Dimensions (maximum)
6
MCU Short per ARINC 600
Height . . . . . . . . . . . . . . . . . . . 7.64 in. (194.06 mm)
Width. . . . . . . . . . . . . . . . . . . . 7.75 in. (196.85 mm)
Length (from rear of connector) . . . . . . . 12.75 in. (323.85 mm)
Weight . . . . . . . . . . . . . . . . . . . . . . . . 24.01b(10.9 kg)
Power Requirements . . . . . . . . . 115 V ac 400 Hz, 80 Watts (maximum)
Mating Connector . . . . . . . . . . . . .
TRI-STAR
PN C-O6B5-99O1-O1OO
Mounting: . . . . . . . . . . . . . . . . . . . . . .
Non Honeywell Tray
RT-91O TCAS Computer Leading Particulars
Table 13-1
The TCAS computer contains the RF transmitter and receivers necessary to
interrogate and
receive replies from transponder equipped aircraft. Dual
microprocessors are utilized to implement the surveillance and collision
avoidance algorithms to decide whether an intruder aircraft should be
considered a threat, and then to determine the appropriate vertical response
to avoid a midair collision or near midair incident.
In addition, output
data is provided to drive displays, and the aircraft audio system, to inform
the flight crew as to what action to take or avoid. An interface is
provided with an on-board Mode S transponder in order to coordinate avoid-
ance maneuvers with other TCAS equipped aircraft. The TCAS computer
transmits ARINC 429 high speed output data to the SG-884 Symbol Generators
as specified in Table 13-2.
22-14-00
Page 198.185
Apr 15/93
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