Challenger 604 Flight Management System

Front 1

At Power-up, the FMS systems

Back 1

Must be manually synchronized only if 3 FMS are installed

Front 2

The data base unit (DBU)

Back 2

Is used to install (update) the database for each FMS

Can write data to floppy disks from the MDC

Can include an optional CD-ROM drive

Front 3

The POS INIT function

Back 3

Is required before the FMS can be synchronized

Front 4

Which FMS are available if the ADG deploys

Back 4

FMS 1 only

Front 5

Status of the database

Back 5

is indicated by white font when it is current

Is indicated by amber font when it is expired

Is shown as amber dashes appear if it is corrupted

Front 6

Each flight management system

Back 6

Gives highest priority to the GPS NAV source for calculating FMS position

Front 7

When the flight management systems are synchronized

Back 7

FMS position initialization and NAV sensor selection remain individually controlled by each FMS

Front 8

The next waypoint is indicated by

Back 8

Magenta font an the legs page and PFD/MFD

Front 9

Information and difinition of messages shown on the PFD/MFD or CDU are found

Back 9

Only in the Collins FMS-6000 pilots guide

Front 10

If the FMS TUNE INHIB button is pressed

Back 10

All FMS are inhibited from tuning radios or mode selections via the RADIO TUNING page

Front 11

A track (route segment) is intercepted by

Back 11

Press DIR, select or enter a waypoint that defines the segment, enter the course to intercept under INTC CRS (or push the adjecent line select key to make the value appear in large font if the course shown is okay), EXEC, select NAV mode

Front 12

In order to have a CLB thrust value displayed on the THRUST LIMITS page

Back 12

The engines must be supplying a pack

Front 13

If NAV 1 input to FMS 1 is lost, then

Back 13

NAV 2 is automatically used

Front 14

The left MFD failed, Can entries for a holding pattern from the FMS 1 CDU be previewed on the right MFD prior to executing?

Back 14

NO

Front 15

The type of FMS approach (V-MDA or RWY) is shown on the

Back 15

LEGS page

Front 16

A holding waypoint depicted as "HOLD AT" means

Back 16

The hold procedure is located at a waypoint other than the final approach fix of an approach entered in the FMS

Front 17

The FMS computes position based on

Back 17

An algorithm that averages the data from all NAV sensors except the IRS

IRS only if no other nav sensors are available