190-01639-00
GSU 75 ADAHRS Installation Manual
Rev. 6
Page 5-11
Table 5-2 Fixed-wing Aircraft Magnetometer Interference Test Sequence Example
Elapsed Time
Since Start of Test (min:secs)
A
ction
0:00
Test begins
0:10
Aileron full right
0:20
Aileron full left
0:30
Aileron level
0:40
Flaps down
0:50
Flaps up
1:00
Landing gear up
1:20
Landing gear down
1:40
Speed brake up
1:50
Speed brake down
2:00
Navigation lights on
2:10
Navigation lights off
2:20
Landing lights on
2:30
Landing lights off
2:40
Taxi lights on
2:50
Taxi lights off
3:00
L Taxi lights on
3:10
L Taxi lights off
3:20
Strobes on
3:30
Strobes off
3:40
Recognition lights on
3:50
Recognition lights off
4:00
Turn on all wing-tip lights simultaneously (typically will
include navigation lights, recognition lights and strobe)
4:10
Turn off all wing-tip lights simultaneously
4:20
Beacon on
4:30
Beacon off
4:40
Pitot heat on
4:50
Pitot heat off
5:00
End of test
340095
The document reference is online, please check the correspondence between the online documentation and the printed version.
