Sequence Hold Low:

Input, when grounded, activates HOLD mode. See

(Pin 13)

the GNC 300 Pilot's Guide (GPN 190-00067-00) for

 

more information.

1.2.3.3 COMM Antenna Connector (J4)

Capable of providing 5 watts, minimum, at 13.8V. Sensitivity of 6 dB SNR, minimum, at 2 uV hard. The COMM antenna shall be approved to TSO C37( ) and C38( ).

1.3LICENCE REQUIREMENTS

The transmitter, as installed in the aircraft, requires an Aircraft Radio Station Licence. This licence is obtained by filing the FCC Form 404. While awaiting the receipt of the station licence, a copy of FCC Form 404 is kept in the aircraft.

This equipment has been type accepted by the FCC and entered on the type accepted equipment list, as GARMIN GNC 300 and must be identified as GARMIN GNC 300 on your Form 404, Aircraft Radio Station Licence application.

CAUTION

THE VHF TRANSMITTER IN THIS EQUIPMENT IS GUARANTEED TO MEET FEDERAL COMMUNICATIONS COMMISSION ACCEPTANCE OVER THE OPERATING TEMPERATURE RANGE. MODIFICATIONS NOT EXPRESSLY APPROVED BY GARMIN COULD VOID THE LICENCES' AUTHORITY TO OPERATE THE EQUIPMENT.

SECTION 2 INSTALLATION CONSIDERATIONS

Careful planning and consideration of the suggestions in this section are required to achieve the desired performance and reliability from the GNC 300.

2.1ANTENNA CONSIDERATIONS 2.1.1 GPS ANTENNA LOCATION

The GNC 300 GA 56 Antenna must be mounted on top of the aircraft. For best performance select a location with an unobstructed view of the sky above the aircraft when in level flight. Figure 2-1 illustrates a typical GPS antenna installation.

For rotorcraft, locate the GA 56 antenna:

1)As far from the main rotor hub as possible. This reduces the percentage of time the blade blocks the antenna.

2)As far below the blade surface as possible if installing the antenna under the blade. This reduces signal distortion caused by the blades.

Av. Kit Install. Manual

190-00067-02 Rev. J

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