89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters
Rev 0 Page 7-45
© Honeywell International Inc. Do not copy without express permission of Honeywell.
7.6.14 Self-test Page
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) 135°
Selected Course (OBS) 150° when interfaced to an HSI with course pointer
Desired Track 150°
Distance To Go 10.0 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.
Table 115 Self-test Output
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