User's Manual Part 2
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CAS / Part No. 9000000
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
34-43-20
15 Feb 2003
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
4--20
Table 4--1. TT--950/951/952 T
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CAS Computer Unit Interface Description (cont)
Connector Pin
Designation
Functional Description
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CAS Computer Unit Left Top Plug (LTP)
LTP --1 Top Antenna 0 Degree Port
J1 on the antenna is color--coded yellow. This antenna port (Note 2) is called the 0
degree port because it produces a transmission pattern in the forward quadrant of the
aircraft. J1 is physically located toward the rear of the antenna and to the rear of the
aircraft when antenna is properly installed. The T
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CAS computer unit checks the built--in
dc to ground resistance of this antenna port. It must detect approximately 1000 Ohms or
TCAS fails its antenna test.
LTP --2 Top Antenna 270 Degree Port
J2 on the antenna is color--coded black. This antenna port (Note 2) is called the 270
degree port because it produces a transmission pattern in the left wing quadrant of the
aircraft. J2 is physically located toward the right wing of the aircraft when antenna is
properly installed. The TCAS function checks the built--in dc to ground resistance of this
antenna port. It must detect approximately 8000 Ohms or it reports antenna test failure.
LTP --3 Top Antenna 180 Degree Port
J3 on the antenna is color--coded blue. This antenna port (Note 2) is called the 180
degree port because it produces a transmission pattern in the rear quadrant of the
aircraft. J3 is physically located toward the front of the antenna and to the front of the
aircraft when antenna is installed properly. The T
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CAS computer unit checks the built--in
dc to ground resistance of this antenna port. It must detect approximately 4000 Ohms or
it reports antenna test failure.
LTP --4 Top Antenna 90 Degree Port
J4 on the antenna is color--coded red. This antenna port (Note 2) is called the 90 degree
port because it produces a transmission pattern in the right wing quadrant of the aircraft.
J4 is physically located toward the left wing of the aircraft when antenna is properly
installed. The TCAS function checks the built--in dc to ground resistance of this antenna
port. It must detect approximately 2000 Ohms or it reports antenna test failure.
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CAS Computer Unit Left Middle Plug (LMP)
LMP --1 Bottom Antenna 0 Degree Port
J1 on the antenna is color--coded yellow. Same as top antenna 0 degree port (LTP--1).
In addition, this port (Note 2) is used as the omnidirectional antenna connection. The
TCAS function determines that a bottom omnidirectional antenna is installed if it detects
less than 500 Ohms (50 Ohms typical) to ground on this pin and an open circuit (>13k
Ohms) at LMP-- 2, --3, and --4 or a dc short (<500 Ohms) if unused ports are terminated
at back of mounting tray.
LMP --2 Bottom Antenna 90 Degree Port
J2 on the antenna is color--coded black. This antenna port (Note 2) is called the 90
degree port because it produces a transmission pattern in the right wing quadrant of the
aircraft. J2 is physically located toward the left wing of the aircraft when antenna is
properly installed. The TCAS function checks the built in dc to ground resistance of this
antenna port. It must detect approximately 8000 Ohms or it reports antenna test failure.