Honeywell CAS-100 Maintenance Manual page 50

Table 3. Aircraft Equipment Required But Not Supplied By Honeywell (cont)
Aircraft Equipment
Aircraft Switches Landing Gear Switch
Air/Ground Switch
Suppression Bus
Static Input Source (pneumatic)
OR
Altitude Rate Source (electrical)
Pressure Altimeter Source
Cockpit Speaker
Miscellaneous Installation Hardware
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
Supplies the aircraft landing gear extended or retracted
discrete status input to the TCAS processor.
Supplies the aircraft on-the-ground/ in-flight discrete
status input to the TCAS processor.
Supplies mutual suppression of L-band
equipment on the aircraft including the TCAS processor
bi-directional bus.
Supplies the aircraft static pressure source input to the
TA/VSI or RA/VSI.
Supplies the aircraft altitude rate on an electrical ARINC
429, ARINC 565, or ARINC 575 input to the TA/VSI or
RA/VSI.
Supplies the aircraft pressure altitude input to the Mode
S transponder. Refer to the applicable Mode S
transponder system maintenance manual for the types of
pressure altimeters that can be used with the Mode S
transponder.
Audio speaker, 8 ohms, 4 watts nominal. Annunciates
voice advisory messages from the voice synthesizer in
TPA-81A TCAS processor.
Assembly brackets, wire, cables, nuts, bolts, screws, and
etc.
Description
34-45-47
Page 16
1 Dec 2003