Garmin GIA 6300 Informazioni sull'installazione - Pagina 12

Sfoglia online o scarica il pdf Informazioni sull'installazione per Display avionico Garmin GIA 6300. Garmin GIA 6300 14.

9 GIA6300 Pin Out

See the GIA 6300 pin out at the Prism location below. This document also lists the keying for each

connector.

prism://hw-bin-vc.aviation.garmin.com/gia6300/trunk/Design/IO Board/GIA 6300 Pin Out.docx

Electrical equipment, supporting brackets, and racks should be electrically bonded to the aircraft's main

structure. Refer to SAE ARP 1870 section 5 when aluminum surface preparation is required to achieve

electrical bond. An equivalent OEM bonding procedure may also be substituted. The electrical bond

should achieve direct current (DC) resistance less than or equal to 2.5 milliohms to local structure to

where the equipment is mounted. Compliance should be verified by inspection using a calibrated

milliohm meter.

A statement like below should be in the harness fabrication section somewhere.

The wiring shall be prepared per the Garmin specifications, 190-00313-12 Circular Connector (and

Configuration module) Installation Instructions.

The GIA6300 VHF COM antenna should be well removed from all projections, engines and propellers.

The ground plane surface directly below the antenna should be a flat plane over as large an area as

possible (18 inches square, minimum). The antenna should be mounted a minimum of three feet from

any DME antennas, three feet from any GPS antennas, and as far as practical from the VHF NAV and ELT

antennas. Some ELTs have exhibited re-radiation problems generating harmonics which may interfere

with other signals.

In addition, the COM antenna must have at least 16 dB of isolation from other COM antennas to prevent

damage to the GIA6300 COM receiver. For COM antennas mounted on the same side of the fuselage, 16

dB of isolation can be achieved by a physical separation of approximately 4 feet (1.2 meters).

If simultaneous use of two or more COM transceivers is desired the COM antennas must be spaced for

maximum isolation. For a two COM installation, one COM antenna should be mounted on the top of the

fuselage and the other antenna should be mounted on the bottom of the fuselage. For installations with

three COM transceivers, one COM antenna should be mounted on the top of the fuselage and the other

two antennas should be mounted on the bottom of the fuselage and physically separated from each

other as much as possible.

The recommended minimum isolation between COM antennas for simultaneous use of two or more

COM units is 40 dB. Separating the COM antennas between the top and bottom of the fuselage typically

provides 35 – 45 dB of isolation for metal skin aircraft. For COM antennas mounted on the same side of

the fuselage, 40 dB of isolation can be achieved by a physical separation of approximately 60 feet (18.3

meters). At antenna isolations of less than 40 dB, there may be reductions in receiver sensitivity (range),

squelch breaks, or bleed-through.

190-01561-00

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GIA 6300 Installation Manual

Page 12