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When the DME TEST control is selected, the TEST annunciation shows in large cyan text. The DME distance is 100 NM, the TTG is 60 minutes, the station ID is AOK, and the ground speed is 100 knots. This test lasts about 10 seconds.
STATION IDENTIFIER
The navaid identifier is shown in the navigation data field above the distance display. Data for the identifier is supplied by the DME. In DME hold, the identifier is removed from view.
NAVIGATION ALERT FLAGS
NAVIGATION SOURCE WARNING FLAG
A red boxed navigation source flag (VOR, LOC, and FMS) is displayed during a failure of the selected NAV source. The navigation display is removed from view when the flag is displayed.
BEARING FLAG
Invalid data from the selected bearing source causes the bearing source annunciator to be replaced by a red boxed warning flag. The bearing pointer is removed from view when the flag is displayed.
HORIZONTAL SITUATION INDICATOR (HSI)
The horizontal situation indicator (HSI) represents the compass card, which incorporates selectable navaids, bearing and course pointers. HSI indications include:
-Course pointer
-Lateral deviation bar
-Lateral deviation scale
-To/from indicator
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
11-01-20 NAVIGATION DISPLAYS (Cont)
LATERAL DEVIATION SCALE
The lateral deviation scale has two dots on each side of the course arrow. Each dot represents:
-In VOR, 5° of deviation
-In LOC, 1° of deviation
-In FMS, 5 nautical miles
TO/FROM INDICATOR
The TO/FROM arrow is an outlined triangle on the course/desired track pointer. The arrow points toward the head of the
pointer to indicate a “TO” and toward the tail to indicate a “from”.
The color of the TO/FROM indicator is green for VOR onside information and amber for cross-side information.
In FMS mode the entire display is magenta.
AUTO FLIGHT CONTROL SYSTEM DISPLAY
The PFD presents automatic flight control system (AFCS) information consisting of flight guidance mode, autopilot mode indications, and flight director command bars.
AUTOPILOT INDICATION
Autopilot information concerning engagement, disengagement and flight director in use is displayed in the top center por-tion of the attitude display. A green AP indicates the autopilot has been engaged and the horizontal arrow points to the FD coupled side.
A flashing red AP indicates that the autopilot has disengaged. The AP symbol flashes for five seconds and the aural cavalry charge is heard. A white arrow indicates that the autopilot is not engaged and control of the FD is transferred to the indicated side when engaged.
FLIGHT GUIDANCE MODE
Flight Guidance modes are displayed on the top center portion of the PFD, with three fields divided by thin vertical grey lines. The left field of the line represents the lateral modes. The center field represents AP/YD engagement. The right side represents the vertical modes. Active modes are green and armed modes are white.
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