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
RTP-13H
Programmable/Strobed Ground Discrete Output
Spare /TAWS/XPDR 500 mA
RTP-13J
Ground Discrete Output
Terrain Display Select #1 500 mA
RTP-13K
Programmable/Strobed Ground Discrete Output
Spare /TAWS/XPDR 500 mA
RTP-14A
Ground Discrete Output
Terrain Display Select #2 500 mA
RTP-14B
Ground Discrete Monitor Output
GPWS Monitor 250 mA
RTP-14C
Ground Discrete Monitor Output
Terrain Not Available Monitor 250 mA
RTP-14D
Ground Discrete Monitor Output
Terrain Monitor 250 mA
RTP-14E
Discrete Input (Gnd/Open)
XPDR Functional Test
RTP-14F
Discrete Input (Gnd/Open), Latch
Standby/ON
RTP-14G
Discrete Input (Gnd/Open)
XPDR Mode S Address Bit A23
RTP-14H
Discrete Input (Gnd/Open)
XPDR Mode S Address Bit A24
RTP-14J
Ground Discrete Output
Spare
RTP-14K
Discrete Output 500 mA
XPDR Fail #2
RTP-15A
Discrete Output 5 V dc / 100 mA
XPDR Fail #1
RTP-15B,
15C
ARINC 429 TCAS Output
This bus outputs Dataloader or ADLP COMM A data.
RTP-15D
APM Power
+12 V dc power source for the Airplane Personality Module. Connect to APM J1-7.
RTP-15E
APM Return
This is the Ground return for +12 V dc APM power source. Connect to APM J1-8.
See pin RTP-15D
4-44
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
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