Garmin GNS 430 Manuale operativo del pilota - Pagina 2

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Anche per Garmin GNS 430: Manuale del pilota (22 pagine), Manuale di istruzioni (6 pagine), Addendum al Manuale del Pilota (27 pagine), Addendum al Manuale del Pilota (4 pagine), Riferimento rapido (23 pagine), Addendum al Manuale del Pilota (22 pagine), Specifiche (2 pagine), Riferenza rapida (17 pagine), Manuale operativo (27 pagine)

Section 9

Supplements

Section 1 - General

The airplane is equipped with a Garmin GNS 430 GPS Navigator with

VHF Nav, ILS, and VHF Com herein referred to as the "Navigator." The

GNS 430 is capable of providing IFR enroute, terminal, and approach

navigation with position accuracies better than 15 meters. The system

utilizes the Global Positioning System (GPS) satellite network to derive

the airplane's position (latitude, longitude, and altitude) and the

altitude digitizer to enhance the altitude calculation.

The GARMIN GNS 430 GPS Navigator may be installed in single or

dual installations. If one GNS 430 is installed, it will be designated

'GPS 1,' and either a GARMIN GNC 250XLGPS Navigator or a

GARMIN GNC 420 GPS Navigator will be installed as GPS 2. Refer to

applicable supplements for descriptions of these units.

If two GARMIN GNS 430 Navigators are installed, the upper unit will

be designated 'GPS 1' and the lower unit will be designated 'GPS 2.' In

these installations, the MFD and the HSI will display GPS 1

information and the CDI (VOR/LOC/ILS/GS Indicator) will display GPS

2 information.

Refer to GPS 430 INTEGRATION in the NORMAL Procedures

Section of this supplement for a more detailed description of

GPS 430 integration in the various configurations.

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• Note •

Figure - 1

Garmin GNS 430 Front Panel

Cirrus Design

SR20

SR20_FM09_1109

P/N 11934-S22

Revision 2: 08-15-07