Bedienungsanleitung Garmin GNS 430 (Seite 19 von 124) (Englisch)

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400 SERIES INSTALLATION MANUAL Page 2-3

P/N 190-00140-02 Page Rev L

2.2.8 COM, VOR/LOC, and Glideslope Antenna Installation Instructions

Install the COM, VOR/LOC, and Glideslope antennas according to the manufacturer’s recommendations.

Avoid running other wires and coaxial cables near the VOR/LOC antenna cable.

2.3 RACK CONSIDERATIONS

Plan a location which gives the pilot complete and comfortable access to the entire keypad and which is

plainly visible from the pilot’s perspective. Installation of remote switches and annunciators may not be

required if the 400 Series unit is installed in the pilot’s normal field of view (refer to the FAA letter in

Appendix B).

Check that there is adequate depth for the rack in the instrument panel. A location away from heating

vents or other sources of heat generation is optimal.

2.4 CABLING AND WIRING

Coaxial cable with 50 Ω nominal impedance and meeting applicable aviation regulations should be used

for the installation. A typical maximum cable length for the GPS antenna is 40 feet. The installer should

insure that the attenuation does not exceed 10 dB at 1.5 GHz for the specific installation.

Check that there is ample space for the cabling and mating connectors. Avoid sharp bends in cabling,

particularly the COM antenna cable, and routing near aircraft control cables. Cabling for the 400 Series

unit should not be routed near components or cabling which are sources of electrical noise. Do not route

the COM antenna coax near any ADF antenna cables. Route the GPS, VOR/LOC, and Glideslope antenna

cables as far as possible away from all COM transceivers and antenna cables.

2.5 COOLING AIR

The 400 Series units meet all TSO requirements without external cooling. However, as with all electronic

equipment, lower operating temperatures extend equipment life. On the average, reducing the operating

temperature by 15-20 °C (25 to 35 °F) doubles the mean time between failure (MTBF). Recommended

airflow rating is 1 CFM (cubic foot per minute) at a pressure equivalent to 0.1 inches of water. Potential

damage to your 400 Series unit may occur by using outside forced air to cool the equipment. Therefore, it

is recommended that an electric forced air fan be installed, of the indicated rating, to cool this equipment.

Units tightly packed in the avionics stack heat each other through radiation, convection, and sometimes by

direct conduction. Even a single unit operates at a much higher temperature in still air than in moving air.

Fans or some other means of moving the air around electronic equipment are usually a worthwhile

investment. A 5/8” diameter air fitting is provided on the rear of the mounting rack for the purpose of

admitting cooling air under such conditions. If a form of forced air cooling is installed, make certain that

rainwater cannot enter and be sprayed on the equipment.

2.6 MINIMUM INSTALLATION REQUIREMENTS

Below is a list of required devices for TSO C129a category A1 and A2 certification. For a specific list of

equipment used in the initial STC, obtain a copy of “GNS 430 in Piper PA32 Documented Installation”

(P/N 190-00140-06). The FAA or the governing organization should approve deviations from that set of

equipment.

Pressure Altitude Device

This device delivers pressure altitude data to the 400 Series unit. This data can come from a parallel

encoding altimeter, blind encoder, serializer, or an air data system.

Manual Course Device (Required for GNS 430 Only)

This device delivers the manual course select to the 400 Series unit, which is required for the GNS 430

VOR receiver, and optional for the 400/420/430 GPS receiver. Course information can come from an

analog resolver, or from an EFIS/EHSI via ARINC 429 serial data.

HSI/CDI Indicator or EFIS

This device displays Nav Flag, Left/Right, To/From, Glideslope Flag, and Up/Down. The indicator(s)

used in conjunction with the GNS 430 VOR/ILS receivers shall be TSO'd.

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