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The AEOLUS-SENSE PRO complies fully with applicable Electronic Emissions and Flame
Resistance standards. More specifically:
Electronic Emissions: The AEOLUS-SENSE PRO deploys a WiFi network with transmitter
power 9mW EIRP. Accordingly, it complies fully with the 10mW limit imposed by PS-
ANM-25-13 and part 15 of FCC rules.
Flame Resistance: Materials, design and construction of the AEOLUS-SENSE PRO are
flame resistant and in compliance with CAR regulation 3.
2 AEOLUS-SENSE PRO Maintenance
AEOLUS-SENSE PRO has been designed and manufactured for long and maintenance-free
operation. Still, care must be applied for the following:
AEOLUS-SENSE PRO Compass: Any replacement and/or relocation of metallic items in
the cockpit may require re-calibration of the Compass. Please follow the steps outlined in
section 1.4 of the current document for Compass calibration.
3 Use Limitations and Abnormal Operation
The temperature and voltage operational ranges of AEOLUS-SENSE PRO are as follows:
Temperature range:
-20C to 65C
or
-4F to 149F
Operation Voltage:
10-32Vdc
Operation Current:
for model 4 ADS-b =0.5A, for model 4T ADS-B max 4A during tablet
charging. Please use a fuse of 10A.
Inflight power reset:
in case of inflight power reset or if you turn on the unit during the flight after
losing your main systems, please note that there is
no limitation or constraint
of attitude for correct
operation of the AEOLUS-SENSE PRO. This means that the AEOLUS-SENSE PRO will recover in
any flight attitude, such as sharp turns, strong turbulence, etc. No constraint is imposed of straight
and leveled flight for recovery, which sometimes, in IMC is impossible to know. In this case, if you
don’t have a visual reference, please wait for about 40 to 60 secs for full recovery of the Artificial
Horizon.
Loss of GPS or Pitot/static:
our system uses both GPS and pitot/static for correct attitude
indication. In case of loss of one of them, correct operation relays on the other one. If you lose both,
then operation is based on less attitude accurate information provided by other inertial sensors and,
depending on the kind of flight, there will be a slight drift after 15 to 30 mins.
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