Lynx NGT-9000
Installation Manual
3.10.2.6 FIS-B Uplink Check
Before performing this check ensure that the GPS position on the NGT-9000 is acquired, and that the
NGT-9000 is in
Ground Test
mode (in air). If installed the ADS-B Out Fail lamp is OFF.
1.
Perform the FIS-B check using the IFR-6000 (or equivalent) Ramp Test Set. The test set simulates
FIS-B ground base uplink (such as a METAR).
2.
Set the unit to each of the FIS-B screens listed below and verify that information (such as a METAR).
is being displayed.
•
FIS-B Graphic Application screen
•
FIS-B Graphic Winds and Temp
•
FIS-B Text data
3.10.2.7 TAS Traffic Check
Test required only for models with TAS. The TAS antenna calibration needs to be completed prior to this
test.
Before performing this check, ensure that the NGT-9000 is in
Ground Test
mode (in air).
1.
Perform the TAS check using the IFR-6000 (or equivalent) Ramp Test Set. The test set simulates
TAS intruders by manually defining a scenario and can then verify the correct Traffic Advisories
have occurred on the unit. Intruding flight patterns are programmed from the IFR-6000 screen.
2.
Verify that Traffic information displayed on the unit with that being transmitted by the test set.
3.
Compare and verify the heading data transmitted by the test set is being displayed correctly on the
unit.
4.
Verify audio alerts are being heard through the audio system. Adjustment of the audio volume may
be required. Refer to the configuration setup for instructions.
•
Electromagnetic Interference (E.M.I.) Check
Check the following applicable aircraft systems, as well as any other system or device that is not listed,
for interference. Initial tests are to be conducted with the aircraft operating on external ground power.
Disregard any system or device that does not apply.
NOTE
The Electromagnetic Interference Check is required only for initial system
installations and not required if the unit is removed or replaced.
1.
Communications
a.
Cockpit Intercom
Using the cockpit intercom, verify interference free communications between the crew while
monitoring the effects of the unit.
0040-17001-01
Installation Checkout
Page 3-31
Revision A
January 15, 2015
