User's Manual

Table Of Contents
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
T
3
CAS/Part No.9005000
Table 4-2: T
3
CAS Computer Unit Interface Description
(Applicable to Part No. 9005000-11801 and -55801)
Connector
Pin
Designation
Functional Description
RMP-11E,
11F
ARINC 429 Input: MMR/GPS #1 (Left) [RMP-11E (A), RMP-11F (B)]
This high-speed 429 input is used to receive GPS label input containing position,
velocity and quality information for the use of ADS-B IN applications and by the
transponder function of ADS-B OUT.
RMP-11G,
11H
ARINC 429 Input: AFMC – EFIS #1 [RMP-11G (A), RMP-11H (B)]
This high-speed 429 input from the Flight Management Computer (FMC) Electronic
Flight Instrument System (EFIS) provides position, heading, track angle, speed, etc.
information to the T
3
CAS.
RMP-11J,
11K
ARINC 429 Input: ADIRU #1 (Left) / 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.
RMP-12A
Reserved Program Input
Reserved for future use.
4-52
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
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