Honeywell International Inc. 9PGTPL-100A Manuale Utente

Page 22

1 Mar 2006

TPL-100A Processor / Part No. 940-0530-001

Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.

 

115 V 400 Hz

Primary power source for MILACAS-FR 
Processor, TA/VSI, RA/VSI, dedicated TCAS 
traffic display, and Mode S transponder system

5 V ac or dc, or 28 V dc lighting bus

Panel lighting power source for TA/VSI, RA/VSI, 
and dedicated TCAS traffic display

5 V ac or 28 V dc power source
(separate)

Fault lamp power for Mode S transponder/TCAS 
control unit

ARINC 429 Attitude/heading
reference system (digital)

Supplies own pitch, roll, and heading of the 
aircraft on an ARINC 429 digital input to the 
MILACAS-FR Processor.

Radio altimeter - digital type
(one or two)

Supplies the altitude of own aircraft on an 
ARINC 429 digital input to the MILACAS-FR 
Processor.

Aircraft switches

• Landing gear switch

•  Air/ground switch

Supplies the status of aircraft landing gear 
extended or retracted discrete input to 
MILACAS-FR Processor.

Supplies the status of aircraft on-the-ground/ 
in-flight discrete status input to MILACAS-FR 
Processor.

Suppression bus

Supplies mutual suppression of L-band
equipment on aircraft including MILACAS-FR 
Processor bidirectional bus.

Altitude rate source
(electrical)

Supplies the altitude rate of the aircraft on an 
electrical ARINC 429, ARINC 565, or ARINC 
575 input to the TA/VSI and RA/VSI.

Pressure altimeter source

Supplies the 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.

Cockpit speaker

Audio speaker, 8 ohms, 4 Watts nominal. 
Annunciates voice advisory messages from the 
voice synthesizer in the MILACAS-FR 
Processor.

Miscellaneous installation
hardware

Mounting bracketry, wire, cables, nuts, bolts, 
screws, and other items.