Installation Manual

AVIATOR UAV 200
Installation Manual
Document: 677-A0219_IM issue 1.4
COBHAM PUBLIC
Page 21 of 61
The overall pointing error of the antenna beam is dependent on the accuracy of the aircraft attitude data
provided by the navigation system. The total pointing error must be less than 2.5° to ensure optimal
performance.
The AVIATOR UAV 200 uses the installation angles as part of the beam steering calculations. See Section
8.1.1 – Initial Configuration of the AVIATOR UAV 200 for details on how to configure the installation angles.
4.5.8 Lightning Strike
The AVIATOR UAV 200 is not protected against direct lightning strikes.
4.6 EQUIPMENT INSTALLATION
Use six 8-32 UNC x 1D, 0.164” [4.1656 mm] screws to mount the terminal. Each screw fits into a locking
thread insert to ensure that the screws remain secure.
The mounting holes are used for bonding to the airframe for power dissipation and RF grounding.
The installer must ensure the correct length and type of mounting screws used. Refer to the Outline
Drawing [1] for the required mounting screw insertion depth.
4.7 AVIATOR UAV 200 REMOVAL
To remove the AVIATOR UAV 200 as follows after gaining access to the terminal in the aircraft:
1. Disconnect the external interface cable
2. Remove the six mounting screws