
EX5000 Installation Manual
P/N 600-00073 Rev 24
- 85 -
6.2 Electro-Magnetic Compatibility (EMC) Check
The EMC check verifies that all of the electronic systems installed on the aircraft are compatible.
Operating the MFD should not result in Nav flags, constant location lightning strikes on the WX-500
sensor, noise on COMM channels, or other phenomena.
●
COM Radios
—Scan through radio channels to ensure there is no interference caused by the
MFD. Check random frequencies from 118.00 MHz through 136.975 MHz as well as your local
ground and tower frequencies to ensure there is no break in squelch due to the installation.
●
GPS
—Ensure that correct position is displayed and that there is no change in satellite signal
strength with the MFD powered off.
●
Autopilot
—Ensure that autopilot Self Test passes OK with the MFD powered on.
●
Other Instruments
—Verify there is no adverse effect on other instruments with the MFD powered
on.
6.3 Lightning Sensor Strike Test
After the Lightning Sensor has been installed and set up, as discussed in Section 5.6, “Lightning
Sensor Setup” on page 41,
Lightning Strike Test
will be available from the Maintenance Mode Page.
➤
To perform the Lightning Strike Test:
1.
Press Lightning Strike Test
from the Maintenance Mode PAge.
2.
The MFD will switch to the Map page and display a single strike at 15 mile range and 45 degrees
relative bearing. If it does not, there may be an inconsistency with the heading source, wiring, or
MFD setup.
6.4 Traffic Test
After completing all configuration procedures, confirm that the MFD is configured for the correct Traffic
sensor.
6.5 2-Way Datalink Satellite Reception Confirmation
The satellite networks transmit very low power signals that the EX5000 must receive. If the antenna is
not properly installed or if there is excessive electromagnetic interference (such as a nearby radio
transmitter, ground power cart, or inadequately grounded avionics), the system will not achieve
successful reception.
➤
To assess system performance.
1.
Bring the aircraft to an area with the clearest view of the sky to the horizon.
2.
Monitor the Datalink Info table (shown in Figure 22), for a few minutes (up to 5) under each of the
following conditions:
■
Other Avionics OFF
■
Avionics ON
■
Engines at idle
■
Engines at takeoff power.
Содержание 700-00004 Series
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