2. D. (3) (c)
(d)
(e)
(f)
DADC Failures - DADC failures are indicated by replacing the
SAT and TAS numerical values by amber dashes (Figure 215).
FMS
Failure - A failure of the FMS removes the active flight
plan waypoints, navaids,
and airports from the display. This
indication will also be given in the event of an invalid
heading display (Figure 215). The digital GSPD window is
replaced by amber dashes.
Weather Radar Failure - A failure is shown by displaying an
amber WX in the weather radar mode annunciation box (Figure
215).
EFIS Self-Test
- This test is initiated through the on-side
display controller TEST mode when airspeed is valid and less
than 60 knots and the
WOW switch is active.
Selecting the EFIS
self-test shows the invalid flags for the following MAP display
-parameters:
● IRS
● DADC
. VERT TRK, TRK CHG Annunciations
(4) Compass (COMP) Mode
The COMP mode is comprised of the following functions (Figure 217):
● 360-Degree Compass Rose
● Digital Heading Readout
● Magnetic/True Annunciation
. Heading Bug with Digital Readout
. Wind Display in Vector or X-Y Formats
● Course Pointer/CDI with Digital Readout
● Navigation Source Digital Distance Readout
● Navigation Source Annunciation
● To/From Indicator
● Bearing Pointers Circle/Diamond
c Bearing Pointer
Source Annunciation
● Vertical NAV Scale (GS/VNAV)
● NAV Preview Mode
22-14-00
Page 246
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document,
To Next Page
Loading...
