B
B
B
B
2.2.4
Configuration Module Installation
System configuration is defined via a Configuration Module which contains the aircraft
interface and functionality definitions specific to the installed aircraft.
2.2.4.1
Cooling Considerations
A. Make sure that the unit is installed in a location where the ambient tem-
peratures are -67°F to +158°F (-55°C to +70°C).
2.2.4.2
Installation Considerations
A. The Configuration Module must be mounted to the airframe within maxi-
mum cable/harness length of 2 feet. Make sure to leave adequate space
to mount the Configuration Module when installing the Processor Unit.
2.2.4.3
Installation Procedure
A. Install the Configuration Module into the airframe. Refer to figure 2- 2 .
B. Tighten the mounting screws to secure the Configuration Module.
Rev 0, October/2000
10609I00.ZIPCDL
KMH 880/KTA 870
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