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P/N 11934-S22

Section 9

Cirrus Design

Supplements

SR20

2.

Single GARMIN GNS 430 (GPS 1) interfaced with the HSI and
MFD and a single GARMIN GNC 420 (GPS 2) interfaced with the
CDI (VOR/LOC) indicator.

a.

In this configuration, pressing the alternate-action CDI push-
button on the GARMIN GNS 430 (GPS 1) alternately selects
GPS or NAV for display on the HSI and MFD each time the
button is pressed. The HSI source is indicated by illumination
of the “GPS” or “VLOC” annunciation in the lower left corner of
the GNS 430 display. 

• Note •

The HSI displays course deviation from a VOR, Localizer
(LOC), or Glideslope (G/S) when VLOC is the navigation
source and displays GPS track deviation when GPS is
the selected navigation source.

b.

GPS 2 in this configuration is a GARMIN GNC 420 GPS
Navigator interfaced with the CDI (VOR/LOC Indicator). This
unit displays GPS data on the unit’s display panel and on the
remote CDI (VOR/LOC Indicator). 

Refer to the SR20 POH

Supplement for GARMIN GNC 420 GPS Navigator

, P/N

11934-S23. 

3.

Dual GARMIN GNS 430 units are installed. GPS 1 in this
configuration is the uppermost GNS 430 unit in the console and
GPS 2 is the lower GNS 430 unit.

a.

GPS 1 in this configuration is a GARMIN GNS 430 GPS
Navigator with VHF Com interfaced with the HSI and MFD.
Pressing the alternate-action CDI push-button on GPS 1
alternately selects GPS or NAV for display in the HSI and
MFD each time the button is depressed. The HSI source is
indicated by illumination of the “GPS” or “VLOC” annunciation
in the lower left corner of the GNS 430 display. 

• Note •

The HSI displays course deviation from a VOR, Localizer
(LOC) or Glideslope (G/S) when VLOC is the navigation
source and displays GPS track deviation when GPS is
the selected navigation source.

Revision 2: 08-15-07

Содержание GNS 430

Страница 1: ...ments Section Section 9 of the Cirrus Design SR20 Pilot s Operating Handbook This document must be carried in the airplane at all times Information in this supplement either adds to supersedes or dele...

Страница 2: ...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...

Страница 3: ...use of the GPS Navigator The software status stated in the pilot s guide must match that displayed on the equipment 3 The Navigator must utilize software version 2 XX where X is a digit 0 9 or later 4...

Страница 4: ...ilize remaining operational navigation equipment as required 2 If RAIM NOT AVAILABLE or RAIM POSITION WARNING message is displayed continue to navigate using the GPS equipment or revert to an alternat...

Страница 5: ...ree configurations 1 Single GARMIN GNS 430 GPS 1 interfaced with the CDI and MFD and a single GARMIN GNC 250XL GPS 2 not integrated with a remote indicator a In this configuration pressing the alterna...

Страница 6: ...tor interfaced with the CDI VOR LOC Indicator This unit displays GPS data on the unit s display panel and on the remote CDI VOR LOC Indicator Refer to the SR20 POH Supplement for GARMIN GNC 420 GPS Na...

Страница 7: ...GPS 1 Navigator Com Power Switch Rotate CCW OFF Section 5 Performance No change from basic Handbook Section 6 Weight Balance No change from basic Handbook Section 7 Systems Description Note This suppl...

Страница 8: ...paragraphs describe the GPS NAV and COM functions of this unit For a complete description as well as full operating instructions refer to the Garmin GNS 430 Pilot s Guide and Reference GPS Navigator...

Страница 9: ...ls are integrated into the Garmin GNS 430 control mounted in the center console The receiver control provides active and standby frequency indication frequency memory storage and knob operated frequen...

Страница 10: ...a standard feature found in GNS 430 units with main software version 5 01 or above and valid terrain and obstacle databases installed Garmin TERRAIN is a terrain awareness system incorporated into GNS...

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