Honeywell International Inc. 9PGTPA-100A Benutzerhandbuch
Page 2035
1 Dec 2003
34-45-4
7
MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
C. TCAS Omni Antenna Installation
(1) Antenna Positioning and Wiring Specifications
Refer to paragraph 5.B.(1) and 5.C.(5).
(2) Mounting
Refer to manufacturer's installation documentation.
D. TA/VSI and RA/VSI Unit Installation
The TA/VSI or RA/VSI display units must be installed in a applicable location in the aircraft
cockpit, giving careful thought to see and easy operation. Both the TA/VSI and RA/VSI use
customer supplied screw clamp fasteners to attach them to the instrument panel. Use the
outline drawings Figures 2011, 2012, and 2013 for reference to position the display units and
to cut and drill the instrument panel.
cockpit, giving careful thought to see and easy operation. Both the TA/VSI and RA/VSI use
customer supplied screw clamp fasteners to attach them to the instrument panel. Use the
outline drawings Figures 2011, 2012, and 2013 for reference to position the display units and
to cut and drill the instrument panel.
Attach the electrical connector to the aft of the units. If an optional aircraft pressure source is
used as an input to the TA/VSI or RA/VSI attach the pneumatic tube to the aft of the units.
used as an input to the TA/VSI or RA/VSI attach the pneumatic tube to the aft of the units.
E. Dedicated TCAS Traffic Display
The ITA-81A Traffic Display must installed in a applicable location in the aircraft cockpit, in
available reach and view of the personnel. Four Dzus fasteners (Type PPSC35-44A), one
found at each corner of the front panel, attach the display to the aircraft instrument panel. All
electrical connections between the system and the display are made through the connector
plug found at the aft of the unit. Make sure that there is sufficient clearance permitted at the
aft of the unit for the connecting cable assembly. The total mounting space necessary can be
determined from the dimension data contained on Figure 2014.
available reach and view of the personnel. Four Dzus fasteners (Type PPSC35-44A), one
found at each corner of the front panel, attach the display to the aircraft instrument panel. All
electrical connections between the system and the display are made through the connector
plug found at the aft of the unit. Make sure that there is sufficient clearance permitted at the
aft of the unit for the connecting cable assembly. The total mounting space necessary can be
determined from the dimension data contained on Figure 2014.
F. Mode S Transponder System Component Installation
Refer to applicable Mode S transponder system maintenance manual.