Installation Manual

AVIATOR UAV 200
Installation Manual
Document: 677-A0219_IM issue 1.4
COBHAM PUBLIC
Page 22 of 61
5. MAINTENANCE
5.1 GENERAL
The AVIATOR UAV 200 does not require routine maintenance or adjustment apart from routine wiring
installation checks.
Non-disclosure. By using the AVIATOR UAV 200 you recognize that the radome/dust cover is not designed
to be a removable part and agree not to attempt its removal by any means. It is permanently bonded in
order to cover the antenna sub-assembly. The antenna sub-assembly also contains proprietary design
information that may not be accessed or disclosed without the express written consent of Omnipless
Manufacturing (PTY) Ltd.
5.1.1 Maintenance Intervals
There are no specified inspection intervals of the SATCOM system. Refer to Table 5-1 for information on
inspection actions applicable to the AVIATOR UAV 200.
Table 5-1: Inspection tasks for AVIATOR UAV 200
Inspection
Action
Check the radome/dust cover for cracks.
Return product to manufacturer (do
not attempt to remove radome/dust
cover from the product)
Check SATCOM-to-mounting structure ground
resistance.
Tighten mounting screws.
Check cabling for broken or frayed wires.
Replace the damaged wires.
5.1.2 Repair and Servicing
The AVIATOR UAV 200 is not field-repairable, and must be returned to the supplier for repair. For
information on how to return a unit for repair, see Section 9.2.
5.2 EVENTS GENERATED BY THE AVIATOR 200 UAV
If the AVIATOR 200 UAV malfunctions, it creates event logs stored in memory. The terminal can generate
an event log file on demand via the Web Interface DASHBOARD which can be downloaded and stored on the
attached computer. This event log file should be sent to the supplier to investigate the failure.
NOTE: The event log data is lost if the terminal is powered down, so any logs would need to be downloaded
while it is still powered to capture any failure conditions.
The following events may be generated by the terminal during power-on self-test or continuous monitoring:
 Satellite information
 Channel information
 Satellite Connection information
 Signal metrics
 Temperature
 CPU status
 HPA status
 DSP status
 Memory information
 Data sent and received
 USIM status
 Position
 Orientation
 Power supply
 Executable Software information
 AT Commands