User's Manual

SYSTEM DESCRIPTION AND INSTALLATION MANUAL
T
3
CAS/Part No.9005000
C. System Configurations
The T
3
CAS may be installed in different aircraft configurations depending on the current
TCAS, TAWS/RWS and Transponder equipment installed on the aircraft. The T
3
CAS
uses an Airplane Personality Module (APM) or embedded AAA to hold aircraft specific
configuration data. The APM is used in place of program pin inputs to provide system
configuration. An Aircraft Specific Database (ASDB) provides the aircraft specific
interface requirements for the T
3
CAS System and is loaded into the APM at the time of
system installation. The following table shows the core T
3
CAS configurable functions:
1-38
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
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