User's Manual

SYSTEM DESCRIPTION AND INSTALLATION MANUAL
TCAS 3000 Traffic Alert and Collision Avoidance System
344323
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
Page 450
15 Dec 2005
Table 48. XS950 Data Link Transponder Interface Descriptions (cont)
Connector Pin
Designation
Functional Description
P1C9 FAN RETURN (NO): ()
See pin P1C6.
P1C10 XPDR +28 V dc INPUT POWER: (H)
This pin along with the +28 V dc RETURN line (P1C3) provide the 28 V dc power
requirements for the transponder.
NOTE: Only 55XXX thru 99XXX transponders accept 28 V dc input power. If the 28
V dc version is used, the power should be connected through an 8 amp circuit
breaker, and the pins for the 115 V ac input (P1C1 and P1C7) should be left
unconnected.
P1C11 CHASSIS GROUND INPUT:
Connect to aircraft frame.
P1C12,
P1C13
MUTUAL SUPPRESSION BUS INPUT/OUTPUT:
LBand suppression coax must be RG142 or equivalent coaxial cable. P1C12 and
P1C13 are connected internally. Connection to only one pin is required.
The Interface descriptions that follow are for the 53pin ARINC 615 Portable Data Loader connector
J1 mounted on the front panel of the transponder. These descriptions are used to make up the
cable that is used to interface between the transponder and the ARINC 615 Data Loader or a
RS232 PC Serial Port.
J11, 2 XPDR ARINC 429 PDL BUS INPUT: (J11 [A], J12 [B])
This differential pair input is a high speed ARINC 429 bus (100K bits/second nominal) is
used to input data from the data loader to the transponder. The standards for this
interface are defined in ARINC 615 “Airborne Computer High Speed Data Loader”.
These pins should be connected to pins 1 and 2 of the PDL cable interface.
J15 INPUT BUS SHIELD:
The shields from the input bus (J11, 2) should be connected to this pin.
J18, 9 XPDR ARINC 429 PDL BUS OUTPUT: (J18 [A], J19 [B])
This differential pair output is a high speed ARINC 429 bus (100K bits/second nominal)
used to output data from the transponder to the data loader. The standards for this
interface are defined in ARINC 615 “Airborne Computer High Speed Data Loader”.
These pins should be connected to pins 8 and 9 of the PDL cable interface.
J116 OUTPUT BUS SHIELD:
The shields from the output bus (J18, 9) should be connected to this pin.
J118 PDL LINK A:
Connect this pin to pin 18 of the PDL cable interface.
J119 PDL LINK B:
Connect this pin to pin 19 of the PDL cable interface.