User's Manual

Table Of Contents
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
T
3
CAS/Part No.9005000
Table 4-1: T
3
CAS Computer Unit Interface Description (cont)
(Applicable to Part No. 9005000-10000, -10101, -10202, -10204, and -11203)
Connector
Pin
Designation
Functional Description
RMP-11G,
11H
ARINC 429 Input: FMC #1:EIS [RMP-11G (A), RMP-11H (B)]
This high-speed 429 input from the Flight Management Computer (FMC) Electronic
Instrument System (EIS) provides position information from the FMC to the T
3
CAS.
NOTE: These pins are designated for FMC #1 if T
3
CAS is operating in full
configuration mode with TAWS, TCAS and internal transponder enabled. Else
these pins are Spares.
RMP-11J,
11K
ARINC 429 Input: ADIRU #1/ADR [RMP-11J (A), RMP-11K (B)]
This low-speed 429 input from the Air Data/Inertial Reference Unit (ADIRU) #1
provides altitude, airspeed, altitude rate and temperature information to the T
3
CAS.
NOTE: These pins are designated for ADIRU #1 if T
3
CAS is operating in full
configuration mode with TAWS, TCAS and internal transponder enabled. Else
these pins are Spares.
RMP-12A
Reserved Program Input
Reserved for future use.
4-18
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.