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pointer will be removed.
If a VOR bearing is displayed with true heading selected, the bearing pointer will be displayed
without correction for magnetic variation, and a white “T” is displayed after the bearing icon.
Bearing Pointer Menu
Figure 11−10−39
Drift Angle Pointer (Track Pointer Display)
The drift angle pointer (green circle) indicates the aircraft drift angle in relationship to a
programmed FMS route. The amount of aircraft drift is indicated by the angular displacement of
the green circle from the aircraft heading indicator. The drift angle pointer is green when the
on-side FMS is the NAV source.
Wind Display
When FMS-sensed winds are more than 5 knots, a green wind speed magnitude direction arrow
and a digital readout are displayed on the left side of the PFD/MFD navigation formats.
The wind is computed by the onside FMS regardless of the active NAV source, and its
magnitude values are from 5 to 255 knots.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−44
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
NAVIGATION DISPLAYS (CONT'D)
Navigation Display Indications
Figure 11−10−40
FMS (VNAV) and ILS (GS) Vertical Deviation Display
If LOC is the preselect or active NAV Source, a glideslope deviation scale is displayed to the left
of the altitude tape. The vertical deviation is displayed as a diamond-shaped pointer against a
vertical analog scale. The vertical deviation scale goes out of view when LOC is no longer the
active NAV source.
In the case of a GS failure, the diamond pointer will be removed, and a red boxed GS will be
displayed at the lower end of the scale.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−45
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
NAVIGATION DISPLAYS (CONT'D)
When the FMS is the active NAV source, the vertical deviation scale is also in view for VNAV
commands to be displayed. The VNAV pointer is displayed as an FMS magenta waypoint
symbol, or yellow waypoint from cross-side FMS.
In the case of a VNAV failure, the pointer will be removed, and a red boxed VNV will be
displayed above the deviation scale.
Flight Path Vector (FPV)
The Flight Path Vector (FPV) symbol indicates the actual flight path vector in space. The lateral
position, computed by IRS, represents the angular distance of the aircraft track to the heading.
The vertical position represents the climb or descent angle relative to the horizon.
The FPV is displayed by selecting FLT PATH VCTR in the CONFIG submenu of the PFD Menu.
The FPV is limited laterally between the airspeed tape and the altitude tape, and vertically
limited between the lateral deviation scale and the FMA.
Maker Beacon Display
On the ADI, the marker beacon is used in conjunction with the ILS, and is displayed to the right
of the airplane symbol.
When the aircraft is flying over a marker beacon, the following annunciation is presented:
• Outer marker is a boxed, cyan OM legend (GS intercept approximately 1,400 ft above
touchdown).
• Middle marker is a boxed, yellow MM legend (GS intercept approximately 200 ft above
touchdown).
• Airway/inner marker is a boxed, white IM legend (GS intercept approximately 100 ft
above touchdown).
Navigation Indications on ADI and FLT PATH VCTR Menu Selection
Figure 11−10−41
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−46
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
NAVIGATION DISPLAYS (CONT'D)
Navigation Source Warning Flags
A red boxed navigation source flag (VOR, LOC or FMS) is displayed during a failure of the
selected NAV source. The navigation display is removed from view when the flag is displayed.
A red boxed GS will be displayed at the lower end of the vertical deviation scale for a GS failure.
For an FMS VNAV failure, a red boxed VNV will be displayed above the vertical deviation scale.
In case of a LOC failure, a red boxed LOC will be displayed on the left side of the lateral
deviation scale of the ADI.
Navigation Source Warning Flags
Figure 11−10−42
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−47
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EFIS COMPARATOR MONITOR
Description
Comparators alert the pilots of any disagreement of data between specific systems. Each PFD
performs its own software monitoring, and continuously compares its information with the data
presented on the other PFD.
When an EFIS comparison disagreement between the PFDs is detected, a flashing yellow data
　
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