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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
and notes.
B. Tighten the mounting screws to secure the Configuration Module.
Rev 3, August/2002
10609I03.CDL
KMH 880/KTA 870
Figure 2- 2
Page 2-11
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