Bedienungsanleitung Garmin GNS 430 (Seite 15 von 124) (Englisch)

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400 SERIES INSTALLATION MANUAL Page 1-7

P/N 190-00140-02 Page Rev L

1.4 LICENSE REQUIREMENTS

The following guidance is provided to help ensure the proper licensing of the GNC 420/GNS 430 COM:

1. The Telecommunications Act of 1996 effective February 8, 1996 provides the FCC discretion to

eliminate radio station license requirements for aircraft. At present, an individual license to operate

the 400 Series aboard a private aircraft is not needed in many circumstances. Please see FCC Fact

Sheet PR5000 or contact the FCC at 1-800-322-1117 for more information.

2. No license change is required for an aircraft which already has a station license per FCC 404

Instructions dated 1994.

3. If an aircraft license is required or desired, contact the FCC at 1-800-322-1117 to request FCC Form

404, “Application for Aircraft Radio Station License,” to apply for FCC authorization. The FCC also

has a “Fax on Demand” service to provide forms by FAX at 202-418-0177.

This equipment has been type accepted by the FCC. The bandwidth/emission designator is 6K00 A3E.

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 INVALIDATE THE LICENSE AND MAKE IT UNLAWFUL TO OPERATE THE

EQUIPMENT.

1.5 CERTIFICATION

The GPS receivers in the 400 Series units are certified for IFR enroute, terminal, and non-precision

approaches. The 400 Series initial certification was accomplished via STC’s by Garmin in a Piper PA32.

See Appendix B for copies of the STC’s.

The 400 Series units have been qualified to RTCA/DO-160 Section 22 lightning requirements. Special

installation considerations are required, refer to the Environmental Qualification Forms in Appendix A.

1.6 FAULT DETECTION AND EXCLUSION (FDE)

NOTE

The 400 Series equipment as installed has been found to comply with the requirements for GPS

primary means of navigation in oceanic and remote airspace, when used in conjunction with the

400 Series Trainer Program incorporating the FDE Prediction Program. This does not constitute

an operational approval.

The Garmin 400 Series Main and GPS Software version 3.00 and higher incorporate Fault Detection and

Exclusion (FDE) display interface and control, satisfying the requirements for GPS as a Primary Means of

Navigation for Oceanic/Remote Operations per FAA Notice N8110.60.

Fault Detection and Exclusion consists of two parts. The fault detection function detects a satellite failure

that can affect navigation. The exclusion function refers to the capability of excluding one or more failed

satellites and preventing them from affecting navigation.

FDE is provided for Oceanic and Remote Operations, non-precision approaches, en route and terminal

phases of flight. FDE for non-oceanic flight phases adhere to the same missed alert probability, false alert

probability, and failed exclusion probability specified by N8110.60.

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