Honeywell International Inc. 9PGTPA-100A Manuale Utente

Page 2035

1 Dec 2003

CAS-100 COLLISION AVOIDANCE SYSTEM

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(1) Antenna Positioning and Wiring Specifications

Refer to paragraph 5.B.(1) and 5.C.(5).

(2) Mounting

Refer to manufacturer's installation documentation.

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.

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.

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.

Refer to applicable Mode S transponder system maintenance manual.