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Garmin GSU 75 - Table 5-2 Fixed-Wing Aircraft Magnetometer Interference Test Sequence Example

Garmin GSU 75
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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)
Action
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 Landing + Taxi lights on
3:10 Landing + 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.

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