6-62
General
SELF TEST OUTPUT
For the duration that the notification of legal rights page is
displayed during normal power up on the ground, all remote
annunciator lamps are lit up and the system generates a specific
set of electrical outputs for the purpose of self-test and
troubleshooting. The table below defines the outputs transmitted
during this time
.
Parameter
Self-test Value
Course Deviation
Half-scale left deviation, TO
indication, flag stowed
Glideslope/Vertical
Deviation
Half-scale up deviation, flag
stowed
Annunciators
All on
Bearing to Waypoint (RMI)
35°
Selected Course (OBS)
150° when interfaced to an
HSI with course pointer
Desired Track
50°
Distance To Go
0.0 NM
Time To Go
4 minutes
Active Waypoint
“AVDYN”
Groundspeed
150 knots
Present Position
N39°04.05’, W094°53.86’
Waypoint Alert
Active
Phase of Flight
Enroute
Message Alert
Active
GPS Integrity
Invalid
Roll Steering (if applicable
)
Flight Director commands 0°
bank (level flight) for 5
seconds; commands
increasing right bank at
1°/second for 5 seconds;
commands 5° right bank for
5 seconds; commands
decreasing right bank at
1°/second for 5 seconds,
until command is 0° bank
again. This cycle repeats
continuously
.
Summary of Contents for IFD540
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Page 8: ......
Page 82: ...2 28 FMS Pages Approaches Dropdown Box Procedures Brackets ...
Page 91: ...2 37 FMS Pages Four Additional Rows of Weather Data on Info Tab Info Tab Nearby Navaids ...
Page 101: ...2 47 FMS Pages User Waypoint Airfield Depiction on Map ...
Page 154: ...3 50 Map Pages Curved Flight Path with Next Leg Depiction Fly By Waypoint Depiction 1 ...
Page 156: ...3 52 Map Pages Missed Approach Enabled in Map SVS View ...
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