation in synchronized (SYNC) or independent (INDEP) modes. By default, dual-FMS airplanes power up in SYNC, and triple-FMS airplanes power up in INDEP mode.
In the triple-FMS configuration, the flight crew decides which two FMSs to synchronize. FMS 3 is selected using the FMS reversionary selector switch (see Figure 17.10.77). SYNC/INDEP mode selections are made on the FMS CONTROL page of the CDU.
When two FMSs are synchronized, they share the following parameters:
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Flight plan edits;
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Performance initialization;
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Leg sequencing (based on NAV source selection);
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Active database selection;
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Fix entries on FIX INFO page;
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Deselection of navaids;
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Performance mode selection, fuel flow and ground speed entered on FUEL MGMT page;
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MAG/TRU display mode;
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Thrust management;
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Direct-to edits;
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Holding pattern data; and
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Enabling/disabling of VOR/DME from the navigation solution.
Parameters that are not synchronized include:
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FMC position initialization; and
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Selection and tuning of on-side sensors.
When the FMSs are operated in INDEP mode, all parameters must be manually entered in each FMS.
For additional information about SYNC/INDEP operation, see the “Collins FMS-6000 for the Challenger 605” Pilot’s Guide.
Controls and Indicators
FMS CDU Tune Inhibit
The FMS CDUs may be inhibited from tuning the radios by selection of the CDU 1 INHIB or CDU 2 INHIB switch/light, located on the reversionary panel. The lights illuminate when CDU auto tuning inhibit is selected.
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FMS TUNE INHIB Switch/Light Figure 17.10.76
FMS 3 Reversionary Selector
FMS 3 may be selected using the FMS 3 reversionary selector switch on the center pedestal. FMS 3 replaces FMS 1 or FMS 2 when the rotary selector switch is moved to position 1 or 2 respectively.
FMS 3 Reversionary Selector Figure 17.10.77
FMS Message Displays
The FMS messages are displayed in several locations. Typically, a message remains displayed as long as the condition that generated the message persists. For a complete description of messages and message categories, see the “Collins FMS-6000 for the Challenger 605” Pilot’s Guide.
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